ardupilot/ArduCopter/mode_flowhold.cpp

#include "Copter.h"
#include <utility>

#if !HAL_MINIMIZE_FEATURES && OPTFLOW == ENABLED

/*
  implement FLOWHOLD mode, for position hold using optical flow
  without rangefinder
 */

const AP_Param::GroupInfo Copter::ModeFlowHold::var_info[] = {
    // @Param: _XY_P
    // @DisplayName: FlowHold P gain
    // @Description: FlowHold (horizontal) P gain.
    // @Range: 0.1 6.0
    // @Increment: 0.1
    // @User: Advanced

    // @Param: _XY_I
    // @DisplayName: FlowHold I gain
    // @Description: FlowHold (horizontal) I gain
    // @Range: 0.02 1.00
    // @Increment: 0.01
    // @User: Advanced

    // @Param: _XY_IMAX
    // @DisplayName: FlowHold Integrator Max
    // @Description: FlowHold (horizontal) integrator maximum
    // @Range: 0 4500
    // @Increment: 10
    // @Units: cdeg
    // @User: Advanced

    // @Param: _XY_FILT_HZ
    // @DisplayName: FlowHold filter on input to control
    // @Description: FlowHold (horizontal) filter on input to control
    // @Range: 0 100
    // @Units: Hz
    // @User: Advanced
    AP_SUBGROUPINFO(flow_pi_xy, "_XY_",  1, Copter::ModeFlowHold, AC_PI_2D),

    // @Param: _FLOW_MAX
    // @DisplayName: FlowHold Flow Rate Max
    // @Description: Controls maximum apparent flow rate in flowhold
    // @Range: 0.1 2.5
    // @User: Standard
    AP_GROUPINFO("_FLOW_MAX", 2, Copter::ModeFlowHold, flow_max, 0.6),

    // @Param: _FILT_HZ
    // @DisplayName: FlowHold Filter Frequency
    // @Description: Filter frequency for flow data
    // @Range: 1 100
    // @Units: Hz
    // @User: Standard
    AP_GROUPINFO("_FILT_HZ", 3, Copter::ModeFlowHold, flow_filter_hz, 5),

    // @Param: _QUAL_MIN
    // @DisplayName: FlowHold Flow quality minimum
    // @Description: Minimum flow quality to use flow position hold
    // @Range: 0 255
    // @User: Standard
    AP_GROUPINFO("_QUAL_MIN", 4, Copter::ModeFlowHold, flow_min_quality, 10),

    // 5 was FLOW_SPEED

    // @Param: _BRAKE_RATE
    // @DisplayName: FlowHold Braking rate
    // @Description: Controls deceleration rate on stick release
    // @Range: 1 30
    // @User: Standard
    // @Units: deg/s
    AP_GROUPINFO("_BRAKE_RATE", 6, Copter::ModeFlowHold, brake_rate_dps, 8),

    AP_GROUPEND
};

Copter::ModeFlowHold::ModeFlowHold(void) : Mode()
{
    AP_Param::setup_object_defaults(this, var_info);            
}

#define CONTROL_FLOWHOLD_EARTH_FRAME 0

// flowhold_init - initialise flowhold controller
bool Copter::ModeFlowHold::init(bool ignore_checks)
{
#if FRAME_CONFIG == HELI_FRAME
    // do not allow helis to enter Flow Hold if the Rotor Runup is not complete
    if (!ignore_checks && !motors->rotor_runup_complete()){
        return false;
    }
#endif

    if (!copter.optflow.enabled() || !copter.optflow.healthy()) {
        return false;
    }

    // initialize vertical speeds and leash lengths
    copter.pos_control->set_max_speed_z(-get_pilot_speed_dn(), copter.g.pilot_speed_up);
    copter.pos_control->set_max_accel_z(copter.g.pilot_accel_z);

    // initialise position and desired velocity
    if (!copter.pos_control->is_active_z()) {
        copter.pos_control->set_alt_target_to_current_alt();
        copter.pos_control->set_desired_velocity_z(copter.inertial_nav.get_velocity_z());
    }

    flow_filter.set_cutoff_frequency(copter.scheduler.get_loop_rate_hz(), flow_filter_hz.get());

    quality_filtered = 0;
    flow_pi_xy.reset_I();
    limited = false;

    flow_pi_xy.set_dt(1.0/copter.scheduler.get_loop_rate_hz());

    // start with INS height
    last_ins_height = copter.inertial_nav.get_altitude() * 0.01;
    height_offset = 0;

    return true;
}

/*
  calculate desired attitude from flow sensor. Called when flow sensor is healthy
 */
void Copter::ModeFlowHold::flowhold_flow_to_angle(Vector2f &bf_angles, bool stick_input)
{
    uint32_t now = AP_HAL::millis();

    // get corrected raw flow rate
    Vector2f raw_flow = copter.optflow.flowRate() - copter.optflow.bodyRate();

    // limit sensor flow, this prevents oscillation at low altitudes
    raw_flow.x = constrain_float(raw_flow.x, -flow_max, flow_max);
    raw_flow.y = constrain_float(raw_flow.y, -flow_max, flow_max);

    // filter the flow rate
    Vector2f sensor_flow = flow_filter.apply(raw_flow);

    // scale by height estimate, limiting it to height_min to height_max
    float ins_height = copter.inertial_nav.get_altitude() * 0.01;
    float height_estimate = ins_height + height_offset;

    // compensate for height, this converts to (approx) m/s
    sensor_flow *= constrain_float(height_estimate, height_min, height_max);

    // rotate controller input to earth frame
    Vector2f input_ef = copter.ahrs.rotate_body_to_earth2D(sensor_flow);

    // run PI controller
    flow_pi_xy.set_input(input_ef);

    // get earth frame controller attitude in centi-degrees
    Vector2f ef_output;

    // get P term
    ef_output = flow_pi_xy.get_p();

    if (stick_input) {
        last_stick_input_ms = now;
        braking = true;
    }
    if (!stick_input && braking) {
        // stop braking if either 3s has passed, or we have slowed below 0.3m/s
        if (now - last_stick_input_ms > 3000 || sensor_flow.length() < 0.3) {
            braking = false;
#if 0
            printf("braking done at %u vel=%f\n", now - last_stick_input_ms,
                   (double)sensor_flow.length());
#endif
        }
    }

    if (!stick_input && !braking) {
        // get I term
        if (limited) {
            // only allow I term to shrink in length
            xy_I = flow_pi_xy.get_i_shrink();
        } else {
            // normal I term operation
            xy_I = flow_pi_xy.get_pi();
        }
    }

    if (!stick_input && braking) {
        // calculate brake angle for each axis separately
        for (uint8_t i=0; i<2; i++) {
            float &velocity = sensor_flow[i];
            float abs_vel_cms = fabsf(velocity)*100;
            const float brake_gain = (15.0f * brake_rate_dps.get() + 95.0f) / 100.0f;
            float lean_angle_cd = brake_gain * abs_vel_cms * (1.0f+500.0f/(abs_vel_cms+60.0f));
            if (velocity < 0) {
                lean_angle_cd = -lean_angle_cd;
            }
            bf_angles[i] = lean_angle_cd;
        }
        ef_output.zero();
    }

    ef_output += xy_I;
    ef_output *= copter.aparm.angle_max;

    // convert to body frame
    bf_angles += copter.ahrs.rotate_earth_to_body2D(ef_output);

    // set limited flag to prevent integrator windup
    limited = fabsf(bf_angles.x) > copter.aparm.angle_max || fabsf(bf_angles.y) > copter.aparm.angle_max;

    // constrain to angle limit
    bf_angles.x = constrain_float(bf_angles.x, -copter.aparm.angle_max, copter.aparm.angle_max);
    bf_angles.y = constrain_float(bf_angles.y, -copter.aparm.angle_max, copter.aparm.angle_max);

    if (log_counter++ % 20 == 0) {
        DataFlash_Class::instance()->Log_Write("FHLD", "TimeUS,SFx,SFy,Ax,Ay,Qual,Ix,Iy", "Qfffffff",
                                               AP_HAL::micros64(),
                                               (double)sensor_flow.x, (double)sensor_flow.y,
                                               (double)bf_angles.x, (double)bf_angles.y,
                                               (double)quality_filtered,
                                               (double)xy_I.x, (double)xy_I.y);
    }
}

// flowhold_run - runs the flowhold controller
// should be called at 100hz or more
void Copter::ModeFlowHold::run()
{
    FlowHoldModeState flowhold_state;
    float takeoff_climb_rate = 0.0f;

    update_height_estimate();

    // initialize vertical speeds and acceleration
    copter.pos_control->set_max_speed_z(-get_pilot_speed_dn(), copter.g.pilot_speed_up);
    copter.pos_control->set_max_accel_z(copter.g.pilot_accel_z);

    // apply SIMPLE mode transform to pilot inputs
    copter.update_simple_mode();

    // check for filter change
    if (!is_equal(flow_filter.get_cutoff_freq(), flow_filter_hz.get())) {
        flow_filter.set_cutoff_frequency(flow_filter_hz.get());
    }

    // get pilot desired climb rate
    float target_climb_rate = copter.get_pilot_desired_climb_rate(copter.channel_throttle->get_control_in());
    target_climb_rate = constrain_float(target_climb_rate, -get_pilot_speed_dn(), copter.g.pilot_speed_up);

    // get pilot's desired yaw rate
    float target_yaw_rate = copter.get_pilot_desired_yaw_rate(copter.channel_yaw->get_control_in());

    if (!copter.motors->armed() || !copter.motors->get_interlock()) {
        flowhold_state = FlowHold_MotorStopped;
    } else if (takeoff.running() || takeoff.triggered(target_climb_rate)) {
        flowhold_state = FlowHold_Takeoff;
    } else if (!copter.ap.auto_armed || copter.ap.land_complete) {
        flowhold_state = FlowHold_Landed;
    } else {
        flowhold_state = FlowHold_Flying;
    }

    if (copter.optflow.healthy()) {
        const float filter_constant = 0.95;
        quality_filtered = filter_constant * quality_filtered + (1-filter_constant) * copter.optflow.quality();
    } else {
        quality_filtered = 0;
    }

    Vector2f bf_angles;

    // calculate alt-hold angles
    int16_t roll_in = copter.channel_roll->get_control_in();
    int16_t pitch_in = copter.channel_pitch->get_control_in();
    float angle_max = copter.attitude_control->get_althold_lean_angle_max();
    get_pilot_desired_lean_angles(bf_angles.x, bf_angles.y,angle_max, attitude_control->get_althold_lean_angle_max());

    if (quality_filtered >= flow_min_quality &&
        AP_HAL::millis() - copter.arm_time_ms > 3000) {
        // don't use for first 3s when we are just taking off
        Vector2f flow_angles;

        flowhold_flow_to_angle(flow_angles, (roll_in != 0) || (pitch_in != 0));
        flow_angles.x = constrain_float(flow_angles.x, -angle_max/2, angle_max/2);
        flow_angles.y = constrain_float(flow_angles.y, -angle_max/2, angle_max/2);
        bf_angles += flow_angles;
    }
    bf_angles.x = constrain_float(bf_angles.x, -angle_max, angle_max);
    bf_angles.y = constrain_float(bf_angles.y, -angle_max, angle_max);

    // Flow Hold State Machine
    switch (flowhold_state) {

    case FlowHold_MotorStopped:

        copter.motors->set_desired_spool_state(AP_Motors::DESIRED_SHUT_DOWN);
        copter.attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(bf_angles.x, bf_angles.y, target_yaw_rate);
#if FRAME_CONFIG == HELI_FRAME    
        // force descent rate and call position controller
        copter.pos_control->set_alt_target_from_climb_rate(-abs(copter.g.land_speed), copter.G_Dt, false);
#else
        copter.attitude_control->reset_rate_controller_I_terms();
        copter.attitude_control->set_yaw_target_to_current_heading();
        copter.pos_control->relax_alt_hold_controllers(0.0f);   // forces throttle output to go to zero
#endif
        flow_pi_xy.reset_I();
        copter.pos_control->update_z_controller();
        break;

    case FlowHold_Takeoff:
        // set motors to full range
        copter.motors->set_desired_spool_state(AP_Motors::DESIRED_THROTTLE_UNLIMITED);

        // initiate take-off
        if (!takeoff.running()) {
            takeoff.start(constrain_float(g.pilot_takeoff_alt,0.0f,1000.0f));
            // indicate we are taking off
            copter.set_land_complete(false);
            // clear i terms
            copter.set_throttle_takeoff();
        }

        // get take-off adjusted pilot and takeoff climb rates
        takeoff.get_climb_rates(target_climb_rate, takeoff_climb_rate);

        // get avoidance adjusted climb rate
        target_climb_rate = copter.get_avoidance_adjusted_climbrate(target_climb_rate);

        // call attitude controller
        copter.attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(bf_angles.x, bf_angles.y, target_yaw_rate);

        // call position controller
        copter.pos_control->set_alt_target_from_climb_rate_ff(target_climb_rate, copter.G_Dt, false);
        copter.pos_control->add_takeoff_climb_rate(takeoff_climb_rate, copter.G_Dt);
        copter.pos_control->update_z_controller();
        break;

    case FlowHold_Landed:
        // set motors to spin-when-armed if throttle below deadzone, otherwise full range (but motors will only spin at min throttle)
        if (target_climb_rate < 0.0f) {
            copter.motors->set_desired_spool_state(AP_Motors::DESIRED_SPIN_WHEN_ARMED);
        } else {
            copter.motors->set_desired_spool_state(AP_Motors::DESIRED_THROTTLE_UNLIMITED);
        }

        copter.attitude_control->reset_rate_controller_I_terms();
        copter.attitude_control->set_yaw_target_to_current_heading();
        copter.attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(bf_angles.x, bf_angles.y, target_yaw_rate);
        copter.pos_control->relax_alt_hold_controllers(0.0f);   // forces throttle output to go to zero
        copter.pos_control->update_z_controller();
        break;

    case FlowHold_Flying:
        copter.motors->set_desired_spool_state(AP_Motors::DESIRED_THROTTLE_UNLIMITED);

#if AC_AVOID_ENABLED == ENABLED
        // apply avoidance
        copter.avoid.adjust_roll_pitch(bf_angles.x, bf_angles.y, copter.aparm.angle_max);
#endif

        // call attitude controller
        copter.attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(bf_angles.x, bf_angles.y, target_yaw_rate);

        // adjust climb rate using rangefinder
        target_climb_rate = copter.get_surface_tracking_climb_rate(target_climb_rate, copter.pos_control->get_alt_target(), copter.G_Dt);

        // get avoidance adjusted climb rate
        target_climb_rate = copter.get_avoidance_adjusted_climbrate(target_climb_rate);

        // call position controller
        copter.pos_control->set_alt_target_from_climb_rate_ff(target_climb_rate, copter.G_Dt, false);
        copter.pos_control->update_z_controller();
        break;
    }
}

/*
  update height estimate using integrated accelerometer ratio with optical flow
 */
void Copter::ModeFlowHold::update_height_estimate(void)
{
    float ins_height = copter.inertial_nav.get_altitude() * 0.01;

#if 1
    // assume on ground when disarmed, or if we have only just started spooling the motors up
    if (!hal.util->get_soft_armed() ||
        copter.motors->get_desired_spool_state() != AP_Motors::DESIRED_THROTTLE_UNLIMITED ||
        AP_HAL::millis() - copter.arm_time_ms < 1500) {
        height_offset = -ins_height;
        last_ins_height = ins_height;
        return;
    }
#endif

    // get delta velocity in body frame
    Vector3f delta_vel;
    if (!copter.ins.get_delta_velocity(delta_vel)) {
        return;
    }

    // integrate delta velocity in earth frame
    const Matrix3f &rotMat = copter.ahrs.get_rotation_body_to_ned();
    delta_vel = rotMat * delta_vel;
    delta_velocity_ne.x += delta_vel.x;
    delta_velocity_ne.y += delta_vel.y;

    if (!copter.optflow.healthy()) {
        // can't update height model with no flow sensor
        last_flow_ms = AP_HAL::millis();
        delta_velocity_ne.zero();
        return;
    }

    if (last_flow_ms == 0) {
        // just starting up
        last_flow_ms = copter.optflow.last_update();
        delta_velocity_ne.zero();
        height_offset = 0;
        return;
    }

    if (copter.optflow.last_update() == last_flow_ms) {
        // no new flow data
        return;
    }

    // convert delta velocity back to body frame to match the flow sensor
    Vector2f delta_vel_bf = copter.ahrs.rotate_earth_to_body2D(delta_velocity_ne);

    // and convert to an rate equivalent, to be comparable to flow
    Vector2f delta_vel_rate(-delta_vel_bf.y, delta_vel_bf.x);

    // get body flow rate in radians per second
    Vector2f flow_rate_rps = copter.optflow.flowRate() - copter.optflow.bodyRate();

    uint32_t dt_ms = copter.optflow.last_update() - last_flow_ms;
    if (dt_ms > 500) {
        // too long between updates, ignore
        last_flow_ms = copter.optflow.last_update();
        delta_velocity_ne.zero();
        last_flow_rate_rps = flow_rate_rps;
        last_ins_height = ins_height;
        height_offset = 0;
        return;        
    }

    /*
      basic equation is:
      height_m = delta_velocity_mps / delta_flowrate_rps;
     */

    // get delta_flowrate_rps
    Vector2f delta_flowrate = flow_rate_rps - last_flow_rate_rps;
    last_flow_rate_rps = flow_rate_rps;
    last_flow_ms = copter.optflow.last_update();

    /*
      update height estimate
     */
    const float min_velocity_change = 0.04;
    const float min_flow_change = 0.04;
    const float height_delta_max = 0.25;

    /*
      for each axis update the height estimate
     */
    float delta_height = 0;
    uint8_t total_weight = 0;
    float height_estimate = ins_height + height_offset;

    for (uint8_t i=0; i<2; i++) {
        // only use height estimates when we have significant delta-velocity and significant delta-flow
        float abs_flow = fabsf(delta_flowrate[i]);
        if (abs_flow < min_flow_change ||
            fabsf(delta_vel_rate[i]) < min_velocity_change) {
            continue;
        }
        // get instantaneous height estimate
        float height = delta_vel_rate[i] / delta_flowrate[i];
        if (height <= 0) {
            // discard negative heights
            continue;
        }
        delta_height += (height - height_estimate) * abs_flow;
        total_weight += abs_flow;
    }
    if (total_weight > 0) {
        delta_height /= total_weight;
    }

    if (delta_height < 0) {
        // bias towards lower heights, as we'd rather have too low
        // gain than have oscillation. This also compensates a bit for
        // the discard of negative heights above
        delta_height *= 2;
    }

    // don't update height by more than height_delta_max, this is a simple way of rejecting noise
    float new_offset = height_offset + constrain_float(delta_height, -height_delta_max, height_delta_max);

    // apply a simple filter
    height_offset = 0.8 * height_offset + 0.2 * new_offset;

    if (ins_height + height_offset < height_min) {
        // height estimate is never allowed below the minimum
        height_offset = height_min - ins_height;
    }

    // new height estimate for logging
    height_estimate = ins_height + height_offset;

    DataFlash_Class::instance()->Log_Write("FXY", "TimeUS,DFx,DFy,DVx,DVy,Hest,DH,Hofs,InsH,LastInsH,DTms", "QfffffffffI",
                                           AP_HAL::micros64(),
                                           (double)delta_flowrate.x,
                                           (double)delta_flowrate.y,
                                           (double)delta_vel_rate.x,
                                           (double)delta_vel_rate.y,
                                           (double)height_estimate,
                                           (double)delta_height,
                                           (double)height_offset,
                                           (double)ins_height,
                                           (double)last_ins_height,
                                           dt_ms);
    gcs().send_named_float("HEST", height_estimate);
    delta_velocity_ne.zero();
    last_ins_height = ins_height;
}

#endif // OPTFLOW == ENABLED