ardupilot/libraries/AC_AttitudeControl/AC_AttitudeControl.h

// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: t -*-

/// @file    AC_AttitudeControl.h
/// @brief   ArduCopter attitude control library

#ifndef AC_AttitudeControl_H
#define AC_AttitudeControl_H

#include <AP_Common.h>
#include <AP_Param.h>
#include <AP_Math.h>
#include <AP_InertialSensor.h>
#include <AP_AHRS.h>
#include <AP_Motors.h>
#include <DataFlash.h>
#include <AC_PID.h>
#include <APM_PI.h>

// To-Do: change the name or move to AP_Math?
#define AC_ATTITUDE_CONTROL_DEGX100 5729.57795f             // constant to convert from radians to centi-degrees
#define AC_ATTITUDE_RATE_CONTROLLER_TIMEOUT 1.0f            // body-frame rate controller timeout in seconds
#define AC_ATTITUDE_RATE_RP_CONTROLLER_OUT_MAX 5000.0f      // body-frame rate controller maximum output (for roll-pitch axis)
#define AC_ATTITUDE_RATE_YAW_CONTROLLER_OUT_MAX 4500.0f     // body-frame rate controller maximum output (for yaw axis)
#define AC_ATTITUDE_ANGLE_YAW_CONTROLLER_OUT_MAX 4500.0f    // earth-frame angle controller maximum output (for yaw axis)
#define AC_ATTITUDE_ANGLE_CONTROLLER_ANGLE_MAX 4500.0f      // earth-frame angle controller maximum input angle (To-Do: replace with reference to aparm.angle_max)

#define AC_ATTITUDE_RATE_STAB_ROLL_OVERSHOOT_ANGLE_MAX  3000.0f // earth-frame rate stabilize controller's maximum overshoot angle
#define AC_ATTITUDE_RATE_STAB_PITCH_OVERSHOOT_ANGLE_MAX 3000.0f // earth-frame rate stabilize controller's maximum overshoot angle
#define AC_ATTITUDE_RATE_STAB_YAW_OVERSHOOT_ANGLE_MAX   1000.0f // earth-frame rate stabilize controller's maximum overshoot angle

#define AC_ATTITUDE_100HZ_DT                            0.0100f // delta time in seconds for 100hz update rate
#define AC_ATTITUDE_400HZ_DT                            0.0025f // delta time in seconds for 400hz update rate

class AC_AttitudeControl {
public:
	AC_AttitudeControl( AP_AHRS &ahrs,
                        AP_InertialSensor& ins,
                        const AP_Vehicle::MultiCopter &parms,
                        AP_Motors& motors,
                        APM_PI& pi_angle_roll, APM_PI& pi_angle_pitch, APM_PI& pi_angle_yaw,
                        AC_PID& pid_rate_roll, AC_PID& pid_rate_pitch, AC_PID& pid_rate_yaw,
                        int16_t& motor_roll, int16_t& motor_pitch, int16_t& motor_yaw, int16_t& motor_throttle
                        ) :
		_ahrs(ahrs),
        _ins(ins),
        aparm(parms),
        _motors(motors),
        _pi_angle_roll(pi_angle_roll),
        _pi_angle_pitch(pi_angle_pitch),
        _pi_angle_yaw(pi_angle_yaw),
        _pid_rate_roll(pid_rate_roll),
        _pid_rate_pitch(pid_rate_pitch),
        _pid_rate_yaw(pid_rate_yaw),
        _motor_roll(motor_roll),
        _motor_pitch(motor_pitch),
        _motor_yaw(motor_yaw),
        _motor_throttle(motor_throttle),
        _dt(AC_ATTITUDE_100HZ_DT),
        _angle_boost(0),
        _cos_roll(1.0),
        _cos_pitch(1.0),
        _sin_roll(0.0),
        _sin_pitch(0.0)
		{
			AP_Param::setup_object_defaults(this, var_info);
		}

    //
    // initialisation functions
    //

    // set_dt - sets time delta in seconds for all controllers (i.e. 100hz = 0.01, 400hz = 0.0025)
    void set_dt(float delta_sec) { _dt = delta_sec; }
    float get_dt() { return _dt; }

    //
    // angle controller (earth-frame) methods
    //

    // angle_ef_targets - get and set angle controller earth-frame-targets
    Vector3f angle_ef_targets() const { return _angle_ef_target; }
    void angle_ef_targets(Vector3f& angle_cd) { _angle_ef_target = angle_cd; }

    // angle_to_rate_ef_roll - converts earth-frame angle targets to earth-frame rate targets for roll, pitch and yaw axis
    //   targets angles in centi-degrees should be placed in _angle_ef_targets
    //   results in centi-degrees/sec put directly into _rate_ef_target
    void angle_to_rate_ef_roll();
    void angle_to_rate_ef_pitch();
    void angle_to_rate_ef_yaw();

    //
    // stabilized rate controller (earth-frame) methods
    //

    // rate_stab_ef_targets - gets and sets the stabilized rate controller earth-frame targets
    // stabilized rate controllers are better at maintaining a desired rate than the simpler earth-frame rate controllers
    // because they also maintain angle-targets and increase/decrease the rate request passed to the earth-frame rate controller
    // upon the errors between the actual angle and angle-target.
    // 
    Vector3f rate_stab_ef_targets() const { return _rate_stab_ef_target; }
    void rate_stab_ef_targets(Vector3f& rates_cds) { _rate_stab_ef_target = rates_cds; }

    // rate_stab_ef_to_rate_ef_roll - converts earth-frame stabilized rate targets to regular earth-frame rate targets for roll, pitch and yaw axis
    //   targets rates in centi-degrees/second taken from _rate_stab_ef_target
    //   results in centi-degrees/sec put into _rate_ef_target
    void rate_stab_ef_to_rate_ef_roll();
    void rate_stab_ef_to_rate_ef_pitch();
    void rate_stab_ef_to_rate_ef_yaw();

    //
    // stabilized rate controller (body-frame) methods
    //

    // rate_stab_bf_targets - gets and sets the stabilized rate controller body-frame targets
    Vector3f rate_stab_bf_targets() const { return _rate_stab_bf_target; }
    void rate_stab_bf_targets(Vector3f& rates_cds) { _rate_stab_bf_target = rates_cds; }

    // rate_stab_bf_to_rate_ef_roll - converts body-frame stabilized rate targets to regular body-frame rate targets for roll, pitch and yaw axis
    //   targets rates in centi-degrees/second taken from _rate_stab_bf_target
    //   results in centi-degrees/sec put into _rate_bf_target
    void rate_stab_bf_to_rate_bf_roll();
    void rate_stab_bf_to_rate_bf_pitch();
    void rate_stab_bf_to_rate_bf_yaw();

    //
    // rate controller (earth-frame) methods
    //

    // rate_ef_targets - gets and sets rate controller earth-frame-targets
    Vector3f rate_ef_targets() const { return _rate_ef_target; }
    void rate_ef_targets(Vector3f& rates_cds) { _rate_ef_target = rates_cds; }

    // rate_ef_targets_to_bf - converts earth frame rate targets to body frame rate targets
    void rate_ef_targets_to_bf();

    
    //
    // rate controller (body-frame) methods
    //

    // rate_bf_targets - gets and sets rate controller body-frame targets
    // To-Do: can we return these Vector3fs by reference?  i.e. using "&"?
    Vector3f rate_bf_targets() const { return _rate_bf_target; }
    void rate_bf_targets(Vector3f& rates_cds) { _rate_bf_target = rates_cds; }

	// rate_controller_run - run lowest level body-frame rate controller and send outputs to the motors
	// should be called at 100hz or more
	void rate_controller_run();

    //
    // throttle functions
    //

     // set_throttle_out - to be called by upper throttle controllers when they wish to provide throttle output directly to motors
     // provide 0 to cut motors
     void set_throttle_out(int16_t throttle_pwm, bool apply_angle_boost);

     // angle_boost - accessor for angle boost so it can be logged
     int16_t angle_boost() const { return _angle_boost; }

    //
    // helper functions
    //

    /// set_cos_sin_yaw - short-cut to save on calculations to convert from roll-pitch frame to lat-lon frame
    /// To-Do: make these references or calculate in ahrs
    void set_cos_sin_yaw(float cos_roll, float cos_pitch, float sin_roll, float sin_pitch) {
        _cos_roll = cos_roll;
        _cos_pitch = cos_pitch;
        _sin_roll = sin_roll;
        _sin_pitch = sin_pitch;
    }

    // user settable parameters
    static const struct AP_Param::GroupInfo var_info[];

private:

    //
    // body-frame rate controller
    //
	// rate_bf_to_motor_roll - ask the rate controller to calculate the motor outputs to achieve the target body-frame rate (in centi-degrees/sec) for roll, pitch and yaw
    float rate_bf_to_motor_roll(float rate_target_cds);
    float rate_bf_to_motor_pitch(float rate_target_cds);
    float rate_bf_to_motor_yaw(float rate_target_cds);

    //
    // throttle methods
    //

    // get_angle_boost - calculate total body frame throttle required to produce the given earth frame throttle
    int16_t get_angle_boost(int16_t throttle_pwm);

    //
    // logging
    //

    // log data on internal state of the controller. Called at 10Hz
    void log_data(DataFlash_Class &dataflash, uint8_t msgid);

    // dataflash logging packet
    struct PACKED log_Attitude {
        LOG_PACKET_HEADER;
        int16_t roll_in;
        int16_t roll;
        int16_t pitch_in;
        int16_t pitch;
        int16_t yaw_in;
        uint16_t yaw;
        uint16_t nav_yaw;
    } log_ACAttControl;

    // references to external libraries
    AP_AHRS&            _ahrs;
    AP_InertialSensor&  _ins;
    const AP_Vehicle::MultiCopter &aparm;
    AP_Motors&          _motors;
    APM_PI&	            _pi_angle_roll;
    APM_PI&	            _pi_angle_pitch;
    APM_PI&	            _pi_angle_yaw;
    AC_PID&             _pid_rate_roll;
    AC_PID&             _pid_rate_pitch;
    AC_PID&             _pid_rate_yaw;
    int16_t&            _motor_roll;            // g.rc_1.servo_out
    int16_t&            _motor_pitch;           // g.rc_2.servo_out
    int16_t&            _motor_yaw;             // g.rc_4.servo_out
    int16_t&            _motor_throttle;        // g.rc_3.servo_out

    // parameters
    AP_Float            _dummy_param;

    // internal variables
    // To-Do: make rate targets a typedef instead of Vector3f?
    float               _dt;                    // time delta in seconds
    Vector3f            _angle_ef_target;       // angle controller earth-frame targets
    Vector3f            _rate_stab_ef_target;   // stabilized rate controller earth-frame rate targets
    Vector3f            _rate_ef_target;        // rate controller earth-frame targets
    Vector3f            _rate_stab_bf_target;   // stabilized rate controller body-frame rate targets
    Vector3f            _rate_stab_bf_error;    // stabilized rate controller body-frame angle errors
    Vector3f            _rate_bf_target;        // rate controller body-frame targets
    int16_t             _angle_boost;           // used only for logging

    // precalculated values for efficiency saves
    // To-Do: could these be changed to references and passed into the constructor?
    float _cos_roll;
    float _cos_pitch;
    float _sin_roll;
    float _sin_pitch;
};

#define AC_ATTITUDE_CONTROL_LOG_FORMAT(msg) { msg, sizeof(AC_AttitudeControl::log_Attitude),	\
                            "ATT", "cccccCC",      "RollIn,Roll,PitchIn,Pitch,YawIn,Yaw,NavYaw" }

#endif //AC_AttitudeControl_H