Ardupilot

Più simili a questo

SPS 170

da mohd fadhil baharudin

Dreams

da Jessica Roff

Phrasal Verb Take

da jessica vanessa

INGLES

da Rodrigo Cano

AP_Param/AP_Param.h

AP_Param.cpp

AP_Menu/AP_Menu.h

AP_Menu.h

AP_Math/AP_Math.h

vector3.h

vector2.h

rotations.h

quaternion.h

polygon.h

matrix3.h

location.h

edc.h

definitions.h

AP_Location.h

Location.cpp

AP_Common.cpp

Utility

AP_HAL

system.h

HAL.h

SPIDevice.h

Device.h

OpticalFlow.h

Util.h

Semaphores.h

Scheduler.h

RCOutput.h

RCInput.h

GPIO.h

Storage.h

AnalogIn.h

UARTDriver.h

AP_HAL_Main.h

AP_HAL_Macros.h

AP_HAL_Boards.h

AP_HAL_Namespace.h

AP_Avoidance/AP_Avoidance.h

AP_Common/AP_Common.h

AP_AdvancedFailsafe/AP_AdvancedFailsafe.h

#include // Common dependencies #include #include #include #include #include // Application dependencies #include #include // Serial manager library #include // ArduPilot GPS library #include // ArduPilot Mega Flash Memory Library #include // ArduPilot Mega Analog to Digital Converter Library #include #include // ArduPilot Mega Magnetometer Library #include // ArduPilot Mega Vector/Matrix math Library #include // interface and maths for accelerometer calibration #include // ArduPilot Mega Inertial Sensor (accel & gyro) Library #include #include #include #include // Mission command library #include // PID library #include // PID library (2-axis) #include // Heli specific Rate PID library #include // P library #include // Attitude control library #include // Attitude control library for traditional helicopter #include // Position control library #include // RC Channel Library #include // AP Motors library #include // Range finder library #include #include // statistics library #include #include // Optical Flow library #include // RSSI Library #include // Filter library #include // APM FIFO Buffer #include // APM relay #include #include // Photo or video camera #include // Camera/Antenna mount #include // needed for AHRS build #include // needed for AHRS build #include // ArduPilot Mega inertial navigation library #include // ArduCopter waypoint navigation library #include // circle navigation library #include // ArduPilot Mega Declination Helper Library #include // Arducopter Fence library #include // Arducopter stop at fence library #include // main loop scheduler #include // RC input mapping library #include // Notify library #include // Battery monitor library #include // board configuration library #include // Landing Gear library #include #include #include #include // Pilot input handling library #include // Heli specific pilot input handling library #include SITL/SITL.h

AP_Arming/AP_Arming.h

AP_Rally/AP_Rally.h

GCS_MAVLink/GCS.h

#include

AP_AHRS/AP_AHRS.h

ArduCopter.h

StorageManager/StorageManager.h

Copter.h

/*

  This program is free software: you can redistribute it and/or modify

  it under the terms of the GNU General Public License as published by

  the Free Software Foundation, either version 3 of the License, or

  (at your option) any later version.

  This program is distributed in the hope that it will be useful,

  but WITHOUT ANY WARRANTY; without even the implied warranty of

  MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the

  GNU General Public License for more details.

  You should have received a copy of the GNU General Public License

  along with this program. If not, see <http://www.gnu.org/licenses/>.

 */

#pragma once

/*

 This is the main Copter class

 */

////////////////////////////////////////////////////////////////////////////////

// Header includes

////////////////////////////////////////////////////////////////////////////////

#include <cmath>

#include <stdio.h>

#include <stdarg.h>

#include <AP_HAL/AP_HAL.h>

// Common dependencies

#include <AP_Common/AP_Common.h>

#include <AP_Common/Location.h>

#include <AP_Menu/AP_Menu.h>

#include <AP_Param/AP_Param.h>

#include <StorageManager/StorageManager.h>

// Application dependencies

#include <GCS_MAVLink/GCS.h>

#include <AP_SerialManager/AP_SerialManager.h> // Serial manager library

#include <AP_GPS/AP_GPS.h>      // ArduPilot GPS library

#include <DataFlash/DataFlash.h>     // ArduPilot Mega Flash Memory Library

#include <AP_ADC/AP_ADC.h>      // ArduPilot Mega Analog to Digital Converter Library

#include <AP_Baro/AP_Baro.h>

#include <AP_Compass/AP_Compass.h>    // ArduPilot Mega Magnetometer Library

#include <AP_Math/AP_Math.h>      // ArduPilot Mega Vector/Matrix math Library

#include <AP_AccelCal/AP_AccelCal.h>        // interface and maths for accelerometer calibration

#include <AP_InertialSensor/AP_InertialSensor.h> // ArduPilot Mega Inertial Sensor (accel & gyro) Library

#include <AP_AHRS/AP_AHRS.h>

#include <AP_NavEKF2/AP_NavEKF2.h>

#include <AP_NavEKF3/AP_NavEKF3.h>

#include <AP_Mission/AP_Mission.h>    // Mission command library

#include <AC_PID/AC_PID.h>      // PID library

#include <AC_PID/AC_PI_2D.h>     // PID library (2-axis)

#include <AC_PID/AC_HELI_PID.h>    // Heli specific Rate PID library

#include <AC_PID/AC_P.h>       // P library

#include <AC_AttitudeControl/AC_AttitudeControl_Multi.h> // Attitude control library

#include <AC_AttitudeControl/AC_AttitudeControl_Heli.h> // Attitude control library for traditional helicopter

#include <AC_AttitudeControl/AC_PosControl.h>   // Position control library

#include <RC_Channel/RC_Channel.h>    // RC Channel Library

#include <AP_Motors/AP_Motors.h>     // AP Motors library

#include <AP_RangeFinder/AP_RangeFinder.h>  // Range finder library

#include <AP_Proximity/AP_Proximity.h>

#include <AP_Stats/AP_Stats.h>  // statistics library

#include <AP_Beacon/AP_Beacon.h>

#include <AP_OpticalFlow/AP_OpticalFlow.h>  // Optical Flow library

#include <AP_RSSI/AP_RSSI.h>         // RSSI Library

#include <Filter/Filter.h>      // Filter library

#include <AP_Buffer/AP_Buffer.h>     // APM FIFO Buffer

#include <AP_Relay/AP_Relay.h>     // APM relay

#include <AP_ServoRelayEvents/AP_ServoRelayEvents.h>

#include <AP_Camera/AP_Camera.h>     // Photo or video camera

#include <AP_Mount/AP_Mount.h>     // Camera/Antenna mount

#include <AP_Airspeed/AP_Airspeed.h>    // needed for AHRS build

#include <AP_Vehicle/AP_Vehicle.h>    // needed for AHRS build

#include <AP_InertialNav/AP_InertialNav.h>  // ArduPilot Mega inertial navigation library

#include <AC_WPNav/AC_WPNav.h>     // ArduCopter waypoint navigation library

#include <AC_WPNav/AC_Circle.h>     // circle navigation library

#include <AP_Declination/AP_Declination.h>  // ArduPilot Mega Declination Helper Library

#include <AC_Fence/AC_Fence.h>     // Arducopter Fence library

#include <AC_Avoidance/AC_Avoid.h>     // Arducopter stop at fence library

#include <AP_Scheduler/AP_Scheduler.h>   // main loop scheduler

#include <AP_RCMapper/AP_RCMapper.h>    // RC input mapping library

#include <AP_Notify/AP_Notify.h>     // Notify library

#include <AP_BattMonitor/AP_BattMonitor.h>  // Battery monitor library

#include <AP_BoardConfig/AP_BoardConfig.h>  // board configuration library

#include <AP_LandingGear/AP_LandingGear.h>  // Landing Gear library

#include <AP_Terrain/AP_Terrain.h>

#include <AP_ADSB/AP_ADSB.h>

#include <AP_RPM/AP_RPM.h>

#include <AC_InputManager/AC_InputManager.h>    // Pilot input handling library

#include <AC_InputManager/AC_InputManager_Heli.h> // Heli specific pilot input handling library

#include <AP_Button/AP_Button.h>

#include <AP_Arming/AP_Arming.h>

// Configuration

#include "defines.h"

#include "config.h"

#include "GCS_Mavlink.h"

#include "AP_Rally.h"     // Rally point library

#include "AP_Arming.h"

// libraries which are dependent on #defines in defines.h and/or config.h

#if SPRAYER == ENABLED

#include <AC_Sprayer/AC_Sprayer.h>    // crop sprayer library

#endif

#if GRIPPER_ENABLED == ENABLED

#include <AP_Gripper/AP_Gripper.h>      // gripper stuff

#endif

#if PARACHUTE == ENABLED

#include <AP_Parachute/AP_Parachute.h>   // Parachute release library

#endif

#if PRECISION_LANDING == ENABLED

#include <AC_PrecLand/AC_PrecLand.h>

#include <AP_IRLock/AP_IRLock.h>

#endif

#if FRSKY_TELEM_ENABLED == ENABLED

#include <AP_Frsky_Telem/AP_Frsky_Telem.h>

#endif

#if ADVANCED_FAILSAFE == ENABLED

#include "afs_copter.h"

#endif

// Local modules

#include "Parameters.h"

#include "avoidance_adsb.h"

#if CONFIG_HAL_BOARD == HAL_BOARD_SITL

#include <SITL/SITL.h>

#endif

class Copter : public AP_HAL::HAL::Callbacks {

public:

  friend class GCS_MAVLINK_Copter;

  friend class AP_Rally_Copter;

  friend class Parameters;

  friend class ParametersG2;

  friend class AP_Avoidance_Copter;

#if ADVANCED_FAILSAFE == ENABLED

  friend class AP_AdvancedFailsafe_Copter;

#endif

  friend class AP_Arming_Copter;

  Copter(void);

  // HAL::Callbacks implementation.

  void setup() override;

  void loop() override;

private:

  // key aircraft parameters passed to multiple libraries

  AP_Vehicle::MultiCopter aparm;

  // cliSerial isn't strictly necessary - it is an alias for hal.console. It may

  // be deprecated in favor of hal.console in later releases.

  AP_HAL::BetterStream* cliSerial;

  // Global parameters are all contained within the 'g' class.

  Parameters g;

  ParametersG2 g2;

  // main loop scheduler

  AP_Scheduler scheduler;

  // AP_Notify instance

  AP_Notify notify;

  // used to detect MAVLink acks from GCS to stop compassmot

  uint8_t command_ack_counter;

  // has a log download started?

  bool in_log_download;

  // primary input control channels

  RC_Channel *channel_roll;

  RC_Channel *channel_pitch;

  RC_Channel *channel_throttle;

  RC_Channel *channel_yaw;

  // Dataflash

  DataFlash_Class DataFlash;

  AP_GPS gps;

  // flight modes convenience array

  AP_Int8 *flight_modes;

  AP_Baro barometer;

  Compass compass;

  AP_InertialSensor ins;

  RangeFinder rangefinder {serial_manager, ROTATION_PITCH_270};

  struct {

    bool enabled:1;

    bool alt_healthy:1; // true if we can trust the altitude from the rangefinder

    int16_t alt_cm;  // tilt compensated altitude (in cm) from rangefinder

    uint32_t last_healthy_ms;

    LowPassFilterFloat alt_cm_filt; // altitude filter

    int8_t glitch_count;

  } rangefinder_state = { false, false, 0, 0 };

  AP_RPM rpm_sensor;

  // Inertial Navigation EKF

  NavEKF2 EKF2{&ahrs, barometer, rangefinder};

  NavEKF3 EKF3{&ahrs, barometer, rangefinder};

  AP_AHRS_NavEKF ahrs{ins, barometer, gps, rangefinder, EKF2, EKF3, AP_AHRS_NavEKF::FLAG_ALWAYS_USE_EKF};

#if CONFIG_HAL_BOARD == HAL_BOARD_SITL

  SITL::SITL sitl;

#endif

  // Mission library

  AP_Mission mission;

  // Arming/Disarming mangement class

  AP_Arming_Copter arming {ahrs, barometer, compass, battery, inertial_nav, ins};

  // Optical flow sensor

#if OPTFLOW == ENABLED

  OpticalFlow optflow{ahrs};

#endif

  // gnd speed limit required to observe optical flow sensor limits

  float ekfGndSpdLimit;

  // scale factor applied to velocity controller gain to prevent optical flow noise causing excessive angle demand noise

  float ekfNavVelGainScaler;

  // system time in milliseconds of last recorded yaw reset from ekf

  uint32_t ekfYawReset_ms = 0;

  int8_t ekf_primary_core;

  // GCS selection

  AP_SerialManager serial_manager;

  static const uint8_t num_gcs = MAVLINK_COMM_NUM_BUFFERS;

  GCS_MAVLINK_Copter gcs_chan[MAVLINK_COMM_NUM_BUFFERS];

  GCS _gcs; // avoid using this; use gcs()

  GCS &gcs() { return _gcs; }

  // User variables

#ifdef USERHOOK_VARIABLES

# include USERHOOK_VARIABLES

#endif

  // Documentation of GLobals:

  union {

    struct {

      uint8_t unused1        : 1; // 0

      uint8_t simple_mode      : 2; // 1,2  // This is the state of simple mode : 0 = disabled ; 1 = SIMPLE ; 2 = SUPERSIMPLE

      uint8_t pre_arm_rc_check    : 1; // 3   // true if rc input pre-arm checks have been completed successfully

      uint8_t pre_arm_check     : 1; // 4   // true if all pre-arm checks (rc, accel calibration, gps lock) have been performed

      uint8_t auto_armed       : 1; // 5   // stops auto missions from beginning until throttle is raised

      uint8_t logging_started    : 1; // 6   // true if dataflash logging has started

      uint8_t land_complete     : 1; // 7   // true if we have detected a landing

      uint8_t new_radio_frame    : 1; // 8   // Set true if we have new PWM data to act on from the Radio

      uint8_t usb_connected     : 1; // 9   // true if APM is powered from USB connection

      uint8_t rc_receiver_present  : 1; // 10   // true if we have an rc receiver present (i.e. if we've ever received an update

      uint8_t compass_mot      : 1; // 11   // true if we are currently performing compassmot calibration

      uint8_t motor_test       : 1; // 12   // true if we are currently performing the motors test

      uint8_t initialised      : 1; // 13   // true once the init_ardupilot function has completed. Extended status to GCS is not sent until this completes

      uint8_t land_complete_maybe  : 1; // 14   // true if we may have landed (less strict version of land_complete)

      uint8_t throttle_zero     : 1; // 15   // true if the throttle stick is at zero, debounced, determines if pilot intends shut-down when not using motor interlock

      uint8_t system_time_set    : 1; // 16   // true if the system time has been set from the GPS

      uint8_t gps_base_pos_set    : 1; // 17   // true when the gps base position has been set (used for RTK gps only)

      enum HomeState home_state   : 2; // 18,19 // home status (unset, set, locked)

      uint8_t using_interlock    : 1; // 20   // aux switch motor interlock function is in use

      uint8_t motor_emergency_stop  : 1; // 21   // motor estop switch, shuts off motors when enabled

      uint8_t land_repo_active    : 1; // 22   // true if the pilot is overriding the landing position

      uint8_t motor_interlock_switch : 1; // 23   // true if pilot is requesting motor interlock enable

      uint8_t in_arming_delay    : 1; // 24   // true while we are armed but waiting to spin motors

    };

    uint32_t value;

  } ap;

  // This is the state of the flight control system

  // There are multiple states defined such as STABILIZE, ACRO,

  control_mode_t control_mode;

  mode_reason_t control_mode_reason = MODE_REASON_UNKNOWN;

  control_mode_t prev_control_mode;

  mode_reason_t prev_control_mode_reason = MODE_REASON_UNKNOWN;

  // Structure used to detect changes in the flight mode control switch

  struct {

    int8_t debounced_switch_position; // currently used switch position

    int8_t last_switch_position;    // switch position in previous iteration

    uint32_t last_edge_time_ms;    // system time that switch position was last changed

  } control_switch_state;

  struct {

    bool running;

    float max_speed;

    float alt_delta;

    uint32_t start_ms;

  } takeoff_state;

  // altitude below which we do no navigation in auto takeoff

  float auto_takeoff_no_nav_alt_cm;

  RCMapper rcmap;

  // board specific config

  AP_BoardConfig BoardConfig;

  // receiver RSSI

  uint8_t receiver_rssi;

  // Failsafe

  struct {

    uint8_t rc_override_active : 1; // 0 // true if rc control are overwritten by ground station

    uint8_t radio       : 1; // 1 // A status flag for the radio failsafe

    uint8_t battery      : 1; // 2 // A status flag for the battery failsafe

    uint8_t gcs        : 1; // 4 // A status flag for the ground station failsafe

    uint8_t ekf        : 1; // 5 // true if ekf failsafe has occurred

    uint8_t terrain      : 1; // 6 // true if the missing terrain data failsafe has occurred

    uint8_t adsb        : 1; // 7 // true if an adsb related failsafe has occurred

    int8_t radio_counter;      // number of iterations with throttle below throttle_fs_value

    uint32_t last_heartbeat_ms;   // the time when the last HEARTBEAT message arrived from a GCS - used for triggering gcs failsafe

    uint32_t terrain_first_failure_ms; // the first time terrain data access failed - used to calculate the duration of the failure

    uint32_t terrain_last_failure_ms; // the most recent time terrain data access failed

  } failsafe;

  // sensor health for logging

  struct {

    uint8_t baro    : 1;  // true if baro is healthy

    uint8_t compass  : 1;  // true if compass is healthy

    uint8_t primary_gps;    // primary gps index

  } sensor_health;

  // Motor Output

#if FRAME_CONFIG == HELI_FRAME

 #define MOTOR_CLASS AP_MotorsHeli_Single

#else

 #define MOTOR_CLASS AP_MotorsMulticopter

#endif

  MOTOR_CLASS *motors;

  // GPS variables

  // Sometimes we need to remove the scaling for distance calcs

  float scaleLongDown;

  // Location & Navigation

  int32_t wp_bearing;

  // The location of home in relation to the copter in centi-degrees

  int32_t home_bearing;

  // distance between plane and home in cm

  int32_t home_distance;

  // distance between plane and next waypoint in cm.

  uint32_t wp_distance;

  LandStateType land_state = LandStateType_FlyToLocation; // records state of land (flying to location, descending)

  struct {

    PayloadPlaceStateType state = PayloadPlaceStateType_Calibrating_Hover_Start; // records state of place (descending, releasing, released, ...)

    uint32_t hover_start_timestamp; // milliseconds

    float hover_throttle_level;

    uint32_t descend_start_timestamp; // milliseconds

    uint32_t place_start_timestamp; // milliseconds

    float descend_throttle_level;

    float descend_start_altitude;

    float descend_max; // centimetres

  } nav_payload_place;

  // Auto

  AutoMode auto_mode; // controls which auto controller is run

  // Guided

  GuidedMode guided_mode; // controls which controller is run (pos or vel)

  // RTL

  RTLState rtl_state; // records state of rtl (initial climb, returning home, etc)

  bool rtl_state_complete; // set to true if the current state is completed

  struct {

    // NEU w/ Z element alt-above-ekf-origin unless use_terrain is true in which case Z element is alt-above-terrain

    Location_Class origin_point;

    Location_Class climb_target;

    Location_Class return_target;

    Location_Class descent_target;

    bool land;

    bool terrain_used;

  } rtl_path;

  // Circle

  bool circle_pilot_yaw_override; // true if pilot is overriding yaw

  // SIMPLE Mode

  // Used to track the orientation of the copter for Simple mode. This value is reset at each arming

  // or in SuperSimple mode when the copter leaves a 20m radius from home.

  float simple_cos_yaw;

  float simple_sin_yaw;

  int32_t super_simple_last_bearing;

  float super_simple_cos_yaw;

  float super_simple_sin_yaw;

  // Stores initial bearing when armed - initial simple bearing is modified in super simple mode so not suitable

  int32_t initial_armed_bearing;

  // Loiter control

  uint16_t loiter_time_max;        // How long we should stay in Loiter Mode for mission scripting (time in seconds)

  uint32_t loiter_time;          // How long have we been loitering - The start time in millis

  // Brake

  uint32_t brake_timeout_start;

  uint32_t brake_timeout_ms;

  // Delay the next navigation command

  int32_t nav_delay_time_max; // used for delaying the navigation commands (eg land,takeoff etc.)

  uint32_t nav_delay_time_start;

  // Flip

  Vector3f flip_orig_attitude;    // original copter attitude before flip

  // throw mode state

  struct {

    ThrowModeStage stage;

    ThrowModeStage prev_stage;

    uint32_t last_log_ms;

    bool nextmode_attempted;

    uint32_t free_fall_start_ms;  // system time free fall was detected

    float free_fall_start_velz;  // vertical velocity when free fall was detected

  } throw_state = {Throw_Disarmed, Throw_Disarmed, 0, false, 0, 0.0f};

  // Battery Sensors

  AP_BattMonitor battery;

  // FrSky telemetry support

#if FRSKY_TELEM_ENABLED == ENABLED

  AP_Frsky_Telem frsky_telemetry;

#endif

  // Variables for extended status MAVLink messages

  uint32_t control_sensors_present;

  uint32_t control_sensors_enabled;

  uint32_t control_sensors_health;

  // Altitude

  // The cm/s we are moving up or down based on filtered data - Positive = UP

  int16_t climb_rate;

  float target_rangefinder_alt; // desired altitude in cm above the ground

  int32_t baro_alt;      // barometer altitude in cm above home

  float baro_climbrate;    // barometer climbrate in cm/s

  LowPassFilterVector3f land_accel_ef_filter; // accelerations for land and crash detector tests

  // filtered pilot's throttle input used to cancel landing if throttle held high

  LowPassFilterFloat rc_throttle_control_in_filter;

  // 3D Location vectors

  // Current location of the copter (altitude is relative to home)

  Location_Class current_loc;

  // Navigation Yaw control

  // auto flight mode's yaw mode

  uint8_t auto_yaw_mode;

  // Yaw will point at this location if auto_yaw_mode is set to AUTO_YAW_ROI

  Vector3f roi_WP;

  // bearing from current location to the yaw_look_at_WP

  float yaw_look_at_WP_bearing;

  // yaw used for YAW_LOOK_AT_HEADING yaw_mode

  int32_t yaw_look_at_heading;

  // Deg/s we should turn

  int16_t yaw_look_at_heading_slew;

  // heading when in yaw_look_ahead_bearing

  float yaw_look_ahead_bearing;

  // Delay Mission Scripting Command

  int32_t condition_value; // used in condition commands (eg delay, change alt, etc.)

  uint32_t condition_start;

  // IMU variables

  // Integration time (in seconds) for the gyros (DCM algorithm)

  // Updated with the fast loop

  float G_Dt;

  // Inertial Navigation

  AP_InertialNav_NavEKF inertial_nav;

  // Attitude, Position and Waypoint navigation objects

  // To-Do: move inertial nav up or other navigation variables down here

  AC_AttitudeControl *attitude_control;

  AC_PosControl *pos_control;

  AC_WPNav *wp_nav;

  AC_Circle *circle_nav;

  // Performance monitoring

  int16_t pmTest1;

  // System Timers

  // --------------

  // Time in microseconds of main control loop

  uint32_t fast_loopTimer;

  // Counter of main loop executions. Used for performance monitoring and failsafe processing

  uint16_t mainLoop_count;

  // Loiter timer - Records how long we have been in loiter

  uint32_t rtl_loiter_start_time;

  // arm_time_ms - Records when vehicle was armed. Will be Zero if we are disarmed.

  uint32_t arm_time_ms;

  // Used to exit the roll and pitch auto trim function

  uint8_t auto_trim_counter;

  // Reference to the relay object

  AP_Relay relay;

  // handle repeated servo and relay events

  AP_ServoRelayEvents ServoRelayEvents;

  // Reference to the camera object (it uses the relay object inside it)

#if CAMERA == ENABLED

  AP_Camera camera;

#endif

  // Camera/Antenna mount tracking and stabilisation stuff

#if MOUNT == ENABLED

  // current_loc uses the baro/gps soloution for altitude rather than gps only.

  AP_Mount camera_mount;

#endif

  // AC_Fence library to reduce fly-aways

#if AC_FENCE == ENABLED

  AC_Fence  fence;

#endif

#if AC_AVOID_ENABLED == ENABLED

  AC_Avoid avoid;

#endif

  // Rally library

#if AC_RALLY == ENABLED

  AP_Rally_Copter rally;

#endif

  // RSSI 

  AP_RSSI rssi;   

  // Crop Sprayer

#if SPRAYER == ENABLED

  AC_Sprayer sprayer;

#endif

  // Parachute release

#if PARACHUTE == ENABLED

  AP_Parachute parachute;

#endif

  // Landing Gear Controller

  AP_LandingGear landinggear;

  // terrain handling

#if AP_TERRAIN_AVAILABLE && AC_TERRAIN

  AP_Terrain terrain;

#endif

  // Precision Landing

#if PRECISION_LANDING == ENABLED

  AC_PrecLand precland;

#endif

  // Pilot Input Management Library

  // Only used for Helicopter for AC3.3, to be expanded to include Multirotor

  // child class for AC3.4

#if FRAME_CONFIG == HELI_FRAME

  AC_InputManager_Heli input_manager;

#endif

  AP_ADSB adsb {ahrs};

  // avoidance of adsb enabled vehicles (normally manned vheicles)

  AP_Avoidance_Copter avoidance_adsb{ahrs, adsb};

  // use this to prevent recursion during sensor init

  bool in_mavlink_delay;

  // true if we are out of time in our event timeslice

  bool gcs_out_of_time;

  // last valid RC input time

  uint32_t last_radio_update_ms;

  // Top-level logic

  // setup the var_info table

  AP_Param param_loader;

#if FRAME_CONFIG == HELI_FRAME

  // Mode filter to reject RC Input glitches. Filter size is 5, and it draws the 4th element, so it can reject 3 low glitches,

  // and 1 high glitch. This is because any "off" glitches can be highly problematic for a helicopter running an ESC

  // governor. Even a single "off" frame can cause the rotor to slow dramatically and take a long time to restart.

  ModeFilterInt16_Size5 rotor_speed_deglitch_filter {4};

  // Tradheli flags

  struct {

    uint8_t dynamic_flight     : 1;  // 0 // true if we are moving at a significant speed (used to turn on/off leaky I terms)

    uint8_t init_targets_on_arming : 1;  // 1 // true if we have been disarmed, and need to reset rate controller targets when we arm

  } heli_flags;

  int16_t hover_roll_trim_scalar_slew;

#endif

  // ground effect detector

  struct {

    bool takeoff_expected;

    bool touchdown_expected;

    uint32_t takeoff_time_ms;

    float takeoff_alt_cm;

  } gndeffect_state;

  // set when we are upgrading parameters from 3.4

  bool upgrading_frame_params;

  static const AP_Scheduler::Task scheduler_tasks[];

  static const AP_Param::Info var_info[];

  static const struct LogStructure log_structure[];

  void compass_accumulate(void);

  void compass_cal_update(void);

  void barometer_accumulate(void);

  void perf_update(void);

  void fast_loop();

  void rc_loop();

  void throttle_loop();

  void update_mount();

  void update_trigger(void);

  void update_batt_compass(void);

  void ten_hz_logging_loop();

  void twentyfive_hz_logging();

  void three_hz_loop();

  void one_hz_loop();

  void update_GPS(void);

  void init_simple_bearing();

  void update_simple_mode(void);

  void update_super_simple_bearing(bool force_update);

  void read_AHRS(void);

  void update_altitude();

  void set_home_state(enum HomeState new_home_state);

  bool home_is_set();

  void set_auto_armed(bool b);

  void set_simple_mode(uint8_t b);

  void set_failsafe_radio(bool b);

  void set_failsafe_battery(bool b);

  void set_failsafe_gcs(bool b);

  void set_land_complete(bool b);

  void set_land_complete_maybe(bool b);

  void update_using_interlock();

  void set_motor_emergency_stop(bool b);

  float get_smoothing_gain();

  void get_pilot_desired_lean_angles(float roll_in, float pitch_in, float &roll_out, float &pitch_out, float angle_max);

  float get_pilot_desired_yaw_rate(int16_t stick_angle);

  void check_ekf_reset();

  float get_roi_yaw();

  float get_look_ahead_yaw();

  void update_throttle_hover();

  void set_throttle_takeoff();

  float get_pilot_desired_throttle(int16_t throttle_control, float thr_mid = 0.0f);

  float get_pilot_desired_climb_rate(float throttle_control);

  float get_non_takeoff_throttle();

  float get_surface_tracking_climb_rate(int16_t target_rate, float current_alt_target, float dt);

  float get_avoidance_adjusted_climbrate(float target_rate);

  void auto_takeoff_set_start_alt(void);

  void auto_takeoff_attitude_run(float target_yaw_rate);

  void set_accel_throttle_I_from_pilot_throttle();

  void rotate_body_frame_to_NE(float &x, float &y);

  void gcs_send_heartbeat(void);

  void gcs_send_deferred(void);

  void send_heartbeat(mavlink_channel_t chan);

  void send_attitude(mavlink_channel_t chan);

  void send_fence_status(mavlink_channel_t chan);

  void send_extended_status1(mavlink_channel_t chan);

  void send_location(mavlink_channel_t chan);

  void send_nav_controller_output(mavlink_channel_t chan);

  void send_simstate(mavlink_channel_t chan);

  void send_hwstatus(mavlink_channel_t chan);

  void send_vfr_hud(mavlink_channel_t chan);

  void send_current_waypoint(mavlink_channel_t chan);

  void send_rangefinder(mavlink_channel_t chan);

  void send_proximity(mavlink_channel_t chan, uint16_t count_max);

  void send_rpm(mavlink_channel_t chan);

  void rpm_update();

  void button_update();

  void init_proximity();

  void update_proximity();

  void stats_update();

  void init_beacon();

  void update_beacon();

  void send_pid_tuning(mavlink_channel_t chan);

  void gcs_send_message(enum ap_message id);

  void gcs_send_mission_item_reached_message(uint16_t mission_index);

  void gcs_data_stream_send(void);

  void gcs_check_input(void);

  void gcs_send_text(MAV_SEVERITY severity, const char *str);

  void do_erase_logs(void);

  void Log_Write_AutoTune(uint8_t axis, uint8_t tune_step, float meas_target, float meas_min, float meas_max, float new_gain_rp, float new_gain_rd, float new_gain_sp, float new_ddt);

  void Log_Write_AutoTuneDetails(float angle_cd, float rate_cds);

  void Log_Write_Current();

  void Log_Write_Optflow();

  void Log_Write_Nav_Tuning();

  void Log_Write_Control_Tuning();

  void Log_Write_Performance();

  void Log_Write_Attitude();

  void Log_Write_MotBatt();

  void Log_Write_Event(uint8_t id);

  void Log_Write_Data(uint8_t id, int32_t value);

  void Log_Write_Data(uint8_t id, uint32_t value);

  void Log_Write_Data(uint8_t id, int16_t value);

  void Log_Write_Data(uint8_t id, uint16_t value);

  void Log_Write_Data(uint8_t id, float value);

  void Log_Write_Error(uint8_t sub_system, uint8_t error_code);

  void Log_Write_Baro(void);

  void Log_Write_Parameter_Tuning(uint8_t param, float tuning_val, int16_t control_in, int16_t tune_low, int16_t tune_high);

  void Log_Write_Home_And_Origin();

  void Log_Sensor_Health();

#if FRAME_CONFIG == HELI_FRAME

  void Log_Write_Heli(void);

#endif

  void Log_Write_Precland();

  void Log_Write_GuidedTarget(uint8_t target_type, const Vector3f& pos_target, const Vector3f& vel_target);

  void Log_Write_Throw(ThrowModeStage stage, float velocity, float velocity_z, float accel, float ef_accel_z, bool throw_detect, bool attitude_ok, bool height_ok, bool position_ok);

  void Log_Write_Proximity();

  void Log_Write_Beacon();

  void Log_Write_Vehicle_Startup_Messages();

  void Log_Read(uint16_t log_num, uint16_t start_page, uint16_t end_page);

  void start_logging() ;

  void load_parameters(void);

  void convert_pid_parameters(void);

  void userhook_init();

  void userhook_FastLoop();

  void userhook_50Hz();

  void userhook_MediumLoop();

  void userhook_SlowLoop();

  void userhook_SuperSlowLoop();

  void update_home_from_EKF();

  void set_home_to_current_location_inflight();

  bool set_home_to_current_location();

  bool set_home_to_current_location_and_lock();

  bool set_home_and_lock(const Location& loc);

  bool set_home(const Location& loc);

  bool far_from_EKF_origin(const Location& loc);

  void set_system_time_from_GPS();

  void exit_mission();

  void do_RTL(void);

  bool verify_takeoff();

  bool verify_land();

  bool verify_payload_place();

  bool verify_loiter_unlimited();

  bool verify_loiter_time();

  bool verify_RTL();

  bool verify_wait_delay();

  bool verify_within_distance();

  bool verify_yaw();

  void do_take_picture();

  void log_picture();

  MAV_RESULT mavlink_compassmot(mavlink_channel_t chan);

  void delay(uint32_t ms);

  bool acro_init(bool ignore_checks);

  void acro_run();

  void get_pilot_desired_angle_rates(int16_t roll_in, int16_t pitch_in, int16_t yaw_in, float &roll_out, float &pitch_out, float &yaw_out);

  bool althold_init(bool ignore_checks);

  void althold_run();

  bool auto_init(bool ignore_checks);

  void auto_run();

  void auto_takeoff_start(const Location& dest_loc);

  void auto_takeoff_run();

  void auto_wp_start(const Vector3f& destination);

  void auto_wp_start(const Location_Class& dest_loc);

  void auto_wp_run();

  void auto_spline_run();

  void auto_land_start();

  void auto_land_start(const Vector3f& destination);

  void auto_land_run();

  void do_payload_place(const AP_Mission::Mission_Command& cmd);

  void auto_payload_place_start();

  void auto_payload_place_start(const Vector3f& destination);

  void auto_payload_place_run();

  bool auto_payload_place_run_should_run();

  void auto_payload_place_run_loiter();

  void auto_payload_place_run_descend();

  void auto_payload_place_run_release();

  void auto_rtl_start();

  void auto_rtl_run();

  void auto_circle_movetoedge_start(const Location_Class &circle_center, float radius_m);

  void auto_circle_start();

  void auto_circle_run();

  void auto_nav_guided_start();

  void auto_nav_guided_run();

  bool auto_loiter_start();

  void auto_loiter_run();

  uint8_t get_default_auto_yaw_mode(bool rtl);

  void set_auto_yaw_mode(uint8_t yaw_mode);

  void set_auto_yaw_look_at_heading(float angle_deg, float turn_rate_dps, int8_t direction, uint8_t relative_angle);

  void set_auto_yaw_roi(const Location &roi_location);

  float get_auto_heading(void);

  bool autotune_init(bool ignore_checks);

  void autotune_stop();

  bool autotune_start(bool ignore_checks);

  void autotune_run();

  void autotune_attitude_control();

  void autotune_backup_gains_and_initialise();

  void autotune_load_orig_gains();

  void autotune_load_tuned_gains();

  void autotune_load_intra_test_gains();

  void autotune_load_twitch_gains();

  void autotune_save_tuning_gains();

  void autotune_update_gcs(uint8_t message_id);

  bool autotune_roll_enabled();

  bool autotune_pitch_enabled();

  bool autotune_yaw_enabled();

  void autotune_twitching_test(float measurement, float target, float &measurement_min, float &measurement_max);

  void autotune_updating_d_up(float &tune_d, float tune_d_min, float tune_d_max, float tune_d_step_ratio, float &tune_p, float tune_p_min, float tune_p_max, float tune_p_step_ratio, float target, float measurement_min, float measurement_max);

  void autotune_updating_d_down(float &tune_d, float tune_d_min, float tune_d_step_ratio, float &tune_p, float tune_p_min, float tune_p_max, float tune_p_step_ratio, float target, float measurement_min, float measurement_max);

  void autotune_updating_p_down(float &tune_p, float tune_p_min, float tune_p_step_ratio, float target, float measurement_max);

  void autotune_updating_p_up(float &tune_p, float tune_p_max, float tune_p_step_ratio, float target, float measurement_max);

  void autotune_updating_p_up_d_down(float &tune_d, float tune_d_min, float tune_d_step_ratio, float &tune_p, float tune_p_min, float tune_p_max, float tune_p_step_ratio, float target, float measurement_min, float measurement_max);

  void autotune_twitching_measure_acceleration(float &rate_of_change, float rate_measurement, float &rate_measurement_max);

  void autotune_get_poshold_attitude(float &roll_cd, float &pitch_cd, float &yaw_cd);

  void avoidance_adsb_update(void);

#if ADVANCED_FAILSAFE == ENABLED

  void afs_fs_check(void);

#endif

  bool brake_init(bool ignore_checks);

  void brake_run();

  void brake_timeout_to_loiter_ms(uint32_t timeout_ms);

  bool circle_init(bool ignore_checks);

  void circle_run();

  bool drift_init(bool ignore_checks);

  void drift_run();

  float get_throttle_assist(float velz, float pilot_throttle_scaled);

  bool flip_init(bool ignore_checks);

  void flip_run();

  bool guided_init(bool ignore_checks);

  bool guided_takeoff_start(float final_alt_above_home);

  void guided_pos_control_start();

  void guided_vel_control_start();

  void guided_posvel_control_start();

  void guided_angle_control_start();

  bool guided_set_destination(const Vector3f& destination);

  bool guided_set_destination(const Location_Class& dest_loc);

  void guided_set_velocity(const Vector3f& velocity);

  void guided_set_destination_posvel(const Vector3f& destination, const Vector3f& velocity);

  void guided_set_angle(const Quaternion &q, float climb_rate_cms, bool use_yaw_rate, float yaw_rate_rads);

  void guided_run();

  void guided_takeoff_run();

  void guided_pos_control_run();

  void guided_vel_control_run();

  void guided_posvel_control_run();

  void guided_angle_control_run();

  void guided_set_desired_velocity_with_accel_and_fence_limits(const Vector3f& vel_des);

  void guided_limit_clear();

  void guided_limit_set(uint32_t timeout_ms, float alt_min_cm, float alt_max_cm, float horiz_max_cm);

  void guided_limit_init_time_and_pos();

  bool guided_limit_check();

  bool guided_nogps_init(bool ignore_checks);

  void guided_nogps_run();

  bool land_init(bool ignore_checks);

  void land_run();

  void land_gps_run();

  void land_nogps_run();

  int32_t land_get_alt_above_ground(void);

  void land_run_vertical_control(bool pause_descent = false);

  void land_run_horizontal_control();

  void land_do_not_use_GPS();

  void set_mode_land_with_pause(mode_reason_t reason);

  bool landing_with_GPS();

  bool loiter_init(bool ignore_checks);

  void loiter_run();

#if PRECISION_LANDING == ENABLED

  bool do_precision_loiter() const;

  void precision_loiter_xy();

  void set_precision_loiter_enabled(bool value) { _precision_loiter_enabled = value; }

  bool _precision_loiter_enabled;

#endif

  bool poshold_init(bool ignore_checks);

  void poshold_run();

  void poshold_update_pilot_lean_angle(float &lean_angle_filtered, float &lean_angle_raw);

  int16_t poshold_mix_controls(float mix_ratio, int16_t first_control, int16_t second_control);

  void poshold_update_brake_angle_from_velocity(int16_t &brake_angle, float velocity);

  void poshold_update_wind_comp_estimate();

  void poshold_get_wind_comp_lean_angles(int16_t &roll_angle, int16_t &pitch_angle);

  void poshold_roll_controller_to_pilot_override();

  void poshold_pitch_controller_to_pilot_override();

  // Throw to launch functionality

  bool throw_init(bool ignore_checks);

  void throw_run();

  bool throw_detected();

  bool throw_attitude_good();

  bool throw_height_good();

  bool throw_position_good();

  bool rtl_init(bool ignore_checks);

  void rtl_restart_without_terrain();

  void rtl_run();

  void rtl_climb_start();

  void rtl_return_start();

  void rtl_climb_return_run();

  void rtl_loiterathome_start();

  void rtl_loiterathome_run();

  void rtl_descent_start();

  void rtl_descent_run();

  void rtl_land_start();

  void rtl_land_run();

  void rtl_build_path(bool terrain_following_allowed);

  void rtl_compute_return_target(bool terrain_following_allowed);

  bool sport_init(bool ignore_checks);

  void sport_run();

  bool stabilize_init(bool ignore_checks);

  void stabilize_run();

  void crash_check();

  void parachute_check();

  void parachute_release();

  void parachute_manual_release();

  // support for AP_Avoidance custom flight mode, AVOID_ADSB

  bool avoid_adsb_init(bool ignore_checks);

  void avoid_adsb_run();

  bool avoid_adsb_set_velocity(const Vector3f& velocity_neu);

  void ekf_check();

  bool ekf_over_threshold();

  void failsafe_ekf_event();

  void failsafe_ekf_off_event(void);

  void esc_calibration_startup_check();

  void esc_calibration_passthrough();

  void esc_calibration_auto();

  bool should_disarm_on_failsafe();

  void failsafe_radio_on_event();

  void failsafe_radio_off_event();

  void failsafe_battery_event(void);

  void failsafe_gcs_check();

  void failsafe_gcs_off_event(void);

  void failsafe_terrain_check();

  void failsafe_terrain_set_status(bool data_ok);

  void failsafe_terrain_on_event();

  void set_mode_RTL_or_land_with_pause(mode_reason_t reason);

  void update_events();

  void failsafe_enable();

  void failsafe_disable();

  void fence_check();

  void fence_send_mavlink_status(mavlink_channel_t chan);

  void update_sensor_status_flags(void);

  bool set_mode(control_mode_t mode, mode_reason_t reason);

  bool gcs_set_mode(uint8_t mode) { return set_mode((control_mode_t)mode, MODE_REASON_GCS_COMMAND); }

  void update_flight_mode();

  void exit_mode(control_mode_t old_control_mode, control_mode_t new_control_mode);

  bool mode_requires_GPS(control_mode_t mode);

  bool mode_has_manual_throttle(control_mode_t mode);

  bool mode_allows_arming(control_mode_t mode, bool arming_from_gcs);

  void notify_flight_mode(control_mode_t mode);

  void heli_init();

  void check_dynamic_flight(void);

  void update_heli_control_dynamics(void);

  void heli_update_landing_swash();

  void heli_update_rotor_speed_targets();

  bool heli_acro_init(bool ignore_checks);

  void heli_acro_run();

  bool heli_stabilize_init(bool ignore_checks);

  void heli_stabilize_run();

  void read_inertia();

  bool land_complete_maybe();

  void update_land_and_crash_detectors();

  void update_land_detector();

  void update_throttle_thr_mix();

  void update_ground_effect_detector(void);

  void landinggear_update();

  void update_notify();

  void motor_test_output();

  bool mavlink_motor_test_check(mavlink_channel_t chan, bool check_rc);

  uint8_t mavlink_motor_test_start(mavlink_channel_t chan, uint8_t motor_seq, uint8_t throttle_type, uint16_t throttle_value, float timeout_sec);

  void motor_test_stop();

  void arm_motors_check();

  void auto_disarm_check();

  bool init_arm_motors(bool arming_from_gcs);

  void init_disarm_motors();

  void motors_output();

  void lost_vehicle_check();

  void run_nav_updates(void);

  void calc_distance_and_bearing();

  void calc_wp_distance();

  void calc_wp_bearing();

  void calc_home_distance_and_bearing();

  void run_autopilot();

  void perf_info_reset();

  void perf_ignore_this_loop();

  void perf_info_check_loop_time(uint32_t time_in_micros);

  uint16_t perf_info_get_num_loops();

  uint32_t perf_info_get_max_time();

  uint32_t perf_info_get_min_time();

  uint16_t perf_info_get_num_long_running();

  uint32_t perf_info_get_num_dropped();

  Vector3f pv_location_to_vector(const Location& loc);

  float pv_alt_above_origin(float alt_above_home_cm);

  float pv_alt_above_home(float alt_above_origin_cm);

  float pv_get_bearing_cd(const Vector3f &origin, const Vector3f &destination);

  float pv_get_horizontal_distance_cm(const Vector3f &origin, const Vector3f &destination);

  float pv_distance_to_home_cm(const Vector3f &destination);

  void default_dead_zones();

  void init_rc_in();

  void init_rc_out();

  void enable_motor_output();

  void read_radio();

  void set_throttle_and_failsafe(uint16_t throttle_pwm);

  void set_throttle_zero_flag(int16_t throttle_control);

  void radio_passthrough_to_motors();

  void init_barometer(bool full_calibration);

  void read_barometer(void);

  void init_rangefinder(void);

  void read_rangefinder(void);

  bool rangefinder_alt_ok();

  void init_compass();

  void init_optflow();

  void update_optical_flow(void);

  void init_precland();

  void update_precland();

  void read_battery(void);

  void read_receiver_rssi(void);

  void epm_update();

  void gripper_update();

  void terrain_update();

  void terrain_logging();

  bool terrain_use();

  void report_batt_monitor();

  void report_frame();

  void report_radio();

  void report_ins();

  void report_flight_modes();

  void report_optflow();

  void print_radio_values();

  void print_switch(uint8_t p, uint8_t m, bool b);

  void print_accel_offsets_and_scaling(void);

  void print_gyro_offsets(void);

  void report_compass();

  void print_blanks(int16_t num);

  void print_divider(void);

  void print_enabled(bool b);

  void report_version();

  void read_control_switch();

  bool check_if_auxsw_mode_used(uint8_t auxsw_mode_check);

  bool check_duplicate_auxsw(void);

  void reset_control_switch();

  uint8_t read_3pos_switch(uint8_t chan);

  void read_aux_switches();

  void init_aux_switches();

  void init_aux_switch_function(int8_t ch_option, uint8_t ch_flag);

  void do_aux_switch_function(int8_t ch_function, uint8_t ch_flag);

  void save_trim();

  void auto_trim();

  void init_ardupilot();

  void startup_INS_ground();

  bool calibrate_gyros();

  bool position_ok();

  bool ekf_position_ok();

  bool optflow_position_ok();

  void update_auto_armed();

  void check_usb_mux(void);

  bool should_log(uint32_t mask);

  void set_default_frame_class();

  void allocate_motors(void);

  uint8_t get_frame_mav_type();

  const char* get_frame_string();

  bool current_mode_has_user_takeoff(bool must_navigate);

  bool do_user_takeoff(float takeoff_alt_cm, bool must_navigate);

  void takeoff_timer_start(float alt_cm);

  void takeoff_stop();

  void takeoff_get_climb_rates(float& pilot_climb_rate, float& takeoff_climb_rate);

  void print_hit_enter();

  void tuning();

  void gcs_send_text_fmt(MAV_SEVERITY severity, const char *fmt, ...);

  bool start_command(const AP_Mission::Mission_Command& cmd);

  bool verify_command(const AP_Mission::Mission_Command& cmd);

  bool verify_command_callback(const AP_Mission::Mission_Command& cmd);

  Location_Class terrain_adjusted_location(const AP_Mission::Mission_Command& cmd) const;

  bool do_guided(const AP_Mission::Mission_Command& cmd);

  void do_takeoff(const AP_Mission::Mission_Command& cmd);

  void do_nav_wp(const AP_Mission::Mission_Command& cmd);

  void do_land(const AP_Mission::Mission_Command& cmd);

  void do_loiter_unlimited(const AP_Mission::Mission_Command& cmd);

  void do_circle(const AP_Mission::Mission_Command& cmd);

  void do_loiter_time(const AP_Mission::Mission_Command& cmd);

  void do_spline_wp(const AP_Mission::Mission_Command& cmd);

#if NAV_GUIDED == ENABLED

  void do_nav_guided_enable(const AP_Mission::Mission_Command& cmd);

  void do_guided_limits(const AP_Mission::Mission_Command& cmd);

#endif

  void do_nav_delay(const AP_Mission::Mission_Command& cmd);

  void do_wait_delay(const AP_Mission::Mission_Command& cmd);

  void do_within_distance(const AP_Mission::Mission_Command& cmd);

  void do_yaw(const AP_Mission::Mission_Command& cmd);

  void do_change_speed(const AP_Mission::Mission_Command& cmd);

  void do_set_home(const AP_Mission::Mission_Command& cmd);

  void do_roi(const AP_Mission::Mission_Command& cmd);

  void do_mount_control(const AP_Mission::Mission_Command& cmd);

#if CAMERA == ENABLED

  void do_digicam_configure(const AP_Mission::Mission_Command& cmd);

  void do_digicam_control(const AP_Mission::Mission_Command& cmd);

#endif

#if PARACHUTE == ENABLED

  void do_parachute(const AP_Mission::Mission_Command& cmd);

#endif

#if GRIPPER_ENABLED == ENABLED

  void do_gripper(const AP_Mission::Mission_Command& cmd);

#endif

  bool verify_nav_wp(const AP_Mission::Mission_Command& cmd);

  bool verify_circle(const AP_Mission::Mission_Command& cmd);

  bool verify_spline_wp(const AP_Mission::Mission_Command& cmd);

#if NAV_GUIDED == ENABLED

  bool verify_nav_guided_enable(const AP_Mission::Mission_Command& cmd);

#endif

  bool verify_nav_delay(const AP_Mission::Mission_Command& cmd);

  void auto_spline_start(const Location_Class& destination, bool stopped_at_start, AC_WPNav::spline_segment_end_type seg_end_type, const Location_Class& next_destination);

  void print_flight_mode(AP_HAL::BetterStream *port, uint8_t mode);

  void log_init(void);

  void run_cli(AP_HAL::UARTDriver *port);

  void init_capabilities(void);

  void dataflash_periodic(void);

  void accel_cal_update(void);

public:

  void mavlink_delay_cb();

  void failsafe_check();

  int8_t dump_log(uint8_t argc, const Menu::arg *argv);

  int8_t erase_logs(uint8_t argc, const Menu::arg *argv);

  int8_t select_logs(uint8_t argc, const Menu::arg *argv);

  bool print_log_menu(void);

  int8_t process_logs(uint8_t argc, const Menu::arg *argv);

  int8_t main_menu_help(uint8_t, const Menu::arg*);

  int8_t setup_mode(uint8_t argc, const Menu::arg *argv);

  int8_t setup_factory(uint8_t argc, const Menu::arg *argv);

  int8_t setup_set(uint8_t argc, const Menu::arg *argv);

  int8_t setup_show(uint8_t argc, const Menu::arg *argv);

  int8_t esc_calib(uint8_t argc, const Menu::arg *argv);

  int8_t test_mode(uint8_t argc, const Menu::arg *argv);

  int8_t test_baro(uint8_t argc, const Menu::arg *argv);

  int8_t test_compass(uint8_t argc, const Menu::arg *argv);

  int8_t test_ins(uint8_t argc, const Menu::arg *argv);

  int8_t test_optflow(uint8_t argc, const Menu::arg *argv);

  int8_t test_relay(uint8_t argc, const Menu::arg *argv);

  int8_t test_shell(uint8_t argc, const Menu::arg *argv);

  int8_t test_rangefinder(uint8_t argc, const Menu::arg *argv);

  int8_t reboot_board(uint8_t argc, const Menu::arg *argv);

};

#define MENU_FUNC(func) FUNCTOR_BIND(&copter, &Copter::func, int8_t, uint8_t, const Menu::arg *)

extern const AP_HAL::HAL& hal;

extern Copter copter;

using AP_HAL::mill

avoidance_adsb.h

#pragma once

#include <AP_Avoidance/AP_Avoidance.h>

// Provide Copter-specific implementation of avoidance. While most of

// the logic for doing the actual avoidance is present in

// AP_Avoidance, this class allows Copter to override base

// functionality - for example, not doing anything while landed.

class AP_Avoidance_Copter : public AP_Avoidance {

public:

  AP_Avoidance_Copter(AP_AHRS &ahrs, class AP_ADSB &adsb) :

    AP_Avoidance(ahrs, adsb) { }

private:

  // helper function to set modes and always succeed

  void set_mode_else_try_RTL_else_LAND(control_mode_t mode);

protected:

  // override avoidance handler

  MAV_COLLISION_ACTION handle_avoidance(const AP_Avoidance::Obstacle *obstacle, MAV_COLLISION_ACTION requested_action) override;

  // override recovery handler

  void handle_recovery(uint8_t recovery_action) override;

  // check flight mode is avoid_adsb

  bool check_flightmode(bool allow_mode_change);

  // vertical avoidance handler

  bool handle_avoidance_vertical(const AP_Avoidance::Obstacle *obstacle, bool allow_mode_change);

  // horizontal avoidance handler

  bool handle_avoidance_horizontal(const AP_Avoidance::Obstacle *obstacle, bool allow_mode_change);

  // perpendicular (3 dimensional) avoidance handler

  bool handle_avoidance_perpendicular(const AP_Avoidance::Obstacle *obstacle, bool allow_mode_change);

  // control mode before avoidance began

  control_mode_t prev_control_mode = RTL;

};

Parameters.h

#pragma once

#include <AP_Common/AP_Common.h>

// Global parameter class.

//

class Parameters {

public:

  // The version of the layout as described by the parameter enum.

  //

  // When changing the parameter enum in an incompatible fashion, this

  // value should be incremented by one.

  //

  // The increment will prevent old parameters from being used incorrectly

  // by newer code.

  //

  static const uint16_t    k_format_version = 120;

  // The parameter software_type is set up solely for ground station use

  // and identifies the software type (eg ArduPilotMega versus

  // ArduCopterMega)

  // GCS will interpret values 0-9 as ArduPilotMega. Developers may use

  // values within that range to identify different branches.

  //

  static const uint16_t    k_software_type = 10;     // 0 for APM

                                // trunk

  // Parameter identities.

  //

  // The enumeration defined here is used to ensure that every parameter

  // or parameter group has a unique ID number.

This number is used by

  // AP_Param to store and locate parameters in EEPROM.

  //

  // Note that entries without a number are assigned the next number after

  // the entry preceding them.

When adding new entries, ensure that they

  // don't overlap.

  //

  // Try to group related variables together, and assign them a set

  // range in the enumeration.

Place these groups in numerical order

  // at the end of the enumeration.

  //

  // WARNING: Care should be taken when editing this enumeration as the

  //

AP_Param load/save code depends on the values here to identify

  //

variables saved in EEPROM.

  //

  //

  enum {

    // Layout version number, always key zero.

    //

    k_param_format_version = 0,

    k_param_software_type,

    k_param_ins_old,            // *** Deprecated, remove with next eeprom number change

    k_param_ins,              // libraries/AP_InertialSensor variables

    k_param_NavEKF2_old, // deprecated - remove

    k_param_NavEKF2,

    k_param_g2, // 2nd block of parameters

    k_param_NavEKF3,

    // simulation

    k_param_sitl = 10,

    // barometer object (needed for SITL)

    k_param_barometer,

    // scheduler object (for debugging)

    k_param_scheduler,

    // relay object

    k_param_relay,

    // (old) EPM object

    k_param_epm_unused,

    // BoardConfig object

    k_param_BoardConfig,

    // GPS object

    k_param_gps,

    // Parachute object

    k_param_parachute,

    // Landing gear object

    k_param_landinggear,  // 18

    // Input Management object

    k_param_input_manager, // 19

    // Misc

    //

    k_param_log_bitmask_old = 20,     // Deprecated

    k_param_log_last_filenumber,      // *** Deprecated - remove

                        // with next eeprom number

                        // change

    k_param_toy_yaw_rate,         // deprecated - remove

    k_param_crosstrack_min_distance,

// deprecated - remove with next eeprom number change

    k_param_rssi_pin,         // unused, replaced by rssi_ library parameters

    k_param_throttle_accel_enabled,  // deprecated - remove

    k_param_wp_yaw_behavior,

    k_param_acro_trainer,

    k_param_pilot_velocity_z_max,

    k_param_circle_rate,        // deprecated - remove

    k_param_rangefinder_gain,

    k_param_ch8_option,

    k_param_arming_check_old,   // deprecated - remove

    k_param_sprayer,

    k_param_angle_max,

    k_param_gps_hdop_good,

    k_param_battery,

    k_param_fs_batt_mah,

    k_param_angle_rate_max,    // remove

    k_param_rssi_range,      // unused, replaced by rssi_ library parameters

    k_param_rc_feel_rp,

    k_param_NavEKF,        // deprecated - remove

    k_param_mission,        // mission library

    k_param_rc_13_old,

    k_param_rc_14_old,

    k_param_rally,

    k_param_poshold_brake_rate,

    k_param_poshold_brake_angle_max,

    k_param_pilot_accel_z,

    k_param_serial0_baud,     // deprecated - remove

    k_param_serial1_baud,     // deprecated - remove

    k_param_serial2_baud,     // deprecated - remove

    k_param_land_repositioning,

    k_param_rangefinder, // rangefinder object

    k_param_fs_ekf_thresh,

    k_param_terrain,

    k_param_acro_rp_expo,

    k_param_throttle_deadzone,

    k_param_optflow,

    k_param_dcmcheck_thresh,    // deprecated - remove

    k_param_log_bitmask,

    k_param_cli_enabled,

    k_param_throttle_filt,

    k_param_throttle_behavior,

    k_param_pilot_takeoff_alt, // 64

    // 65: AP_Limits Library

    k_param_limits = 65,      // deprecated - remove

    k_param_gpslock_limit,     // deprecated - remove

    k_param_geofence_limit,    // deprecated - remove

    k_param_altitude_limit,    // deprecated - remove

    k_param_fence,

    k_param_gps_glitch,      // deprecated

    k_param_baro_glitch,      // 71 - deprecated

    // AP_ADSB Library

    k_param_adsb,         // 72

    k_param_notify,        // 73

    // 74: precision landing object

    k_param_precland = 74,

    //

    // 75: Singlecopter, CoaxCopter

    //

    k_param_single_servo_1 = 75,  // remove

    k_param_single_servo_2,    // remove

    k_param_single_servo_3,    // remove

    k_param_single_servo_4,    // 78 - remove

    //

    // 80: Heli

    //

    k_param_heli_servo_1 = 80, // remove

    k_param_heli_servo_2,   // remove

    k_param_heli_servo_3,   // remove

    k_param_heli_servo_4,   // remove

    k_param_heli_pitch_ff,   // remove

    k_param_heli_roll_ff,   // remove

    k_param_heli_yaw_ff,    // remove

    k_param_heli_stab_col_min, // remove

    k_param_heli_stab_col_max, // remove

    k_param_heli_servo_rsc,  // 89 = full! - remove

    //

    // 90: misc2

    //

    k_param_motors = 90,

    k_param_disarm_delay,

    k_param_fs_crash_check,

    k_param_throw_motor_start,

    k_param_terrain_follow,  // 94

    k_param_avoid,

    k_param_avoidance_adsb,

    // 97: RSSI

    k_param_rssi = 97,

    //

    // 100: Inertial Nav

    //

    k_param_inertial_nav = 100, // deprecated

    k_param_wp_nav,

    k_param_attitude_control,

    k_param_pos_control,

    k_param_circle_nav,  // 104

    // 110: Telemetry control

    //

    k_param_gcs0 = 110,

    k_param_gcs1,

    k_param_sysid_this_mav,

    k_param_sysid_my_gcs,

    k_param_serial1_baud_old, // deprecated

    k_param_telem_delay,

    k_param_gcs2,

    k_param_serial2_baud_old, // deprecated

    k_param_serial2_protocol, // deprecated

    k_param_serial_manager,

    k_param_ch9_option,

    k_param_ch10_option,

    k_param_ch11_option,

    k_param_ch12_option,

    k_param_takeoff_trigger_dz,

    k_param_gcs3,

    k_param_gcs_pid_mask,  // 126

    //

    // 135 : reserved for Solo until features merged with master

    //

    k_param_rtl_speed_cms = 135,

    k_param_fs_batt_curr_rtl,

    k_param_rtl_cone_slope, // 137

    //

    // 140: Sensor parameters

    //

    k_param_imu = 140, // deprecated - can be deleted

    k_param_battery_monitoring = 141, // deprecated - can be deleted

    k_param_volt_div_ratio, // deprecated - can be deleted

    k_param_curr_amp_per_volt, // deprecated - can be deleted

    k_param_input_voltage, // deprecated - can be deleted

    k_param_pack_capacity, // deprecated - can be deleted

    k_param_compass_enabled,

    k_param_compass,

    k_param_rangefinder_enabled_old, // deprecated

    k_param_frame_type,

    k_param_optflow_enabled,  // deprecated

    k_param_fs_batt_voltage,

    k_param_ch7_option,

    k_param_auto_slew_rate,  // deprecated - can be deleted

    k_param_rangefinder_type_old,  // deprecated

    k_param_super_simple = 155,

    k_param_axis_enabled = 157, // deprecated - remove with next eeprom number change

    k_param_copter_leds_mode, // deprecated - remove with next eeprom number change

    k_param_ahrs, // AHRS group // 159

    //

    // 160: Navigation parameters

    //

    k_param_rtl_altitude = 160,

    k_param_crosstrack_gain,

// deprecated - remove with next eeprom number change

    k_param_rtl_loiter_time,

    k_param_rtl_alt_final,

    k_param_tilt_comp,

//164

deprecated - remove with next eeprom number change

    //

    // Camera and mount parameters

    //

    k_param_camera = 165,

    k_param_camera_mount,

    k_param_camera_mount2,   // deprecated

    //

    // Batery monitoring parameters

    //

    k_param_battery_volt_pin = 168, // deprecated - can be deleted

    k_param_battery_curr_pin, // 169 deprecated - can be deleted

    //

    // 170: Radio settings

    //

    k_param_rc_1_old = 170,

    k_param_rc_2_old,

    k_param_rc_3_old,

    k_param_rc_4_old,

    k_param_rc_5_old,

    k_param_rc_6_old,

    k_param_rc_7_old,

    k_param_rc_8_old,

    k_param_rc_10_old,

    k_param_rc_11_old,

    k_param_throttle_min,     // remove

    k_param_throttle_max,     // remove

    k_param_failsafe_throttle,

    k_param_throttle_fs_action,  // remove

    k_param_failsafe_throttle_value,

    k_param_throttle_trim,     // remove

    k_param_esc_calibrate,

    k_param_radio_tuning,

    k_param_radio_tuning_high,

    k_param_radio_tuning_low,

    k_param_rc_speed = 192,

    k_param_failsafe_battery_enabled,

    k_param_throttle_mid,     // remove

    k_param_failsafe_gps_enabled, // remove

    k_param_rc_9_old,

    k_param_rc_12_old,

    k_param_failsafe_gcs,

    k_param_rcmap, // 199

    //

    // 200: flight modes

    //

    k_param_flight_mode1 = 200,

    k_param_flight_mode2,

    k_param_flight_mode3,

    k_param_flight_mode4,

    k_param_flight_mode5,

    k_param_flight_mode6,

    k_param_simple_modes,

    //

    // 210: Waypoint data

    //

    k_param_waypoint_mode = 210, // remove

    k_param_command_total,   // remove

    k_param_command_index,   // remove

    k_param_command_nav_index, // remove

    k_param_waypoint_radius,  // remove

    k_param_circle_radius,   // remove

    k_param_waypoint_speed_max, // remove

    k_param_land_speed,

    k_param_auto_velocity_z_min, // remove

    k_param_auto_velocity_z_max, // remove - 219

    k_param_land_speed_high,

    //

    // 220: PI/D Controllers

    //

    k_param_acro_rp_p = 221,

    k_param_axis_lock_p,  // remove

    k_param_pid_rate_roll,   // remove

    k_param_pid_rate_pitch,  // remove

    k_param_pid_rate_yaw,   // remove

    k_param_p_stabilize_roll, // remove

    k_param_p_stabilize_pitch, // remove

    k_param_p_stabilize_yaw,  // remove

    k_param_p_pos_xy,

    k_param_p_loiter_lon,   // remove

    k_param_pid_loiter_rate_lat,  // remove

    k_param_pid_loiter_rate_lon,  // remove

    k_param_pid_nav_lat,    // remove

    k_param_pid_nav_lon,    // remove

    k_param_p_alt_hold,

    k_param_p_vel_z,

    k_param_pid_optflow_roll,   // remove

    k_param_pid_optflow_pitch,   // remove

    k_param_acro_balance_roll_old, // remove

    k_param_acro_balance_pitch_old, // remove

    k_param_pid_accel_z,

    k_param_acro_balance_roll,

    k_param_acro_balance_pitch,

    k_param_acro_yaw_p,

    k_param_autotune_axis_bitmask,

    k_param_autotune_aggressiveness,

    k_param_pi_vel_xy,

    k_param_fs_ekf_action,

    k_param_rtl_climb_min,

    k_param_rpm_sensor,

    k_param_autotune_min_d, // 251

    k_param_arming, // 252 - AP_Arming

    k_param_DataFlash = 253, // 253 - Logging Group

    // 254,255: reserved

    // the k_param_* space is 9-bits in size

    // 511: reserved

  };

  AP_Int16    format_version;

  AP_Int8    software_type;

  // Telemetry control

  //

  AP_Int16    sysid_this_mav;

  AP_Int16    sysid_my_gcs;

  AP_Int8    telem_delay;

#if CLI_ENABLED == ENABLED

  AP_Int8    cli_enabled;

#endif

  AP_Float    throttle_filt;

  AP_Int16    throttle_behavior;

  AP_Int16    takeoff_trigger_dz;

  AP_Float    pilot_takeoff_alt;

  AP_Int16    rtl_altitude;

  AP_Int16    rtl_speed_cms;

  AP_Float    rtl_cone_slope;

  AP_Float    rangefinder_gain;

  AP_Int8    failsafe_battery_enabled; // battery failsafe enabled

  AP_Float    fs_batt_voltage;      // battery voltage below which failsafe will be triggered

  AP_Float    fs_batt_mah;        // battery capacity (in mah) below which failsafe will be triggered

  AP_Int8    failsafe_gcs;       // ground station failsafe behavior

  AP_Int16    gps_hdop_good;       // GPS Hdop value at or below this value represent a good position

  AP_Int8    compass_enabled;

  AP_Int8    super_simple;

  AP_Int16    rtl_alt_final;

  AP_Int16    rtl_climb_min;       // rtl minimum climb in cm

  AP_Int8    wp_yaw_behavior;      // controls how the autopilot controls yaw during missions

  AP_Int8    rc_feel_rp;        // controls vehicle response to user input with 0 being extremely soft and 100 begin extremely crisp

  AP_Int16    poshold_brake_rate;    // PosHold flight mode's rotation rate during braking in deg/sec

  AP_Int16    poshold_brake_angle_max;  // PosHold flight mode's max lean angle during braking in centi-degrees

  // Waypoints

  //

  AP_Int32    rtl_loiter_time;

  AP_Int16    land_speed;

  AP_Int16    land_speed_high;

  AP_Int16    pilot_velocity_z_max;    // maximum vertical velocity the pilot may request

  AP_Int16    pilot_accel_z;       // vertical acceleration the pilot may request

  // Throttle

  //

  AP_Int8    failsafe_throttle;

  AP_Int16    failsafe_throttle_value;

  AP_Int16    throttle_deadzone;

  // Flight modes

  //

  AP_Int8    flight_mode1;

  AP_Int8    flight_mode2;

  AP_Int8    flight_mode3;

  AP_Int8    flight_mode4;

  AP_Int8    flight_mode5;

  AP_Int8    flight_mode6;

  AP_Int8    simple_modes;

  // Misc

  //

  AP_Int32    log_bitmask;

  AP_Int8    esc_calibrate;

  AP_Int8    radio_tuning;

  AP_Int16    radio_tuning_high;

  AP_Int16    radio_tuning_low;

  AP_Int8    frame_type;

  AP_Int8    ch7_option;

  AP_Int8    ch8_option;

  AP_Int8    ch9_option;

  AP_Int8    ch10_option;

  AP_Int8    ch11_option;

  AP_Int8    ch12_option;

  AP_Int8    disarm_delay;

  AP_Int8    land_repositioning;

  AP_Int8    fs_ekf_action;

  AP_Int8    fs_crash_check;

  AP_Float    fs_ekf_thresh;

  AP_Int16    gcs_pid_mask;

  AP_Int8    throw_motor_start;

  AP_Int8    terrain_follow;

  AP_Int16        rc_speed; // speed of fast RC Channels in Hz

  // Acro parameters

  AP_Float        acro_rp_p;

  AP_Float        acro_yaw_p;

  AP_Float        acro_balance_roll;

  AP_Float        acro_balance_pitch;

  AP_Int8        acro_trainer;

  AP_Float        acro_rp_expo;

  // PI/D controllers

  AC_PI_2D        pi_vel_xy;

  AC_P          p_vel_z;

  AC_PID         pid_accel_z;

  AC_P          p_pos_xy;

  AC_P          p_alt_hold;

  // Autotune

  AP_Int8        autotune_axis_bitmask;

  AP_Float        autotune_aggressiveness;

  AP_Float        autotune_min_d;

  // Note: keep initializers here in the same order as they are declared

  // above.

  Parameters() :

    // PID controller

  initial P

   initial I    initial D   initial imax    initial filt hz  pid rate

    //---------------------------------------------------------------------------------------------------------------------------------

    pi_vel_xy       (VEL_XY_P,    VEL_XY_I,            VEL_XY_IMAX,    VEL_XY_FILT_HZ,  WPNAV_LOITER_UPDATE_TIME),

    p_vel_z        (VEL_Z_P),

    pid_accel_z      (ACCEL_Z_P,   ACCEL_Z_I,    ACCEL_Z_D,   ACCEL_Z_IMAX,   ACCEL_Z_FILT_HZ,  MAIN_LOOP_SECONDS),

    // P controller

    initial P

    //----------------------------------------------------------------------

    p_pos_xy        (POS_XY_P),

    p_alt_hold       (ALT_HOLD_P)

  {

  }

};

/*

 2nd block of parameters, to avoid going past 256 top level keys

 */

class ParametersG2 {

public:

  ParametersG2(void);

  // var_info for holding Parameter information

  static const struct AP_Param::GroupInfo var_info[];

  // altitude at which nav control can start in takeoff

  AP_Float wp_navalt_min;

  // button checking

  AP_Button button;

  // vehicle statistics

  AP_Stats stats;

#if GRIPPER_ENABLED

  AP_Gripper gripper;

#endif

  // Throw mode parameters

  AP_Int8 throw_nextmode;

  AP_Int8 throw_type;

  // ground effect compensation enable/disable

  AP_Int8 gndeffect_comp_enabled;

  // beacon (non-GPS positioning) library

  AP_Beacon beacon;

#if PROXIMITY_ENABLED == ENABLED

  // proximity (aka object avoidance) library

  AP_Proximity proximity;

#endif

  // whether to enforce acceptance of packets only from sysid_my_gcs

  AP_Int8 sysid_enforce;

#if ADVANCED_FAILSAFE == ENABLED

  // advanced failsafe library

  AP_AdvancedFailsafe_Copter afs;

#endif

  // developer options

  AP_Int32 dev_options;

  // acro exponent parameters

  AP_Float acro_y_expo;

  AP_Float acro_thr_mid;

  // frame class

  AP_Int8 frame_class;

  // RC input channels

  RC_Channels rc_channels;

  // control over servo output ranges

  SRV_Channels servo_channels;

};

extern const AP_Param::Info    var_info[];

afs_copter.h

/*

  This program is free software: you can redistribute it and/or modify

  it under the terms of the GNU General Public License as published by

  the Free Software Foundation, either version 3 of the License, or

  (at your option) any later version.

  This program is distributed in the hope that it will be useful,

  but WITHOUT ANY WARRANTY; without even the implied warranty of

  MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the

  GNU General Public License for more details.

  You should have received a copy of the GNU General Public License

  along with this program. If not, see <http://www.gnu.org/licenses/>.

 */

#pragma once

/*

 advanced failsafe support for copter

 */

#if ADVANCED_FAILSAFE == ENABLED

#include <AP_AdvancedFailsafe/AP_AdvancedFailsafe.h>

/*

 a plane specific AP_AdvancedFailsafe class

 */

class AP_AdvancedFailsafe_Copter : public AP_AdvancedFailsafe

{

public:

  AP_AdvancedFailsafe_Copter(AP_Mission &_mission, AP_Baro &_baro, const AP_GPS &_gps, const RCMapper &_rcmap);

  // called to set all outputs to termination state

  void terminate_vehicle(void);

protected:

  // setup failsafe values for if FMU firmware stops running

  void setup_IO_failsafe(void);

  // return the AFS mapped control mode

  enum control_mode afs_mode(void);

};

#endif // ADVANCED_FAILSAFE

AP_Arming.h

#pragma once

#include <AP_Arming/AP_Arming.h>

class AP_Arming_Copter : public AP_Arming

{

public:

  AP_Arming_Copter(const AP_AHRS_NavEKF &ahrs_ref, const AP_Baro &baro, Compass &compass,

           const AP_BattMonitor &battery, const AP_InertialNav_NavEKF &inav,

           const AP_InertialSensor &ins) :

    AP_Arming(ahrs_ref, baro, compass, battery),

    _inav(inav),

    _ins(ins),

    _ahrs_navekf(ahrs_ref)

    {

  }

  void update(void);

  bool all_checks_passing(bool arming_from_gcs);

  void pre_arm_rc_checks(bool display_failure);

protected:

  bool pre_arm_checks(bool display_failure) override;

  bool pre_arm_gps_checks(bool display_failure);

  bool pre_arm_ekf_attitude_check();

  bool pre_arm_terrain_check(bool display_failure);

  bool pre_arm_proximity_check(bool display_failure);

  bool arm_checks(bool display_failure, bool arming_from_gcs);

  // NOTE! the following check functions *DO* call into AP_Arming:

  bool ins_checks(bool display_failure) override;

  bool compass_checks(bool display_failure) override;

  bool gps_checks(bool display_failure) override;

  // NOTE! the following check functions *DO NOT* call into AP_Arming!

  bool fence_checks(bool display_failure);

  bool board_voltage_checks(bool display_failure);

  bool parameter_checks(bool display_failure);

  bool motor_checks(bool display_failure);

  bool pilot_throttle_checks(bool display_failure);

  bool barometer_checks(bool display_failure);

  bool rc_calibration_checks(bool display_failure);

  void set_pre_arm_check(bool b);

  void set_pre_arm_rc_check(bool b);

  enum HomeState home_status() const override;

private:

  void gcs_send_text(MAV_SEVERITY severity, const char *str);

  const AP_InertialNav_NavEKF &_inav;

  const AP_InertialSensor &_ins;

  const AP_AHRS_NavEKF &_ahrs_navekf;

};

AP_Rally.h

#pragma once

#include <AP_Rally/AP_Rally.h>

#include <AP_AHRS/AP_AHRS.h>

class AP_Rally_Copter : public AP_Rally

{

public:

  // constructor

  AP_Rally_Copter(AP_AHRS &ahrs) : AP_Rally(ahrs) {};

private:

  bool is_valid(const Location &rally_point) const override;

};

GCS_Mavlink.h

#pragma once

#include <GCS_MAVLink/GCS.h>

// default sensors are present and healthy: gyro, accelerometer, barometer, rate_control, attitude_stabilization, yaw_position, altitude control, x/y position control, motor_control

#define MAVLINK_SENSOR_PRESENT_DEFAULT (MAV_SYS_STATUS_SENSOR_3D_GYRO | MAV_SYS_STATUS_SENSOR_3D_ACCEL | MAV_SYS_STATUS_SENSOR_ABSOLUTE_PRESSURE | MAV_SYS_STATUS_SENSOR_ANGULAR_RATE_CONTROL | MAV_SYS_STATUS_SENSOR_ATTITUDE_STABILIZATION | MAV_SYS_STATUS_SENSOR_YAW_POSITION | MAV_SYS_STATUS_SENSOR_Z_ALTITUDE_CONTROL | MAV_SYS_STATUS_SENSOR_XY_POSITION_CONTROL | MAV_SYS_STATUS_SENSOR_MOTOR_OUTPUTS | MAV_SYS_STATUS_AHRS)

class GCS_MAVLINK_Copter : public GCS_MAVLINK

{

public:

  void data_stream_send(void) override;

protected:

  uint32_t telem_delay() const override;

  bool accept_packet(const mavlink_status_t &status, mavlink_message_t &msg) override;

private:

  void handleMessage(mavlink_message_t * msg) override;

  bool handle_guided_request(AP_Mission::Mission_Command &cmd) override;

  void handle_change_alt_request(AP_Mission::Mission_Command &cmd) override;

  bool try_send_message(enum ap_message id) override;

  void packetReceived(const mavlink_status_t &status,

            mavlink_message_t &msg) override;

};

config.h

//

#pragma once

//////////////////////////////////////////////////////////////////////////////

//////////////////////////////////////////////////////////////////////////////

//

// WARNING WARNING WARNING WARNING WARNING WARNING WARNING WARNING WARNING

//

// DO NOT EDIT this file to adjust your configuration. Create your own

// APM_Config.h and use APM_Config.h.example as a reference.

//

// WARNING WARNING WARNING WARNING WARNING WARNING WARNING WARNING WARNING

///

//////////////////////////////////////////////////////////////////////////////

//////////////////////////////////////////////////////////////////////////////

//

// Default and automatic configuration details.

//

// Notes for maintainers:

//

// - Try to keep this file organised in the same order as APM_Config.h.example

//

#include "defines.h"

///

/// DO NOT EDIT THIS INCLUDE - if you want to make a local change, make that

/// change in your local copy of APM_Config.h.

///

#include "APM_Config.h"

//////////////////////////////////////////////////////////////////////////////

//////////////////////////////////////////////////////////////////////////////

// HARDWARE CONFIGURATION AND CONNECTIONS

//////////////////////////////////////////////////////////////////////////////

//////////////////////////////////////////////////////////////////////////////

#ifndef CONFIG_HAL_BOARD

#error CONFIG_HAL_BOARD must be defined to build ArduCopter

#endif

//////////////////////////////////////////////////////////////////////////////

// HIL_MODE                OPTIONAL

#ifndef HIL_MODE

 #define HIL_MODE    HIL_MODE_DISABLED

#endif

#define MAGNETOMETER ENABLED

// run at 400Hz on all systems

# define MAIN_LOOP_RATE  400

# define MAIN_LOOP_SECONDS 0.0025f

# define MAIN_LOOP_MICROS 2500

#ifndef ARMING_DELAY_SEC

  # define ARMING_DELAY_SEC 2.0f

#endif

//////////////////////////////////////////////////////////////////////////////

// FRAME_CONFIG

//

#ifndef FRAME_CONFIG

 # define FRAME_CONFIG MULTICOPTER_FRAME

#endif

/////////////////////////////////////////////////////////////////////////////////

// TradHeli defaults

#if FRAME_CONFIG == HELI_FRAME

 # define RC_FAST_SPEED            125

 # define WP_YAW_BEHAVIOR_DEFAULT       WP_YAW_BEHAVIOR_LOOK_AHEAD

 # define THR_MIN_DEFAULT           0

 # define AUTOTUNE_ENABLED          DISABLED

#endif

//////////////////////////////////////////////////////////////////////////////

// PWM control

// default RC speed in Hz

#ifndef RC_FAST_SPEED

  # define RC_FAST_SPEED 490

#endif

//////////////////////////////////////////////////////////////////////////////

// Rangefinder

//

#ifndef RANGEFINDER_ENABLED

 # define RANGEFINDER_ENABLED ENABLED

#endif

#ifndef RANGEFINDER_HEALTH_MAX

 # define RANGEFINDER_HEALTH_MAX 3     // number of good reads that indicates a healthy rangefinder

#endif

#ifndef RANGEFINDER_GAIN_DEFAULT

 # define RANGEFINDER_GAIN_DEFAULT 0.8f  // gain for controlling how quickly rangefinder range adjusts target altitude (lower means slower reaction)

#endif

#ifndef THR_SURFACE_TRACKING_VELZ_MAX

 # define THR_SURFACE_TRACKING_VELZ_MAX 150 // max vertical speed change while surface tracking with rangefinder

#endif

#ifndef RANGEFINDER_TIMEOUT_MS

 # define RANGEFINDER_TIMEOUT_MS 1000   // desired rangefinder alt will reset to current rangefinder alt after this many milliseconds without a good rangefinder alt

#endif

#ifndef RANGEFINDER_WPNAV_FILT_HZ

 # define RANGEFINDER_WPNAV_FILT_HZ 0.25f // filter frequency for rangefinder altitude provided to waypoint navigation class

#endif

#ifndef RANGEFINDER_TILT_CORRECTION    // by disable tilt correction for use of range finder data by EKF

 # define RANGEFINDER_TILT_CORRECTION ENABLED

#endif

#ifndef RANGEFINDER_GLITCH_ALT_CM

 # define RANGEFINDER_GLITCH_ALT_CM 200   // amount of rangefinder change to be considered a glitch

#endif

#ifndef RANGEFINDER_GLITCH_NUM_SAMPLES

 # define RANGEFINDER_GLITCH_NUM_SAMPLES 3 // number of rangefinder glitches in a row to take new reading

#endif

//////////////////////////////////////////////////////////////////////////////

// Proximity sensor

//

#ifndef PROXIMITY_ENABLED

 # define PROXIMITY_ENABLED ENABLED

#endif

#ifndef MAV_SYSTEM_ID

 # define MAV_SYSTEM_ID     1

#endif

//////////////////////////////////////////////////////////////////////////////

// Battery monitoring

//

#ifndef FS_BATT_VOLTAGE_DEFAULT

 # define FS_BATT_VOLTAGE_DEFAULT   10.5f   // default battery voltage below which failsafe will be triggered

#endif

#ifndef FS_BATT_MAH_DEFAULT

 # define FS_BATT_MAH_DEFAULT      0    // default battery capacity (in mah) below which failsafe will be triggered

#endif

#ifndef BOARD_VOLTAGE_MIN

 # define BOARD_VOLTAGE_MIN      4.3f    // min board voltage in volts for pre-arm checks

#endif

#ifndef BOARD_VOLTAGE_MAX

 # define BOARD_VOLTAGE_MAX      5.8f    // max board voltage in volts for pre-arm checks

#endif

// prearm GPS hdop check

#ifndef GPS_HDOP_GOOD_DEFAULT

 # define GPS_HDOP_GOOD_DEFAULT    140  // minimum hdop that represents a good position. used during pre-arm checks if fence is enabled

#endif

// GCS failsafe

#ifndef FS_GCS

 # define FS_GCS            DISABLED

#endif

#ifndef FS_GCS_TIMEOUT_MS

 # define FS_GCS_TIMEOUT_MS      5000  // gcs failsafe triggers after 5 seconds with no GCS heartbeat

#endif

// Radio failsafe while using RC_override

#ifndef FS_RADIO_RC_OVERRIDE_TIMEOUT_MS

 # define FS_RADIO_RC_OVERRIDE_TIMEOUT_MS 1000  // RC Radio failsafe triggers after 1 second while using RC_override from ground station

#endif

// Radio failsafe

#ifndef FS_RADIO_TIMEOUT_MS

 #define FS_RADIO_TIMEOUT_MS      500  // RC Radio Failsafe triggers after 500 miliseconds with No RC Input

#endif

// missing terrain data failsafe

#ifndef FS_TERRAIN_TIMEOUT_MS

 #define FS_TERRAIN_TIMEOUT_MS     5000  // 5 seconds of missing terrain data will trigger failsafe (RTL)

#endif

#ifndef PREARM_DISPLAY_PERIOD

# define PREARM_DISPLAY_PERIOD 30

#endif

// pre-arm baro vs inertial nav max alt disparity

#ifndef PREARM_MAX_ALT_DISPARITY_CM

 # define PREARM_MAX_ALT_DISPARITY_CM   100  // barometer and inertial nav altitude must be within this many centimeters

#endif

//////////////////////////////////////////////////////////////////////////////

// EKF Failsafe

#ifndef FS_EKF_ACTION_DEFAULT

 # define FS_EKF_ACTION_DEFAULT    FS_EKF_ACTION_LAND // EKF failsafe triggers land by default

#endif

#ifndef FS_EKF_THRESHOLD_DEFAULT

 # define FS_EKF_THRESHOLD_DEFAULT   0.8f  // EKF failsafe's default compass and velocity variance threshold above which the EKF failsafe will be triggered

#endif

#ifndef EKF_ORIGIN_MAX_DIST_M

 # define EKF_ORIGIN_MAX_DIST_M    50000 // EKF origin and waypoints (including home) must be within 50km

#endif

//////////////////////////////////////////////////////////////////////////////

// MAGNETOMETER

#ifndef MAGNETOMETER

 # define MAGNETOMETER         ENABLED

#endif

#ifndef COMPASS_CAL_STICK_GESTURE_TIME

 #define COMPASS_CAL_STICK_GESTURE_TIME 2.0f // 2 seconds

#endif

#ifndef COMPASS_CAL_STICK_DELAY

 #define COMPASS_CAL_STICK_DELAY 5.0f

#endif

//////////////////////////////////////////////////////////////////////////////

// OPTICAL_FLOW

#ifndef OPTFLOW

 # define OPTFLOW   ENABLED

#endif

//////////////////////////////////////////////////////////////////////////////

// Auto Tuning

#ifndef AUTOTUNE_ENABLED

 # define AUTOTUNE_ENABLED ENABLED

#endif

//////////////////////////////////////////////////////////////////////////////

// Crop Sprayer

#ifndef SPRAYER

 # define SPRAYER ENABLED

#endif

//////////////////////////////////////////////////////////////////////////////

// Precision Landing with companion computer or IRLock sensor

#ifndef PRECISION_LANDING

 # define PRECISION_LANDING ENABLED

#endif

//////////////////////////////////////////////////////////////////////////////

//

gripper

#ifndef GRIPPER_ENABLED

 # define GRIPPER_ENABLED ENABLED

#endif

//////////////////////////////////////////////////////////////////////////////

// Parachute release

#ifndef PARACHUTE

 # define PARACHUTE ENABLED

#endif

//////////////////////////////////////////////////////////////////////////////

// ADSB support

#ifndef ADSB_ENABLED

# define ADSB_ENABLED ENABLED

#endif

//////////////////////////////////////////////////////////////////////////////

// Nav-Guided - allows external nav computer to control vehicle

#ifndef NAV_GUIDED

 # define NAV_GUIDED  ENABLED

#endif

//////////////////////////////////////////////////////////////////////////////

// RADIO CONFIGURATION

//////////////////////////////////////////////////////////////////////////////

//////////////////////////////////////////////////////////////////////////////

//////////////////////////////////////////////////////////////////////////////

// FLIGHT_MODE

//

#ifndef FLIGHT_MODE_1

 # define FLIGHT_MODE_1         STABILIZE

#endif

#ifndef FLIGHT_MODE_2

 # define FLIGHT_MODE_2         STABILIZE

#endif

#ifndef FLIGHT_MODE_3

 # define FLIGHT_MODE_3         STABILIZE

#endif

#ifndef FLIGHT_MODE_4

 # define FLIGHT_MODE_4         STABILIZE

#endif

#ifndef FLIGHT_MODE_5

 # define FLIGHT_MODE_5         STABILIZE

#endif

#ifndef FLIGHT_MODE_6

 # define FLIGHT_MODE_6         STABILIZE

#endif

//////////////////////////////////////////////////////////////////////////////

// Throttle Failsafe

//

#ifndef FS_THR_VALUE_DEFAULT

 # define FS_THR_VALUE_DEFAULT      975

#endif

//////////////////////////////////////////////////////////////////////////////

// Takeoff

//

#ifndef PILOT_TKOFF_ALT_DEFAULT

 # define PILOT_TKOFF_ALT_DEFAULT     0  // default final alt above home for pilot initiated takeoff

#endif

//////////////////////////////////////////////////////////////////////////////

// Landing

//

#ifndef LAND_SPEED

 # define LAND_SPEED  50     // the descent speed for the final stage of landing in cm/s

#endif

#ifndef LAND_START_ALT

 # define LAND_START_ALT 1000    // altitude in cm where land controller switches to slow rate of descent

#endif

#ifndef LAND_REPOSITION_DEFAULT

 # define LAND_REPOSITION_DEFAULT 1 // by default the pilot can override roll/pitch during landing

#endif

#ifndef LAND_WITH_DELAY_MS

 # define LAND_WITH_DELAY_MS    4000  // default delay (in milliseconds) when a land-with-delay is triggered during a failsafe event

#endif

#ifndef LAND_CANCEL_TRIGGER_THR

 # define LAND_CANCEL_TRIGGER_THR 700  // land is cancelled by input throttle above 700

#endif

#ifndef LAND_RANGEFINDER_MIN_ALT_CM

#define LAND_RANGEFINDER_MIN_ALT_CM 200

#endif

//////////////////////////////////////////////////////////////////////////////

// Landing Detector

//

#ifndef LAND_DETECTOR_TRIGGER_SEC

 # define LAND_DETECTOR_TRIGGER_SEC    1.0f  // number of seconds to detect a landing

#endif

#ifndef LAND_DETECTOR_MAYBE_TRIGGER_SEC

 # define LAND_DETECTOR_MAYBE_TRIGGER_SEC 0.2f  // number of seconds that means we might be landed (used to reset horizontal position targets to prevent tipping over)

#endif

#ifndef LAND_DETECTOR_ACCEL_LPF_CUTOFF

# define LAND_DETECTOR_ACCEL_LPF_CUTOFF  1.0f  // frequency cutoff of land detector accelerometer filter

#endif

#ifndef LAND_DETECTOR_ACCEL_MAX

# define LAND_DETECTOR_ACCEL_MAX      1.0f  // vehicle acceleration must be under 1m/s/s

#endif

//////////////////////////////////////////////////////////////////////////////

// CAMERA TRIGGER AND CONTROL

//

#ifndef CAMERA

 # define CAMERA    ENABLED

#endif

//////////////////////////////////////////////////////////////////////////////

// MOUNT (ANTENNA OR CAMERA)

//

#ifndef MOUNT

 # define MOUNT    ENABLED

#endif

//////////////////////////////////////////////////////////////////////////////

// Flight mode definitions

//

// Acro Mode

#ifndef ACRO_RP_P

 # define ACRO_RP_P        4.5f

#endif

#ifndef ACRO_YAW_P

 # define ACRO_YAW_P        4.5f

#endif

#ifndef ACRO_LEVEL_MAX_ANGLE

 # define ACRO_LEVEL_MAX_ANGLE   3000

#endif

#ifndef ACRO_BALANCE_ROLL

 #define ACRO_BALANCE_ROLL     1.0f

#endif

#ifndef ACRO_BALANCE_PITCH

 #define ACRO_BALANCE_PITCH    1.0f

#endif

#ifndef ACRO_RP_EXPO_DEFAULT

 #define ACRO_RP_EXPO_DEFAULT   0.3f

#endif

#ifndef ACRO_Y_EXPO_DEFAULT

 #define ACRO_Y_EXPO_DEFAULT    0.0f

#endif

#ifndef ACRO_THR_MID_DEFAULT

 #define ACRO_THR_MID_DEFAULT   0.0f

#endif

// RTL Mode

#ifndef RTL_ALT_FINAL

 # define RTL_ALT_FINAL      0   // the altitude the vehicle will move to as the final stage of Returning to Launch. Set to zero to land.

#endif

#ifndef RTL_ALT

 # define RTL_ALT

  1500  // default alt to return to home in cm, 0 = Maintain current altitude

#endif

#ifndef RTL_ALT_MIN

 # define RTL_ALT_MIN       200  // min height above ground for RTL (i.e 2m)

#endif

#ifndef RTL_CLIMB_MIN_DEFAULT

 # define RTL_CLIMB_MIN_DEFAULT  0   // vehicle will always climb this many cm as first stage of RTL

#endif

#ifndef RTL_ABS_MIN_CLIMB

 # define RTL_ABS_MIN_CLIMB    250  // absolute minimum initial climb

#endif

#ifndef RTL_CONE_SLOPE_DEFAULT

 # define RTL_CONE_SLOPE_DEFAULT  3.0f  // slope of RTL cone (height / distance). 0 = No cone

#endif

#ifndef RTL_MIN_CONE_SLOPE

 # define RTL_MIN_CONE_SLOPE    0.5f  // minimum slope of cone

#endif

#ifndef RTL_LOITER_TIME

 # define RTL_LOITER_TIME     5000  // Time (in milliseconds) to loiter above home before beginning final descent

#endif

// AUTO Mode

#ifndef WP_YAW_BEHAVIOR_DEFAULT

 # define WP_YAW_BEHAVIOR_DEFAULT WP_YAW_BEHAVIOR_LOOK_AT_NEXT_WP_EXCEPT_RTL

#endif

#ifndef AUTO_YAW_SLEW_RATE

 # define AUTO_YAW_SLEW_RATE  60       // degrees/sec

#endif

#ifndef YAW_LOOK_AHEAD_MIN_SPEED

 # define YAW_LOOK_AHEAD_MIN_SPEED 100      // minimum ground speed in cm/s required before copter is aimed at ground course

#endif

// Super Simple mode

#ifndef SUPER_SIMPLE_RADIUS

 # define SUPER_SIMPLE_RADIUS   1000

#endif

//////////////////////////////////////////////////////////////////////////////

// Stabilize Rate Control

//

#ifndef ROLL_PITCH_YAW_INPUT_MAX

 # define ROLL_PITCH_YAW_INPUT_MAX   4500    // roll, pitch and yaw input range

#endif

#ifndef DEFAULT_ANGLE_MAX

 # define DEFAULT_ANGLE_MAX    4500      // ANGLE_MAX parameters default value

#endif

#ifndef ANGLE_RATE_MAX

 # define ANGLE_RATE_MAX      18000     // default maximum rotation rate in roll/pitch axis requested by angle controller used in stabilize, loiter, rtl, auto flight modes

#endif

//////////////////////////////////////////////////////////////////////////////

// Loiter position control gains

//

#ifndef POS_XY_P

 # define POS_XY_P      

1.0f

#endif

//////////////////////////////////////////////////////////////////////////////

// Stop mode defaults

//

#ifndef BRAKE_MODE_SPEED_Z

 # define BRAKE_MODE_SPEED_Z  250 // z-axis speed in cm/s in Brake Mode

#endif

#ifndef BRAKE_MODE_DECEL_RATE

 # define BRAKE_MODE_DECEL_RATE 750 // acceleration rate in cm/s/s in Brake Mode

#endif

//////////////////////////////////////////////////////////////////////////////

// Velocity (horizontal) gains

//

#ifndef VEL_XY_P

 # define VEL_XY_P       1.0f

#endif

#ifndef VEL_XY_I

 # define VEL_XY_I       0.5f

#endif

#ifndef VEL_XY_IMAX

 # define VEL_XY_IMAX     1000

#endif

#ifndef VEL_XY_FILT_HZ

 # define VEL_XY_FILT_HZ    5.0f

#endif

//////////////////////////////////////////////////////////////////////////////

// PosHold parameter defaults

//

#ifndef POSHOLD_ENABLED

 # define POSHOLD_ENABLED       ENABLED // PosHold flight mode enabled by default

#endif

#ifndef POSHOLD_BRAKE_RATE_DEFAULT

 # define POSHOLD_BRAKE_RATE_DEFAULT  8   // default POSHOLD_BRAKE_RATE param value. Rotation rate during braking in deg/sec

#endif

#ifndef POSHOLD_BRAKE_ANGLE_DEFAULT

 # define POSHOLD_BRAKE_ANGLE_DEFAULT 3000  // default POSHOLD_BRAKE_ANGLE param value. Max lean angle during braking in centi-degrees

#endif

//////////////////////////////////////////////////////////////////////////////

// Throttle control gains

//

#ifndef THR_DZ_DEFAULT

# define THR_DZ_DEFAULT    100      // the deadzone above and below mid throttle while in althold or loiter

#endif

#ifndef ALT_HOLD_P

 # define ALT_HOLD_P      1.0f

#endif

// Velocity (vertical) control gains

#ifndef VEL_Z_P

 # define VEL_Z_P   5.0f

#endif

// Accel (vertical) control gains

#ifndef ACCEL_Z_P

 # define ACCEL_Z_P  0.50f

#endif

#ifndef ACCEL_Z_I

 # define ACCEL_Z_I  1.00f

#endif

#ifndef ACCEL_Z_D

 # define ACCEL_Z_D  0.0f

#endif

#ifndef ACCEL_Z_IMAX

 # define ACCEL_Z_IMAX 800

#endif

#ifndef ACCEL_Z_FILT_HZ

 # define ACCEL_Z_FILT_HZ 20.0f

#endif

// default maximum vertical velocity and acceleration the pilot may request

#ifndef PILOT_VELZ_MAX

 # define PILOT_VELZ_MAX  250  // maximum vertical velocity in cm/s

#endif

#ifndef PILOT_ACCEL_Z_DEFAULT

 # define PILOT_ACCEL_Z_DEFAULT 250 // vertical acceleration in cm/s/s while altitude is under pilot control

#endif

// max distance in cm above or below current location that will be used for the alt target when transitioning to alt-hold mode

#ifndef ALT_HOLD_INIT_MAX_OVERSHOOT

 # define ALT_HOLD_INIT_MAX_OVERSHOOT 200

#endif

// the acceleration used to define the distance-velocity curve

#ifndef ALT_HOLD_ACCEL_MAX

 # define ALT_HOLD_ACCEL_MAX 250  // if you change this you must also update the duplicate declaration in AC_WPNav.h

#endif

#ifndef AUTO_DISARMING_DELAY

# define AUTO_DISARMING_DELAY 10

#endif

//////////////////////////////////////////////////////////////////////////////

// Throw mode configuration

//

#ifndef THROW_HIGH_SPEED

# define THROW_HIGH_SPEED   500.0f // vehicle much reach this total 3D speed in cm/s (or be free falling)

#endif

#ifndef THROW_VERTICAL_SPEED

# define THROW_VERTICAL_SPEED 50.0f // motors start when vehicle reaches this total 3D speed in cm/s

#endif

//////////////////////////////////////////////////////////////////////////////

// Dataflash logging control

//

#ifndef LOGGING_ENABLED

 # define LOGGING_ENABLED        ENABLED

#endif

// Default logging bitmask

#ifndef DEFAULT_LOG_BITMASK

 # define DEFAULT_LOG_BITMASK \

  MASK_LOG_ATTITUDE_MED | \

  MASK_LOG_GPS | \

  MASK_LOG_PM | \

  MASK_LOG_CTUN | \

  MASK_LOG_NTUN | \

  MASK_LOG_RCIN | \

  MASK_LOG_IMU | \

  MASK_LOG_CMD | \

  MASK_LOG_CURRENT | \

  MASK_LOG_RCOUT | \

  MASK_LOG_OPTFLOW | \

  MASK_LOG_COMPASS | \

  MASK_LOG_CAMERA | \

  MASK_LOG_MOTBATT

#endif

//////////////////////////////////////////////////////////////////////////////

// Fence, Rally and Terrain and AC_Avoidance defaults

//

// Enable/disable Fence

#ifndef AC_FENCE

 #define AC_FENCE ENABLED

#endif

#ifndef AC_RALLY

 #define AC_RALLY ENABLED

#endif

#ifndef AC_TERRAIN

 #define AC_TERRAIN ENABLED

#endif

#if AC_TERRAIN && !AC_RALLY

 #error Terrain relies on Rally which is disabled

#endif

#ifndef AC_AVOID_ENABLED

 #define AC_AVOID_ENABLED ENABLED

#endif

#if AC_AVOID_ENABLED && !PROXIMITY_ENABLED

 #error AC_Avoidance relies on PROXIMITY_ENABLED which is disabled

#endif

#if AC_AVOID_ENABLED && !AC_FENCE

 #error AC_Avoidance relies on AC_FENCE which is disabled

#endif

//////////////////////////////////////////////////////////////////////////////

// Developer Items

//

// use this to completely disable the CLI

#ifndef CLI_ENABLED

 # define CLI_ENABLED     ENABLED

#endif

//use this to completely disable FRSKY TELEM

#ifndef FRSKY_TELEM_ENABLED

 # define FRSKY_TELEM_ENABLED     ENABLED

#endif

#ifndef ADVANCED_FAILSAFE

# define ADVANCED_FAILSAFE DISABLED

#endif

APM_Config.h

// User specific config file. Any items listed in config.h can be overridden here.

// If you used to define your CONFIG_APM_HARDWARE setting here, it is no longer

// valid! You should switch to using a HAL_BOARD flag in your local config.mk.

// uncomment the lines below to disable features (flash sizes listed are for APM2 boards and will underestimate savings on Pixhawk and other boards)

//#define LOGGING_ENABLED   DISABLED      // disable dataflash logging to save 11K of flash space

//#define MOUNT        DISABLED      // disable the camera gimbal to save 8K of flash space

//#define AUTOTUNE_ENABLED   DISABLED      // disable the auto tune functionality to save 7k of flash

//#define AC_FENCE       DISABLED      // disable fence to save 2k of flash

//#define CAMERA        DISABLED      // disable camera trigger to save 1k of flash

//#define RANGEFINDER_ENABLED DISABLED      // disable rangefinder to save 1k of flash

//#define PROXIMITY_ENABLED  DISABLED      // disable proximity sensors

//#define POSHOLD_ENABLED   DISABLED      // disable PosHold flight mode to save 4.5k of flash

//#define AC_RALLY       DISABLED      // disable rally points library (must also disable terrain which relies on rally)

//#define AC_TERRAIN      DISABLED      // disable terrain library

//#define PARACHUTE      DISABLED      // disable parachute release to save 1k of flash

//#define CLI_ENABLED     DISABLED      // disable the CLI (command-line-interface) to save 21K of flash space

//#define NAV_GUIDED      DISABLED      // disable external navigation computer ability to control vehicle through MAV_CMD_NAV_GUIDED mission commands

//#define OPTFLOW       DISABLED      // disable optical flow sensor to save 5K of flash space

//#define FRSKY_TELEM_ENABLED DISABLED      // disable FRSky telemetry

//#define ADSB_ENABLED     DISABLED      // disable ADSB support

//#define PRECISION_LANDING  DISABLED      // disable precision landing using companion computer or IRLock sensor

//#define SPRAYER       DISABLED      // disable the crop sprayer feature (two ESC controlled pumps the speed of which depends upon the vehicle's horizontal velocity)

// features below are disabled by default on all boards

//#define CAL_ALWAYS_REBOOT            // flight controller will reboot after compass or accelerometer calibration completes

//#define DISALLOW_GCS_MODE_CHANGE_DURING_RC_FAILSAFE // disable mode changes from GCS during Radio failsafes. Avoids a race condition for vehicle like Solo in which the RC and telemetry travel along the same link

//#define ADVANCED_FAILSAFE  ENABLED      // enabled advanced failsafe which allows running a portion of the mission in failsafe events

// other settings

//#define THROTTLE_IN_DEADBAND 100        // redefine size of throttle deadband in pwm (0 ~ 1000)

//#define HIL_MODE       HIL_MODE_SENSORS  // build for hardware-in-the-loop simulation

// User Hooks : For User Developed code that you wish to run

// Put your variable definitions into the UserVariables.h file (or another file name and then change the #define below).

//#define USERHOOK_VARIABLES "UserVariables.h"

// Put your custom code into the UserCode.cpp with function names matching those listed below and ensure the appropriate #define below is uncommented below

//#define USERHOOK_INIT userhook_init();           // for code to be run once at startup

//#define USERHOOK_FASTLOOP userhook_FastLoop();      // for code to be run at 100hz

//#define USERHOOK_50HZLOOP userhook_50Hz();         // for code to be run at 50hz

//#define USERHOOK_MEDIUMLOOP userhook_MediumLoop();    // for code to be run at 10hz

//#define USERHOOK_SLOWLOOP userhook_SlowLoop();      // for code to be run at 3.3hz

//#define USERHOOK_SUPERSLOWLOOP userhook_SuperSlowLoop(); // for code to be run at 1hz

defines.h

#pragma once

#include <AP_HAL/AP_HAL_Boards.h>

// Just so that it's completely clear...

#define ENABLED        1

#define DISABLED        0

// this avoids a very common config error

#define ENABLE ENABLED

#define DISABLE DISABLED

// Autopilot Yaw Mode enumeration

enum autopilot_yaw_mode {

  AUTO_YAW_HOLD =      0, // pilot controls the heading

  AUTO_YAW_LOOK_AT_NEXT_WP = 1, // point towards next waypoint (no pilot input accepted)

  AUTO_YAW_ROI =       2, // point towards a location held in roi_WP (no pilot input accepted)

  AUTO_YAW_LOOK_AT_HEADING = 3, // point towards a particular angle (not pilot input accepted)

  AUTO_YAW_LOOK_AHEAD =   4, // point in the direction the copter is moving

  AUTO_YAW_RESETTOARMEDYAW = 5, // point towards heading at time motors were armed

};

// Ch6... Ch12 aux switch control

#define AUX_SWITCH_PWM_TRIGGER_HIGH 1800 // pwm value above which the ch7 or ch8 option will be invoked

#define AUX_SWITCH_PWM_TRIGGER_LOW 1200 // pwm value below which the ch7 or ch8 option will be disabled

#define CH6_PWM_TRIGGER_HIGH  1800

#define CH6_PWM_TRIGGER_LOW  1200

// values used by the ap.ch7_opt and ap.ch8_opt flags

#define AUX_SWITCH_LOW       0   // indicates auxiliary switch is in the low position (pwm <1200)

#define AUX_SWITCH_MIDDLE     1   // indicates auxiliary switch is in the middle position (pwm >1200, <1800)

#define AUX_SWITCH_HIGH      2   // indicates auxiliary switch is in the high position (pwm >1800)

// Aux Switch enumeration

enum aux_sw_func {

  AUXSW_DO_NOTHING =     0, // aux switch disabled

  AUXSW_FLIP =        2, // flip

  AUXSW_SIMPLE_MODE =     3, // change to simple mode

  AUXSW_RTL =         4, // change to RTL flight mode

  AUXSW_SAVE_TRIM =      5, // save current position as level

  AUXSW_SAVE_WP =       7, // save mission waypoint or RTL if in auto mode

  AUXSW_CAMERA_TRIGGER =   9, // trigger camera servo or relay

  AUXSW_RANGEFINDER =    10, // allow enabling or disabling rangefinder in flight which helps avoid surface tracking when you are far above the ground

  AUXSW_FENCE =       11, // allow enabling or disabling fence in flight

  AUXSW_RESETTOARMEDYAW =  12, // deprecated. changes yaw to be same as when quad was armed

  AUXSW_SUPERSIMPLE_MODE =  13, // change to simple mode in middle, super simple at top

  AUXSW_ACRO_TRAINER =    14, // low = disabled, middle = leveled, high = leveled and limited

  AUXSW_SPRAYER =      15, // enable/disable the crop sprayer

  AUXSW_AUTO =        16, // change to auto flight mode

  AUXSW_AUTOTUNE =      17, // auto tune

  AUXSW_LAND =        18, // change to LAND flight mode

  AUXSW_GRIPPER =      19, // Operate cargo grippers low=off, middle=neutral, high=on

  AUXSW_PARACHUTE_ENABLE = 21, // Parachute enable/disable

  AUXSW_PARACHUTE_RELEASE = 22, // Parachute release

  AUXSW_PARACHUTE_3POS =   23, // Parachute disable, enable, release with 3 position switch

  AUXSW_MISSION_RESET =   24, // Reset auto mission to start from first command

  AUXSW_ATTCON_FEEDFWD =   25, // enable/disable the roll and pitch rate feed forward

  AUXSW_ATTCON_ACCEL_LIM =  26, // enable/disable the roll, pitch and yaw accel limiting

  AUXSW_RETRACT_MOUNT =   27, // Retract Mount

  AUXSW_RELAY =       28, // Relay pin on/off (only supports first relay)

  AUXSW_LANDING_GEAR =    29, // Landing gear controller

  AUXSW_LOST_COPTER_SOUND = 30, // Play lost copter sound

  AUXSW_MOTOR_ESTOP =    31, // Emergency Stop Switch

  AUXSW_MOTOR_INTERLOCK =  32, // Motor On/Off switch

  AUXSW_BRAKE =       33, // Brake flight mode

AUXSW_RELAY2 =       34, // Relay2 pin on/off (in Mission planner set CH8_OPT = 34)

  AUXSW_RELAY3 =       35, // Relay3 pin on/off (in Mission planner set CH9_OPT = 35)

  AUXSW_RELAY4 =       36, // Relay4 pin on/off (in Mission planner set CH10_OPT = 36)

  AUXSW_THROW =       37, // change to THROW flight mode

  AUXSW_AVOID_ADSB =     38, // enable AP_Avoidance library

  AUXSW_PRECISION_LOITER =  39, // enable precision loiter

  AUXSW_AVOID_PROXIMITY =  40, // enable object avoidance using proximity sensors (ie. horizontal lidar)

  AUXSW_ARMDISARM =     41, // arm or disarm vehicle

  AUXSW_SWITCH_MAX,

};

// Frame types

#define UNDEFINED_FRAME 0

#define MULTICOPTER_FRAME 1

#define HELI_FRAME 2

// HIL enumerations

#define HIL_MODE_DISABLED       0

#define HIL_MODE_SENSORS        1

// Auto Pilot Modes enumeration

enum control_mode_t {

  STABILIZE =  0, // manual airframe angle with manual throttle

  ACRO =     1, // manual body-frame angular rate with manual throttle

  ALT_HOLD =   2, // manual airframe angle with automatic throttle

  AUTO =     3, // fully automatic waypoint control using mission commands

  GUIDED =    4, // fully automatic fly to coordinate or fly at velocity/direction using GCS immediate commands

  LOITER =    5, // automatic horizontal acceleration with automatic throttle

  RTL =     6, // automatic return to launching point

  CIRCLE =    7, // automatic circular flight with automatic throttle

  LAND =     9, // automatic landing with horizontal position control

  DRIFT =    11, // semi-automous position, yaw and throttle control

  SPORT =    13, // manual earth-frame angular rate control with manual throttle

  FLIP =    14, // automatically flip the vehicle on the roll axis

  AUTOTUNE =  15, // automatically tune the vehicle's roll and pitch gains

  POSHOLD =   16, // automatic position hold with manual override, with automatic throttle

  BRAKE =    17, // full-brake using inertial/GPS system, no pilot input

  THROW =    18, // throw to launch mode using inertial/GPS system, no pilot input

  AVOID_ADSB = 19, // automatic avoidance of obstacles in the macro scale - e.g. full-sized aircraft

  GUIDED_NOGPS = 20, // guided mode but only accepts attitude and altitude

};

enum mode_reason_t {

  MODE_REASON_UNKNOWN=0,

  MODE_REASON_TX_COMMAND,

  MODE_REASON_GCS_COMMAND,

  MODE_REASON_RADIO_FAILSAFE,

  MODE_REASON_BATTERY_FAILSAFE,

  MODE_REASON_GCS_FAILSAFE,

  MODE_REASON_EKF_FAILSAFE,

  MODE_REASON_GPS_GLITCH,

  MODE_REASON_MISSION_END,

  MODE_REASON_THROTTLE_LAND_ESCAPE,

  MODE_REASON_FENCE_BREACH,

  MODE_REASON_TERRAIN_FAILSAFE,

  MODE_REASON_BRAKE_TIMEOUT,

  MODE_REASON_FLIP_COMPLETE,

  MODE_REASON_AVOIDANCE,

  MODE_REASON_AVOIDANCE_RECOVERY,

  MODE_REASON_THROW_COMPLETE,

};

// Tuning enumeration

enum tuning_func {

  TUNING_NONE =            0, //

  TUNING_STABILIZE_ROLL_PITCH_KP =  1, // stabilize roll/pitch angle controller's P term

  TUNING_STABILIZE_YAW_KP =      3, // stabilize yaw heading controller's P term

  TUNING_RATE_ROLL_PITCH_KP =     4, // body frame roll/pitch rate controller's P term

  TUNING_RATE_ROLL_PITCH_KI =     5, // body frame roll/pitch rate controller's I term

  TUNING_YAW_RATE_KP =        6, // body frame yaw rate controller's P term

  TUNING_THROTTLE_RATE_KP =      7, // throttle rate controller's P term (desired rate to acceleration or motor output)

  TUNING_WP_SPEED =         10, // maximum speed to next way point (0 to 10m/s)

  TUNING_LOITER_POSITION_KP =    12, // loiter distance controller's P term (position error to speed)

  TUNING_HELI_EXTERNAL_GYRO =    13, // TradHeli specific external tail gyro gain

  TUNING_ALTITUDE_HOLD_KP =     14, // altitude hold controller's P term (alt error to desired rate)

  TUNING_RATE_ROLL_PITCH_KD =    21, // body frame roll/pitch rate controller's D term

  TUNING_VEL_XY_KP =         22, // loiter rate controller's P term (speed error to tilt angle)

  TUNING_ACRO_RP_KP =        25, // acro controller's P term. converts pilot input to a desired roll, pitch or yaw rate

  TUNING_YAW_RATE_KD =        26, // body frame yaw rate controller's D term

  TUNING_VEL_XY_KI =         28, // loiter rate controller's I term (speed error to tilt angle)

  TUNING_AHRS_YAW_KP =        30, // ahrs's compass effect on yaw angle (0 = very low, 1 = very high)

  TUNING_AHRS_KP =          31, // accelerometer effect on roll/pitch angle (0=low)

  TUNING_ACCEL_Z_KP =        34, // accel based throttle controller's P term

  TUNING_ACCEL_Z_KI =        35, // accel based throttle controller's I term

  TUNING_ACCEL_Z_KD =        36, // accel based throttle controller's D term

  TUNING_DECLINATION =        38, // compass declination in radians

  TUNING_CIRCLE_RATE =        39, // circle turn rate in degrees (hard coded to about 45 degrees in either direction)

  TUNING_ACRO_YAW_KP =        40, // acro controller's P term. converts pilot input to a desired roll, pitch or yaw rate

  TUNING_RANGEFINDER_GAIN =     41, // rangefinder gain

  TUNING_EKF_VERTICAL_POS =     42, // EKF's baro vs accel (higher rely on accels more, baro impact is reduced). Range should be 0.2 ~ 4.0? 2.0 is default

  TUNING_EKF_HORIZONTAL_POS =    43, // EKF's gps vs accel (higher rely on accels more, gps impact is reduced). Range should be 1.0 ~ 3.0? 1.5 is default

  TUNING_EKF_ACCEL_NOISE =      44, // EKF's accel noise (lower means trust accels more, gps & baro less). Range should be 0.02 ~ 0.5 0.5 is default (but very robust at that level)

  TUNING_RC_FEEL_RP =        45, // roll-pitch input smoothing

  TUNING_RATE_PITCH_KP =       46, // body frame pitch rate controller's P term

  TUNING_RATE_PITCH_KI =       47, // body frame pitch rate controller's I term

  TUNING_RATE_PITCH_KD =       48, // body frame pitch rate controller's D term

  TUNING_RATE_ROLL_KP =       49, // body frame roll rate controller's P term

  TUNING_RATE_ROLL_KI =       50, // body frame roll rate controller's I term

  TUNING_RATE_ROLL_KD =       51, // body frame roll rate controller's D term

  TUNING_RATE_PITCH_FF =       52, // body frame pitch rate controller FF term

  TUNING_RATE_ROLL_FF =       53, // body frame roll rate controller FF term

  TUNING_RATE_YAW_FF =        54, // body frame yaw rate controller FF term

  TUNING_RATE_MOT_YAW_HEADROOM =   55, // motors yaw headroom minimum

  TUNING_RATE_YAW_FILT =       56 // yaw rate input filter

};

// Acro Trainer types

#define ACRO_TRAINER_DISABLED 0

#define ACRO_TRAINER_LEVELING 1

#define ACRO_TRAINER_LIMITED  2

// RC Feel roll/pitch definitions

#define RC_FEEL_RP_VERY_SOFT    0

#define RC_FEEL_RP_SOFT      25

#define RC_FEEL_RP_MEDIUM     50

#define RC_FEEL_RP_CRISP      75

#define RC_FEEL_RP_VERY_CRISP   100

// Yaw behaviours during missions - possible values for WP_YAW_BEHAVIOR parameter

#define WP_YAW_BEHAVIOR_NONE             0 // auto pilot will never control yaw during missions or rtl (except for DO_CONDITIONAL_YAW command received)

#define WP_YAW_BEHAVIOR_LOOK_AT_NEXT_WP       1 // auto pilot will face next waypoint or home during rtl

#define WP_YAW_BEHAVIOR_LOOK_AT_NEXT_WP_EXCEPT_RTL  2 // auto pilot will face next waypoint except when doing RTL at which time it will stay in it's last

#define WP_YAW_BEHAVIOR_LOOK_AHEAD          3 // auto pilot will look ahead during missions and rtl (primarily meant for traditional helicotpers)

// Auto modes

enum AutoMode {

  Auto_TakeOff,

  Auto_WP,

  Auto_Land,

  Auto_RTL,

  Auto_CircleMoveToEdge,

  Auto_Circle,

  Auto_Spline,

  Auto_NavGuided,

  Auto_Loiter,

  Auto_NavPayloadPlace,

};

// Guided modes

enum GuidedMode {

  Guided_TakeOff,

  Guided_WP,

  Guided_Velocity,

  Guided_PosVel,

  Guided_Angle,

};

// RTL states

enum RTLState {

  RTL_InitialClimb,

  RTL_ReturnHome,

  RTL_LoiterAtHome,

  RTL_FinalDescent,

  RTL_Land

};

// Alt_Hold states

enum AltHoldModeState {

  AltHold_MotorStopped,

  AltHold_Takeoff,

  AltHold_Flying,

  AltHold_Landed

};

// Loiter states

enum LoiterModeState {

  Loiter_MotorStopped,

  Loiter_Takeoff,

  Loiter_Flying,

  Loiter_Landed

};

// Sport states

enum SportModeState {

  Sport_MotorStopped,

  Sport_Takeoff,

  Sport_Flying,

  Sport_Landed

};

// Flip states

enum FlipState {

  Flip_Start,

  Flip_Roll,

  Flip_Pitch_A,

  Flip_Pitch_B,

  Flip_Recover,

  Flip_Abandon

};

// Throw stages

enum ThrowModeStage {

  Throw_Disarmed,

  Throw_Detecting,

  Throw_Uprighting,

  Throw_HgtStabilise,

  Throw_PosHold

};

// Throw types

enum ThrowModeType {

  ThrowType_Upward = 0,

  ThrowType_Drop = 1

};

enum LandStateType {

  LandStateType_FlyToLocation = 0,

  LandStateType_Descending = 1

};

enum PayloadPlaceStateType {

  PayloadPlaceStateType_FlyToLocation,

  PayloadPlaceStateType_Calibrating_Hover_Start,

  PayloadPlaceStateType_Calibrating_Hover,

  PayloadPlaceStateType_Descending_Start,

  PayloadPlaceStateType_Descending,

  PayloadPlaceStateType_Releasing_Start,

  PayloadPlaceStateType_Releasing,

  PayloadPlaceStateType_Released,

  PayloadPlaceStateType_Ascending_Start,

  PayloadPlaceStateType_Ascending,

  PayloadPlaceStateType_Done,

};

// bit options for DEV_OPTIONS parameter

enum DevOptions {

  DevOptionADSBMAVLink = 1,

};

// Logging parameters

#define TYPE_AIRSTART_MSG       0x00

#define TYPE_GROUNDSTART_MSG      0x01

#define LOG_CONTROL_TUNING_MSG     0x04

#define LOG_NAV_TUNING_MSG       0x05

#define LOG_PERFORMANCE_MSG      0x06

#define LOG_OPTFLOW_MSG        0x0C

#define LOG_EVENT_MSG         0x0D

#define LOG_PID_MSG          0x0E  // deprecated

#define LOG_INAV_MSG          0x11  // deprecated

#define LOG_CAMERA_MSG_DEPRECATED   0x12  // deprecated

#define LOG_ERROR_MSG         0x13

#define LOG_DATA_INT16_MSG       0x14

#define LOG_DATA_UINT16_MSG      0x15

#define LOG_DATA_INT32_MSG       0x16

#define LOG_DATA_UINT32_MSG      0x17

#define LOG_DATA_FLOAT_MSG       0x18

#define LOG_AUTOTUNE_MSG        0x19

#define LOG_AUTOTUNEDETAILS_MSG    0x1A

#define LOG_MOTBATT_MSG        0x1E

#define LOG_PARAMTUNE_MSG       0x1F

#define LOG_HELI_MSG          0x20

#define LOG_PRECLAND_MSG        0x21

#define LOG_GUIDEDTARGET_MSG      0x22

#define LOG_THROW_MSG         0x23

#define LOG_PROXIMITY_MSG       0x24

#define LOG_BEACON_MSG         0x25

#define MASK_LOG_ATTITUDE_FAST     (1<<0)

#define MASK_LOG_ATTITUDE_MED     (1<<1)

#define MASK_LOG_GPS          (1<<2)

#define MASK_LOG_PM          (1<<3)

#define MASK_LOG_CTUN         (1<<4)

#define MASK_LOG_NTUN         (1<<5)

#define MASK_LOG_RCIN         (1<<6)

#define MASK_LOG_IMU          (1<<7)

#define MASK_LOG_CMD          (1<<8)

#define MASK_LOG_CURRENT        (1<<9)

#define MASK_LOG_RCOUT         (1<<10)

#define MASK_LOG_OPTFLOW        (1<<11)

#define MASK_LOG_PID          (1<<12)

#define MASK_LOG_COMPASS        (1<<13)

#define MASK_LOG_INAV         (1<<14) // deprecated

#define MASK_LOG_CAMERA        (1<<15)

#define MASK_LOG_MOTBATT        (1UL<<17)

#define MASK_LOG_IMU_FAST       (1UL<<18)

#define MASK_LOG_IMU_RAW        (1UL<<19)

#define MASK_LOG_ANY          0xFFFF

// DATA - event logging

#define DATA_AP_STATE           7

#define DATA_SYSTEM_TIME_SET        8

#define DATA_INIT_SIMPLE_BEARING      9

#define DATA_ARMED             10

#define DATA_DISARMED           11

#define DATA_AUTO_ARMED          15

#define DATA_LAND_COMPLETE_MAYBE      17

#define DATA_LAND_COMPLETE         18

#define DATA_NOT_LANDED          28

#define DATA_LOST_GPS           19

#define DATA_FLIP_START          21

#define DATA_FLIP_END           22

#define DATA_SET_HOME           25

#define DATA_SET_SIMPLE_ON         26

#define DATA_SET_SIMPLE_OFF        27

#define DATA_SET_SUPERSIMPLE_ON      29

#define DATA_AUTOTUNE_INITIALISED     30

#define DATA_AUTOTUNE_OFF         31

#define DATA_AUTOTUNE_RESTART       32

#define DATA_AUTOTUNE_SUCCESS       33

#define DATA_AUTOTUNE_FAILED        34

#define DATA_AUTOTUNE_REACHED_LIMIT    35

#define DATA_AUTOTUNE_PILOT_TESTING    36

#define DATA_AUTOTUNE_SAVEDGAINS      37

#define DATA_SAVE_TRIM           38

#define DATA_SAVEWP_ADD_WP         39

#define DATA_FENCE_ENABLE         41

#define DATA_FENCE_DISABLE         42

#define DATA_ACRO_TRAINER_DISABLED     43

#define DATA_ACRO_TRAINER_LEVELING     44

#define DATA_ACRO_TRAINER_LIMITED     45

#define DATA_GRIPPER_GRAB         46

#define DATA_GRIPPER_RELEASE        47

#define DATA_PARACHUTE_DISABLED      49

#define DATA_PARACHUTE_ENABLED       50

#define DATA_PARACHUTE_RELEASED      51

#define DATA_LANDING_GEAR_DEPLOYED     52

#define DATA_LANDING_GEAR_RETRACTED    53

#define DATA_MOTORS_EMERGENCY_STOPPED   54

#define DATA_MOTORS_EMERGENCY_STOP_CLEARED 55

#define DATA_MOTORS_INTERLOCK_DISABLED   56

#define DATA_MOTORS_INTERLOCK_ENABLED   57

#define DATA_ROTOR_RUNUP_COMPLETE     58 // Heli only

#define DATA_ROTOR_SPEED_BELOW_CRITICAL  59 // Heli only

#define DATA_EKF_ALT_RESET         60

#define DATA_LAND_CANCELLED_BY_PILOT    61

#define DATA_EKF_YAW_RESET         62

#define DATA_AVOIDANCE_ADSB_ENABLE     63

#define DATA_AVOIDANCE_ADSB_DISABLE    64

#define DATA_AVOIDANCE_PROXIMITY_ENABLE  65

#define DATA_AVOIDANCE_PROXIMITY_DISABLE  66

#define DATA_GPS_PRIMARY_CHANGED      67

// Centi-degrees to radians

#define DEGX100 5729.57795f

// Error message sub systems and error codes

#define ERROR_SUBSYSTEM_MAIN        1

#define ERROR_SUBSYSTEM_RADIO       2

#define ERROR_SUBSYSTEM_COMPASS      3

#define ERROR_SUBSYSTEM_OPTFLOW      4

#define ERROR_SUBSYSTEM_FAILSAFE_RADIO   5

#define ERROR_SUBSYSTEM_FAILSAFE_BATT   6

#define ERROR_SUBSYSTEM_FAILSAFE_GPS    7 // not used

#define ERROR_SUBSYSTEM_FAILSAFE_GCS    8

#define ERROR_SUBSYSTEM_FAILSAFE_FENCE   9

#define ERROR_SUBSYSTEM_FLIGHT_MODE    10

#define ERROR_SUBSYSTEM_GPS        11 // not used

#define ERROR_SUBSYSTEM_CRASH_CHECK    12

#define ERROR_SUBSYSTEM_FLIP        13

#define ERROR_SUBSYSTEM_AUTOTUNE      14

#define ERROR_SUBSYSTEM_PARACHUTE     15

#define ERROR_SUBSYSTEM_EKFCHECK      16

#define ERROR_SUBSYSTEM_FAILSAFE_EKFINAV  17

#define ERROR_SUBSYSTEM_BARO        18

#define ERROR_SUBSYSTEM_CPU        19

#define ERROR_SUBSYSTEM_FAILSAFE_ADSB   20

#define ERROR_SUBSYSTEM_TERRAIN      21

#define ERROR_SUBSYSTEM_NAVIGATION     22

#define ERROR_SUBSYSTEM_FAILSAFE_TERRAIN  23

#define ERROR_SUBSYSTEM_EKF_PRIMARY    24

// general error codes

#define ERROR_CODE_ERROR_RESOLVED     0

#define ERROR_CODE_FAILED_TO_INITIALISE  1

#define ERROR_CODE_UNHEALTHY        4

// subsystem specific error codes -- radio

#define ERROR_CODE_RADIO_LATE_FRAME    2

// subsystem specific error codes -- failsafe_thr, batt, gps

#define ERROR_CODE_FAILSAFE_RESOLVED    0

#define ERROR_CODE_FAILSAFE_OCCURRED    1

// subsystem specific error codes -- compass

#define ERROR_CODE_COMPASS_FAILED_TO_READ 2

// subsystem specific error codes -- main

#define ERROR_CODE_MAIN_INS_DELAY     1

// subsystem specific error codes -- crash checker

#define ERROR_CODE_CRASH_CHECK_CRASH    1

#define ERROR_CODE_CRASH_CHECK_LOSS_OF_CONTROL 2

// subsystem specific error codes -- flip

#define ERROR_CODE_FLIP_ABANDONED     2

// subsystem specific error codes -- terrain

#define ERROR_CODE_MISSING_TERRAIN_DATA  2

// subsystem specific error codes -- navigation

#define ERROR_CODE_FAILED_TO_SET_DESTINATION  2

#define ERROR_CODE_RESTARTED_RTL      3

#define ERROR_CODE_FAILED_CIRCLE_INIT   4

#define ERROR_CODE_DEST_OUTSIDE_FENCE   5

// parachute failed to deploy because of low altitude or landed

#define ERROR_CODE_PARACHUTE_TOO_LOW    2

#define ERROR_CODE_PARACHUTE_LANDED    3

// EKF check definitions

#define ERROR_CODE_EKFCHECK_BAD_VARIANCE   2

#define ERROR_CODE_EKFCHECK_VARIANCE_CLEARED 0

// Baro specific error codes

#define ERROR_CODE_BARO_GLITCH       2

// Arming Check Enable/Disable bits

#define ARMING_CHECK_NONE         0x00

#define ARMING_CHECK_ALL          0x01

#define ARMING_CHECK_BARO         0x02

#define ARMING_CHECK_COMPASS        0x04

#define ARMING_CHECK_GPS          0x08

#define ARMING_CHECK_INS          0x10

#define ARMING_CHECK_PARAMETERS      0x20

#define ARMING_CHECK_RC          0x40

#define ARMING_CHECK_VOLTAGE        0x80

// Radio failsafe definitions (FS_THR parameter)

#define FS_THR_DISABLED          0

#define FS_THR_ENABLED_ALWAYS_RTL     1

#define FS_THR_ENABLED_CONTINUE_MISSION  2

#define FS_THR_ENABLED_ALWAYS_LAND    3

// Battery failsafe definitions (FS_BATT_ENABLE parameter)

#define FS_BATT_DISABLED          0   // battery failsafe disabled

#define FS_BATT_LAND            1   // switch to LAND mode on battery failsafe

#define FS_BATT_RTL            2   // switch to RTL mode on battery failsafe

// GCS failsafe definitions (FS_GCS_ENABLE parameter)

#define FS_GCS_DISABLED          0

#define FS_GCS_ENABLED_ALWAYS_RTL     1

#define FS_GCS_ENABLED_CONTINUE_MISSION  2

// EKF failsafe definitions (FS_EKF_ACTION parameter)

#define FS_EKF_ACTION_LAND         1   // switch to LAND mode on EKF failsafe

#define FS_EKF_ACTION_ALTHOLD       2   // switch to ALTHOLD mode on EKF failsafe

#define FS_EKF_ACTION_LAND_EVEN_STABILIZE 3   // switch to Land mode on EKF failsafe even if in a manual flight mode like stabilize

// for mavlink SET_POSITION_TARGET messages

#define MAVLINK_SET_POS_TYPE_MASK_POS_IGNORE   ((1<<0) | (1<<1) | (1<<2))

#define MAVLINK_SET_POS_TYPE_MASK_VEL_IGNORE   ((1<<3) | (1<<4) | (1<<5))

#define MAVLINK_SET_POS_TYPE_MASK_ACC_IGNORE   ((1<<6) | (1<<7) | (1<<8))

#define MAVLINK_SET_POS_TYPE_MASK_FORCE     (1<<9)

#define MAVLINK_SET_POS_TYPE_MASK_YAW_IGNORE   (1<<10)

#define MAVLINK_SET_POS_TYPE_MASK_YAW_RATE_IGNORE (1<<11)

// for PILOT_THR_BHV parameter

#define THR_BEHAVE_FEEDBACK_FROM_MID_STICK (1<<0)

#define THR_BEHAVE_HIGH_THROTTLE_CANCELS_LAND (1<<1)

#define THR_BEHAVE_DISARM_ON_LAND_DETECT (1<<2)