/*
   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_Param/AP_Param.h>
#include <StorageManager/StorageManager.h>

// Application dependencies
#include <GCS_MAVLink/GCS.h>
#include <AP_Logger/AP_Logger.h>          // ArduPilot Mega Flash Memory 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_Mission/AP_Mission.h>     // Mission command library
#include <AC_AttitudeControl/AC_AttitudeControl_Multi.h> // Attitude control library
#include <AC_AttitudeControl/AC_AttitudeControl_Multi_6DoF.h> // 6DoF 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 <AP_Motors/AP_Motors.h>          // AP Motors library
#include <AP_Stats/AP_Stats.h>     // statistics library
#include <Filter/Filter.h>             // Filter library
#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_Loiter.h>
#include <AC_WPNav/AC_Circle.h>          // circle navigation library
#include <AP_Declination/AP_Declination.h>     // ArduPilot Mega Declination Helper Library
#include <AP_RCMapper/AP_RCMapper.h>        // RC input mapping library
#include <AP_BattMonitor/AP_BattMonitor.h>     // Battery monitor library
#include <AP_LandingGear/AP_LandingGear.h>     // Landing Gear library
#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_Arming/AP_Arming.h>
#include <AP_SmartRTL/AP_SmartRTL.h>
#include <AP_TempCalibration/AP_TempCalibration.h>
#include <AC_AutoTune/AC_AutoTune.h>
#include <AP_Parachute/AP_Parachute.h>
#include <AC_Sprayer/AC_Sprayer.h>
#include <AP_ADSB/AP_ADSB.h>
#include <AP_Proximity/AP_Proximity.h>

// Configuration
#include "defines.h"
#include "config.h"

#if FRAME_CONFIG == HELI_FRAME
    #define AC_AttitudeControl_t AC_AttitudeControl_Heli
#else
    #define AC_AttitudeControl_t AC_AttitudeControl_Multi
#endif

#if FRAME_CONFIG == HELI_FRAME
 #define MOTOR_CLASS AP_MotorsHeli
#else
 #define MOTOR_CLASS AP_MotorsMulticopter
#endif

#if MODE_AUTOROTATE_ENABLED == ENABLED
 #include <AC_Autorotation/AC_Autorotation.h> // Autorotation controllers
#endif

#include "RC_Channel.h"         // RC Channel Library

#include "GCS_Mavlink.h"
#include "GCS_Copter.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 BEACON_ENABLED == ENABLED
 #include <AP_Beacon/AP_Beacon.h>
#endif

#if AC_AVOID_ENABLED == ENABLED
 #include <AC_Avoidance/AC_Avoid.h>
#endif
#if AC_OAPATHPLANNER_ENABLED == ENABLED
 #include <AC_WPNav/AC_WPNav_OA.h>
 #include <AC_Avoidance/AP_OAPathPlanner.h>
#endif
#if GRIPPER_ENABLED == ENABLED
 # include <AP_Gripper/AP_Gripper.h>
#endif
#if PRECISION_LANDING == ENABLED
 # include <AC_PrecLand/AC_PrecLand.h>
 # include <AP_IRLock/AP_IRLock.h>
#endif
#if MODE_FOLLOW_ENABLED == ENABLED
 # include <AP_Follow/AP_Follow.h>
#endif
#if AC_FENCE == ENABLED
 # include <AC_Fence/AC_Fence.h>
#endif
#if AC_TERRAIN == ENABLED
 # include <AP_Terrain/AP_Terrain.h>
#endif
#if OPTFLOW == ENABLED
 # include <AP_OpticalFlow/AP_OpticalFlow.h>
#endif
#if RANGEFINDER_ENABLED == ENABLED
 # include <AP_RangeFinder/AP_RangeFinder.h>
#endif

#include <AP_Mount/AP_Mount.h>

#if CAMERA == ENABLED
 # include <AP_Camera/AP_Camera.h>
#endif
#if BUTTON_ENABLED == ENABLED
 # include <AP_Button/AP_Button.h>
#endif

#if OSD_ENABLED || OSD_PARAM_ENABLED
 #include <AP_OSD/AP_OSD.h>
#endif

#if ADVANCED_FAILSAFE == ENABLED
 # include "afs_copter.h"
#endif
#if TOY_MODE_ENABLED == ENABLED
 # include "toy_mode.h"
#endif
#if WINCH_ENABLED == ENABLED
 # include <AP_Winch/AP_Winch.h>
#endif
#if RPM_ENABLED == ENABLED
 #include <AP_RPM/AP_RPM.h>
#endif

#ifdef ENABLE_SCRIPTING
#include <AP_Scripting/AP_Scripting.h>
#endif

// Local modules
#ifdef USER_PARAMS_ENABLED
#include "UserParameters.h"
#endif
#include "Parameters.h"
#if HAL_ADSB_ENABLED
#include "avoidance_adsb.h"
#endif

#if CONFIG_HAL_BOARD == HAL_BOARD_SITL
#include <SITL/SITL.h>
#endif

#include "mode.h"

class Copter : public AP_Vehicle {
public:
    friend class GCS_MAVLINK_Copter;
    friend class GCS_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;
    friend class ToyMode;
    friend class RC_Channel_Copter;
    friend class RC_Channels_Copter;

    friend class AutoTune;

    friend class Mode;
    friend class ModeAcro;
    friend class ModeAcro_Heli;
    friend class ModeAltHold;
    friend class ModeAuto;
    friend class ModeAutoTune;
    friend class ModeAvoidADSB;
    friend class ModeBrake;
    friend class ModeCircle;
    friend class ModeDrift;
    friend class ModeFlip;
    friend class ModeFlowHold;
    friend class ModeFollow;
    friend class ModeGuided;
    friend class ModeLand;
    friend class ModeLoiter;
    friend class ModePosHold;
    friend class ModeRTL;
    friend class ModeSmartRTL;
    friend class ModeSport;
    friend class ModeStabilize;
    friend class ModeStabilize_Heli;
    friend class ModeSystemId;
    friend class ModeThrow;
    friend class ModeZigZag;
    friend class ModeAutorotate;

    Copter(void);

private:

    // key aircraft parameters passed to multiple libraries
    AP_Vehicle::MultiCopter aparm;

    // Global parameters are all contained within the 'g' class.
    Parameters g;
    ParametersG2 g2;

    // used to detect MAVLink acks from GCS to stop compassmot
    uint8_t command_ack_counter;

    // primary input control channels
    RC_Channel *channel_roll;
    RC_Channel *channel_pitch;
    RC_Channel *channel_throttle;
    RC_Channel *channel_yaw;

    AP_Logger logger;

    // flight modes convenience array
    AP_Int8 *flight_modes;
    const uint8_t num_flight_modes = 6;

    struct RangeFinderState {
        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
        float inertial_alt_cm; // inertial alt at time of last rangefinder sample
        uint32_t last_healthy_ms;
        LowPassFilterFloat alt_cm_filt; // altitude filter
        int16_t alt_cm_glitch_protected;    // last glitch protected altitude
        int8_t glitch_count;    // non-zero number indicates rangefinder is glitching
        uint32_t glitch_cleared_ms; // system time glitch cleared
    } rangefinder_state, rangefinder_up_state;

    /*
      return rangefinder height interpolated using inertial altitude
     */
    bool get_rangefinder_height_interpolated_cm(int32_t& ret);

    class SurfaceTracking {
    public:
        // get desired climb rate (in cm/s) to achieve surface tracking
        float adjust_climb_rate(float target_rate);

        // get/set target altitude (in cm) above ground
        bool get_target_alt_cm(float &target_alt_cm) const;
        void set_target_alt_cm(float target_alt_cm);

        // get target and actual distances (in m) for logging purposes
        bool get_target_dist_for_logging(float &target_dist) const;
        float get_dist_for_logging() const;
        void invalidate_for_logging() { valid_for_logging = false; }

        // surface tracking surface
        enum class Surface {
            NONE = 0,
            GROUND = 1,
            CEILING = 2
        };
        // set surface to track
        void set_surface(Surface new_surface);

    private:
        Surface surface = Surface::GROUND;
        float target_dist_cm;       // desired distance in cm from ground or ceiling
        uint32_t last_update_ms;    // system time of last update to target_alt_cm
        uint32_t last_glitch_cleared_ms;    // system time of last handle glitch recovery
        bool valid_for_logging;     // true if target_alt_cm is valid for logging
        bool reset_target;          // true if target should be reset because of change in tracking_state
    } surface_tracking;

#if RPM_ENABLED == ENABLED
    AP_RPM rpm_sensor;
#endif

    // Inertial Navigation EKF - different viewpoint
    AP_AHRS_View *ahrs_view;

#if CONFIG_HAL_BOARD == HAL_BOARD_SITL
    SITL::SITL sitl;
#endif

    // Arming/Disarming management class
    AP_Arming_Copter arming;

    // Optical flow sensor
#if OPTFLOW == ENABLED
    OpticalFlow optflow;
#endif

    // system time in milliseconds of last recorded yaw reset from ekf
    uint32_t ekfYawReset_ms;
    int8_t ekf_primary_core;

    // vibration check
    struct {
        bool high_vibes;    // true while high vibration are detected
        uint32_t start_ms;  // system time high vibration were last detected
        uint32_t clear_ms;  // system time high vibrations stopped
    } vibration_check;

    // GCS selection
    GCS_Copter _gcs; // avoid using this; use gcs()
    GCS_Copter &gcs() { return _gcs; }

    // User variables
#ifdef USERHOOK_VARIABLES
# include USERHOOK_VARIABLES
#endif

    // Documentation of GLobals:
    typedef union {
        struct {
            uint8_t unused1                 : 1; // 0
            uint8_t unused_was_simple_mode  : 2; // 1,2
            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 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_unused    : 1; // 9       // UNUSED
            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_unused  : 1; // 16      // true if the system time has been set from the GPS
            uint8_t gps_glitching           : 1; // 17      // true if GPS glitching is affecting navigation accuracy
            uint8_t using_interlock         : 1; // 20      // aux switch motor interlock function is in use
            uint8_t land_repo_active        : 1; // 21      // true if the pilot is overriding the landing position
            uint8_t motor_interlock_switch  : 1; // 22      // true if pilot is requesting motor interlock enable
            uint8_t in_arming_delay         : 1; // 23      // true while we are armed but waiting to spin motors
            uint8_t initialised_params      : 1; // 24      // true when the all parameters have been initialised. we cannot send parameters to the GCS until this is done
            uint8_t unused3                 : 1; // 25      // was compass_init_location; true when the compass's initial location has been set
            uint8_t unused2                 : 1; // 26      // aux switch rc_override is allowed
            uint8_t armed_with_switch       : 1; // 27      // we armed using a arming switch
        };
        uint32_t value;
    } ap_t;

    ap_t ap;

    AirMode air_mode; // air mode is 0 = not-configured ; 1 = disabled; 2 = enabled

    static_assert(sizeof(uint32_t) == sizeof(ap), "ap_t must be uint32_t");

    // This is the state of the flight control system
    // There are multiple states defined such as STABILIZE, ACRO,
    Mode *flightmode;
    Mode::Number prev_control_mode;

    RCMapper rcmap;

    // inertial nav alt when we armed
    float arming_altitude_m;

    // Failsafe
    struct {
        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

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

        uint8_t radio               : 1; // A status flag for the radio failsafe
        uint8_t gcs                 : 1; // A status flag for the ground station failsafe
        uint8_t ekf                 : 1; // true if ekf failsafe has occurred
        uint8_t terrain             : 1; // true if the missing terrain data failsafe has occurred
        uint8_t adsb                : 1; // true if an adsb related failsafe has occurred
    } failsafe;

    bool any_failsafe_triggered() const {
        return failsafe.radio || battery.has_failsafed() || failsafe.gcs || failsafe.ekf || failsafe.terrain || failsafe.adsb;
    }

    // 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 : 2;    // primary gps index
    } sensor_health;

    // Motor Output
    MOTOR_CLASS *motors;
    const struct AP_Param::GroupInfo *motors_var_info;

    int32_t _home_bearing;
    uint32_t _home_distance;

    // SIMPLE Mode
    // Used to track the orientation of the vehicle for Simple mode. This value is reset at each arming
    // or in SuperSimple mode when the vehicle leaves a 20m radius from home.
    enum class SimpleMode {
        NONE = 0,
        SIMPLE = 1,
        SUPERSIMPLE = 2,
    } simple_mode;

    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;

    // Battery Sensors
    AP_BattMonitor battery{MASK_LOG_CURRENT,
                           FUNCTOR_BIND_MEMBER(&Copter::handle_battery_failsafe, void, const char*, const int8_t),
                           _failsafe_priorities};

#if OSD_ENABLED || OSD_PARAM_ENABLED
    AP_OSD osd;
#endif

    // Altitude
    int32_t baro_alt;            // barometer altitude in cm above home
    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 vehicle (altitude is relative to home)
    Location current_loc;

    // 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_t *attitude_control;
    AC_PosControl *pos_control;
    AC_WPNav *wp_nav;
    AC_Loiter *loiter_nav;

#if MODE_CIRCLE_ENABLED == ENABLED
    AC_Circle *circle_nav;
#endif

    // System Timers
    // --------------
    // 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;
    bool auto_trim_started = false;

    // Camera
#if CAMERA == ENABLED
    AP_Camera camera{MASK_LOG_CAMERA, current_loc};
#endif

    // Camera/Antenna mount tracking and stabilisation stuff
#if HAL_MOUNT_ENABLED
    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

    // Crop Sprayer
#if SPRAYER_ENABLED == ENABLED
    AC_Sprayer sprayer;
#endif

    // Parachute release
#if PARACHUTE == ENABLED
    AP_Parachute parachute{relay};
#endif

    // Landing Gear Controller
#if LANDING_GEAR_ENABLED == ENABLED
    AP_LandingGear landinggear;
#endif

    // terrain handling
#if AP_TERRAIN_AVAILABLE && AC_TERRAIN && MODE_AUTO_ENABLED == ENABLED
    AP_Terrain terrain{mode_auto.mission};
#endif

    // Precision Landing
#if PRECISION_LANDING == ENABLED
    AC_PrecLand precland;
#endif

    // Pilot Input Management Library
    // Only used for Helicopter for now
#if FRAME_CONFIG == HELI_FRAME
    AC_InputManager_Heli input_manager;
#endif

#if HAL_ADSB_ENABLED
    AP_ADSB adsb;

    // avoidance of adsb enabled vehicles (normally manned vehicles)
    AP_Avoidance_Copter avoidance_adsb{adsb};
#endif

    // last valid RC input time
    uint32_t last_radio_update_ms;

    // last esc calibration notification update
    uint32_t esc_calibration_notify_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
    typedef 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 inverted_flight         : 1;    // 1   // true for inverted flight mode
        uint8_t in_autorotation         : 1;    // 2   // true when heli is in autorotation
    } heli_flags_t;
    heli_flags_t 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;

    bool standby_active;

    static const AP_Scheduler::Task scheduler_tasks[];
    static const AP_Param::Info var_info[];
    static const struct LogStructure log_structure[];

    // enum for ESC CALIBRATION
    enum ESCCalibrationModes : uint8_t {
        ESCCAL_NONE = 0,
        ESCCAL_PASSTHROUGH_IF_THROTTLE_HIGH = 1,
        ESCCAL_PASSTHROUGH_ALWAYS = 2,
        ESCCAL_AUTO = 3,
        ESCCAL_DISABLED = 9,
    };

    enum Failsafe_Action {
        Failsafe_Action_None           = 0,
        Failsafe_Action_Land           = 1,
        Failsafe_Action_RTL            = 2,
        Failsafe_Action_SmartRTL       = 3,
        Failsafe_Action_SmartRTL_Land  = 4,
        Failsafe_Action_Terminate      = 5
    };

    enum class FailsafeOption {
        RC_CONTINUE_IF_AUTO             = (1<<0),   // 1
        GCS_CONTINUE_IF_AUTO            = (1<<1),   // 2
        RC_CONTINUE_IF_GUIDED           = (1<<2),   // 4
        CONTINUE_IF_LANDING             = (1<<3),   // 8
        GCS_CONTINUE_IF_PILOT_CONTROL   = (1<<4),   // 16
        RELEASE_GRIPPER                 = (1<<5),   // 32
    };


    enum class FlightOptions {
        DISABLE_THRUST_LOSS_CHECK     = (1<<0),   // 1
        DISABLE_YAW_IMBALANCE_WARNING = (1<<1),   // 2
    };

    static constexpr int8_t _failsafe_priorities[] = {
                                                      Failsafe_Action_Terminate,
                                                      Failsafe_Action_Land,
                                                      Failsafe_Action_RTL,
                                                      Failsafe_Action_SmartRTL_Land,
                                                      Failsafe_Action_SmartRTL,
                                                      Failsafe_Action_None,
                                                      -1 // the priority list must end with a sentinel of -1
                                                     };

    #define FAILSAFE_LAND_PRIORITY 1
    static_assert(_failsafe_priorities[FAILSAFE_LAND_PRIORITY] == Failsafe_Action_Land,
                  "FAILSAFE_LAND_PRIORITY must match the entry in _failsafe_priorities");
    static_assert(_failsafe_priorities[ARRAY_SIZE(_failsafe_priorities) - 1] == -1,
                  "_failsafe_priorities is missing the sentinel");



    // AP_State.cpp
    void set_auto_armed(bool b);
    void set_simple_mode(SimpleMode b);
    void set_failsafe_radio(bool b);
    void set_failsafe_gcs(bool b);
    void update_using_interlock();

    // Copter.cpp
    void get_scheduler_tasks(const AP_Scheduler::Task *&tasks,
                             uint8_t &task_count,
                             uint32_t &log_bit) override;
    void fast_loop() override;
    bool start_takeoff(float alt) override;
    bool set_target_location(const Location& target_loc) override;
    bool set_target_posvel_NED(const Vector3f& target_pos, const Vector3f& target_vel) override;
    bool set_target_velocity_NED(const Vector3f& vel_ned) override;
    bool set_target_angle_and_climbrate(float roll_deg, float pitch_deg, float yaw_deg, float climb_rate_ms, bool use_yaw_rate, float yaw_rate_degs) override;
    void rc_loop();
    void throttle_loop();
    void update_batt_compass(void);
    void fourhundred_hz_logging();
    void ten_hz_logging_loop();
    void twentyfive_hz_logging();
    void three_hz_loop();
    void one_hz_loop();
    void init_simple_bearing();
    void update_simple_mode(void);
    void update_super_simple_bearing(bool force_update);
    void read_AHRS(void);
    void update_altitude();

    // Attitude.cpp
    void update_throttle_hover();
    float get_pilot_desired_climb_rate(float throttle_control);
    float get_non_takeoff_throttle();
    void set_accel_throttle_I_from_pilot_throttle();
    void rotate_body_frame_to_NE(float &x, float &y);
    uint16_t get_pilot_speed_dn() const;

    // avoidance.cpp
    void low_alt_avoidance();

#if HAL_ADSB_ENABLED
    // avoidance_adsb.cpp
    void avoidance_adsb_update(void);
#endif

    // baro_ground_effect.cpp
    void update_ground_effect_detector(void);
    void update_ekf_terrain_height_stable();

    // commands.cpp
    void update_home_from_EKF();
    void set_home_to_current_location_inflight();
    bool set_home_to_current_location(bool lock) WARN_IF_UNUSED;
    bool set_home(const Location& loc, bool lock) WARN_IF_UNUSED;
    bool far_from_EKF_origin(const Location& loc);

    // compassmot.cpp
    MAV_RESULT mavlink_compassmot(const GCS_MAVLINK &gcs_chan);

    // crash_check.cpp
    void crash_check();
    void thrust_loss_check();
    void yaw_imbalance_check();
    LowPassFilterFloat yaw_I_filt{0.05f};
    uint32_t last_yaw_warn_ms;
    void parachute_check();
    void parachute_release();
    void parachute_manual_release();

    // ekf_check.cpp
    void ekf_check();
    bool ekf_over_threshold();
    void failsafe_ekf_event();
    void failsafe_ekf_off_event(void);
    void check_ekf_reset();
    void check_vibration();

    // esc_calibration.cpp
    void esc_calibration_startup_check();
    void esc_calibration_passthrough();
    void esc_calibration_auto();
    void esc_calibration_notify();
    void esc_calibration_setup();

    // events.cpp
    bool failsafe_option(FailsafeOption opt) const;
    void failsafe_radio_on_event();
    void failsafe_radio_off_event();
    void handle_battery_failsafe(const char* type_str, const int8_t action);
    void failsafe_gcs_check();
    void failsafe_gcs_on_event(void);
    void failsafe_gcs_off_event(void);
    void failsafe_terrain_check();
    void failsafe_terrain_set_status(bool data_ok);
    void failsafe_terrain_on_event();
    void gpsglitch_check();
    void set_mode_RTL_or_land_with_pause(ModeReason reason);
    void set_mode_SmartRTL_or_RTL(ModeReason reason);
    void set_mode_SmartRTL_or_land_with_pause(ModeReason reason);
    bool should_disarm_on_failsafe();
    void do_failsafe_action(Failsafe_Action action, ModeReason reason);

    // failsafe.cpp
    void failsafe_enable();
    void failsafe_disable();
#if ADVANCED_FAILSAFE == ENABLED
    void afs_fs_check(void);
#endif

    // fence.cpp
#if AC_FENCE == ENABLED
    void fence_check();
#endif

    // heli.cpp
    void heli_init();
    void check_dynamic_flight(void);
    bool should_use_landing_swash() const;
    void update_heli_control_dynamics(void);
    void heli_update_landing_swash();
    float get_pilot_desired_rotor_speed() const;
    void heli_update_rotor_speed_targets();
    void heli_update_autorotation();
#if MODE_AUTOROTATE_ENABLED == ENABLED
    void heli_set_autorotation(bool autotrotation);
#endif
    // inertia.cpp
    void read_inertia();

    // landing_detector.cpp
    void update_land_and_crash_detectors();
    void update_land_detector();
    void set_land_complete(bool b);
    void set_land_complete_maybe(bool b);
    void update_throttle_mix();

#if LANDING_GEAR_ENABLED == ENABLED
    // landing_gear.cpp
    void landinggear_update();
#endif

    // standby.cpp
    void standby_update();

    // Log.cpp
    void Log_Write_Control_Tuning();
    void Log_Write_Attitude();
    void Log_Write_EKF_POS();
    void Log_Write_MotBatt();
    void Log_Write_Data(LogDataID id, int32_t value);
    void Log_Write_Data(LogDataID id, uint32_t value);
    void Log_Write_Data(LogDataID id, int16_t value);
    void Log_Write_Data(LogDataID id, uint16_t value);
    void Log_Write_Data(LogDataID id, float value);
    void Log_Write_Parameter_Tuning(uint8_t param, float tuning_val, float tune_min, float tune_max);
    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_SysID_Setup(uint8_t systemID_axis, float waveform_magnitude, float frequency_start, float frequency_stop, float time_fade_in, float time_const_freq, float time_record, float time_fade_out);
    void Log_Write_SysID_Data(float waveform_time, float waveform_sample, float waveform_freq, float angle_x, float angle_y, float angle_z, float accel_x, float accel_y, float accel_z);
    void Log_Write_Vehicle_Startup_Messages();
    void log_init(void);

    // mode.cpp
    bool set_mode(Mode::Number mode, ModeReason reason);
    bool set_mode(const uint8_t new_mode, const ModeReason reason) override;
    // called when an attempt to change into a mode is unsuccessful:
    void mode_change_failed(const Mode *mode, const char *reason);
    uint8_t get_mode() const override { return (uint8_t)flightmode->mode_number(); }
    void update_flight_mode();
    void notify_flight_mode();

    // mode_land.cpp
    void set_mode_land_with_pause(ModeReason reason);
    bool landing_with_GPS();

    // motor_test.cpp
    void motor_test_output();
    bool mavlink_motor_test_check(const GCS_MAVLINK &gcs_chan, bool check_rc);
    MAV_RESULT mavlink_motor_test_start(const GCS_MAVLINK &gcs_chan, uint8_t motor_seq, uint8_t throttle_type, float throttle_value, float timeout_sec, uint8_t motor_count);
    void motor_test_stop();

    // motors.cpp
    void arm_motors_check();
    void auto_disarm_check();
    void motors_output();
    void lost_vehicle_check();

    // navigation.cpp
    void run_nav_updates(void);
    int32_t home_bearing();
    uint32_t home_distance();

    // Parameters.cpp
    void load_parameters(void) override;
    void convert_pid_parameters(void);
    void convert_lgr_parameters(void);
    void convert_tradheli_parameters(void) const;
    void convert_fs_options_params(void) const;

    // precision_landing.cpp
    void init_precland();
    void update_precland();

    // radio.cpp
    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();
    int16_t get_throttle_mid(void);

    // sensors.cpp
    void read_barometer(void);
    void init_rangefinder(void);
    void read_rangefinder(void);
    bool rangefinder_alt_ok() const;
    bool rangefinder_up_ok() const;
    void rpm_update();
    void init_optflow();
    void update_optical_flow(void);
    void compass_cal_update(void);
    void accel_cal_update(void);
    void init_proximity();
    void update_proximity();

    // RC_Channel.cpp
    void save_trim();
    void auto_trim();
    void auto_trim_cancel();

    // system.cpp
    void init_ardupilot() override;
    void startup_INS_ground();
    void update_dynamic_notch() override;
    bool position_ok() const;
    bool ekf_has_absolute_position() const;
    bool ekf_has_relative_position() const;
    bool ekf_alt_ok() const;
    void update_auto_armed();
    bool should_log(uint32_t mask);
    const char* get_frame_string() const;
    void allocate_motors(void);
    bool is_tradheli() const;

    // terrain.cpp
    void terrain_update();
    void terrain_logging();

    // tuning.cpp
    void tuning();

    // UserCode.cpp
    void userhook_init();
    void userhook_FastLoop();
    void userhook_50Hz();
    void userhook_MediumLoop();
    void userhook_SlowLoop();
    void userhook_SuperSlowLoop();
    void userhook_auxSwitch1(uint8_t ch_flag);
    void userhook_auxSwitch2(uint8_t ch_flag);
    void userhook_auxSwitch3(uint8_t ch_flag);

    // vehicle specific waypoint info helpers
    bool get_wp_distance_m(float &distance) const override;
    bool get_wp_bearing_deg(float &bearing) const override;
    bool get_wp_crosstrack_error_m(float &xtrack_error) const override;

#if MODE_ACRO_ENABLED == ENABLED
#if FRAME_CONFIG == HELI_FRAME
    ModeAcro_Heli mode_acro;
#else
    ModeAcro mode_acro;
#endif
#endif
    ModeAltHold mode_althold;
#if MODE_AUTO_ENABLED == ENABLED
    ModeAuto mode_auto;
#endif
#if AUTOTUNE_ENABLED == ENABLED
    ModeAutoTune mode_autotune;
#endif
#if MODE_BRAKE_ENABLED == ENABLED
    ModeBrake mode_brake;
#endif
#if MODE_CIRCLE_ENABLED == ENABLED
    ModeCircle mode_circle;
#endif
#if MODE_DRIFT_ENABLED == ENABLED
    ModeDrift mode_drift;
#endif
#if MODE_FLIP_ENABLED == ENABLED
    ModeFlip mode_flip;
#endif
#if MODE_FOLLOW_ENABLED == ENABLED
    ModeFollow mode_follow;
#endif
#if MODE_GUIDED_ENABLED == ENABLED
    ModeGuided mode_guided;
#endif
    ModeLand mode_land;
#if MODE_LOITER_ENABLED == ENABLED
    ModeLoiter mode_loiter;
#endif
#if MODE_POSHOLD_ENABLED == ENABLED
    ModePosHold mode_poshold;
#endif
#if MODE_RTL_ENABLED == ENABLED
    ModeRTL mode_rtl;
#endif
#if FRAME_CONFIG == HELI_FRAME
    ModeStabilize_Heli mode_stabilize;
#else
    ModeStabilize mode_stabilize;
#endif
#if MODE_SPORT_ENABLED == ENABLED
    ModeSport mode_sport;
#endif
#if MODE_SYSTEMID_ENABLED == ENABLED
    ModeSystemId mode_systemid;
#endif
#if HAL_ADSB_ENABLED
    ModeAvoidADSB mode_avoid_adsb;
#endif
#if MODE_THROW_ENABLED == ENABLED
    ModeThrow mode_throw;
#endif
#if MODE_GUIDED_NOGPS_ENABLED == ENABLED
    ModeGuidedNoGPS mode_guided_nogps;
#endif
#if MODE_SMARTRTL_ENABLED == ENABLED
    ModeSmartRTL mode_smartrtl;
#endif
#if !HAL_MINIMIZE_FEATURES && OPTFLOW == ENABLED
    ModeFlowHold mode_flowhold;
#endif
#if MODE_ZIGZAG_ENABLED == ENABLED
    ModeZigZag mode_zigzag;
#endif
#if MODE_AUTOROTATE_ENABLED == ENABLED
    ModeAutorotate mode_autorotate;
#endif

    // mode.cpp
    Mode *mode_from_mode_num(const Mode::Number mode);
    void exit_mode(Mode *&old_flightmode, Mode *&new_flightmode);

public:
    void failsafe_check();      // failsafe.cpp
};

extern Copter copter;

using AP_HAL::millis;
using AP_HAL::micros;