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

/*
 * control_drift.pde - init and run calls for drift flight mode
 */

#ifndef DRIFT_SPEEDGAIN
 # define DRIFT_SPEEDGAIN 14.0f
#endif

#ifndef DRIFT_THR_ASSIST_GAIN
 # define DRIFT_THR_ASSIST_GAIN 1.8f    // gain controlling amount of throttle assistance
#endif

#ifndef DRIFT_THR_ASSIST_MAX
 # define DRIFT_THR_ASSIST_MAX  300.0f  // maximum assistance throttle assist will provide
#endif

#ifndef DRIFT_THR_MIN
 # define DRIFT_THR_MIN         213     // throttle assist will be active when pilot's throttle is above this value
#endif
#ifndef DRIFT_THR_MAX
 # define DRIFT_THR_MAX         787     // throttle assist will be active when pilot's throttle is below this value
#endif

// drift_init - initialise drift controller
static bool drift_init(bool ignore_checks)
{
    if (GPS_ok() || ignore_checks) {
        return true;
    }else{
        return false;
    }
}

// drift_run - runs the drift controller
// should be called at 100hz or more
static void drift_run()
{
    static float breaker = 0.0;
    int16_t target_roll, target_pitch;
    float target_yaw_rate;
    int16_t pilot_throttle_scaled;

    // if not armed or landed and throttle at zero, set throttle to zero and exit immediately
    if(!motors.armed() || (ap.land_complete && g.rc_3.control_in <= 0)) {
        attitude_control.init_targets();
        attitude_control.set_throttle_out(0, false);
        return;
    }

    // convert pilot input to lean angles
    get_pilot_desired_lean_angles(g.rc_1.control_in, g.rc_2.control_in, target_roll, target_pitch);

    // get pilot's desired throttle
    pilot_throttle_scaled = get_pilot_desired_throttle(g.rc_3.control_in);

    // Grab inertial velocity
    const Vector3f& vel = inertial_nav.get_velocity();

    // rotate roll, pitch input from north facing to vehicle's perspective
    float roll_vel =  vel.y * ahrs.cos_yaw() - vel.x * ahrs.sin_yaw(); // body roll vel
    float pitch_vel = vel.y * ahrs.sin_yaw() + vel.x * ahrs.cos_yaw(); // body pitch vel

    float pitch_vel2 = min(fabs(pitch_vel), 800);

    // simple gain scheduling for yaw input
    target_yaw_rate = (float)(target_roll/2) * (1.0 - (pitch_vel2 / 2400.0));

    roll_vel = constrain_float(roll_vel, -322, 322);
    pitch_vel = constrain_float(pitch_vel, -322, 322);

    // always limit roll
    target_roll = roll_vel * -DRIFT_SPEEDGAIN;

    // If we let go of sticks, bring us to a stop
    if(target_pitch == 0){
        // .14/ (.03 * 100) = 4.6 seconds till full breaking
        breaker += .03;
        breaker = min(breaker, DRIFT_SPEEDGAIN);
        target_pitch = pitch_vel * breaker;
    }else{
        breaker = 0.0;
    }

    // throttle assist - adjusts throttle to slow the vehicle's vertical velocity
    //      Only active when pilot's throttle is between 213 ~ 787
    //      Assistance is strongest when throttle is at mid, drops linearly to no assistance at 213 and 787
    float thr_assist = 0.0f;
    if (pilot_throttle_scaled > g.throttle_min && pilot_throttle_scaled < g.throttle_max &&
        pilot_throttle_scaled > DRIFT_THR_MIN && pilot_throttle_scaled < DRIFT_THR_MAX) {
        // calculate throttle assist gain
        thr_assist = 1.2 - ((float)abs(pilot_throttle_scaled - 500) / 240.0f);
        thr_assist = constrain_float(thr_assist, 0.0f, 1.0f) * -DRIFT_THR_ASSIST_GAIN * vel.z;

        // ensure throttle assist never adjusts the throttle by more than 300 pwm
        thr_assist = constrain_float(thr_assist, -DRIFT_THR_ASSIST_MAX, DRIFT_THR_ASSIST_MAX);

        // ensure throttle assist never pushes throttle below throttle_min or above throttle_max
        thr_assist = constrain_float(thr_assist, g.throttle_min - pilot_throttle_scaled, g.throttle_max - pilot_throttle_scaled);
    }

    // call attitude controller
    attitude_control.angle_ef_roll_pitch_rate_ef_yaw_smooth(target_roll, target_pitch, target_yaw_rate, get_smoothing_gain());

    // output pilot's throttle with angle boost
    attitude_control.set_throttle_out(pilot_throttle_scaled + thr_assist, true);
}