mirror of https://github.com/ArduPilot/ardupilot
524 lines
20 KiB
C++
524 lines
20 KiB
C++
/*
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This program is free software: you can redistribute it and/or modify
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it under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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This program is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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#include <AP_Math/AP_Math.h>
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#include <AP_HAL/AP_HAL.h>
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#include "AR_AttitudeControl.h"
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extern const AP_HAL::HAL& hal;
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const AP_Param::GroupInfo AR_AttitudeControl::var_info[] = {
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// @Param: _STR_RAT_P
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// @DisplayName: Steering control rate P gain
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// @Description: Steering control rate P gain. Converts the turn rate error (in radians/sec) to a steering control output (in the range -1 to +1)
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// @Range: 0.000 2.000
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// @Increment: 0.01
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// @User: Standard
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// @Param: _STR_RAT_I
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// @DisplayName: Steering control I gain
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// @Description: Steering control I gain. Corrects long term error between the desired turn rate (in rad/s) and actual
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// @Range: 0.000 2.000
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// @Increment: 0.01
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// @User: Standard
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// @Param: _STR_RAT_IMAX
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// @DisplayName: Steering control I gain maximum
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// @Description: Steering control I gain maximum. Constraings the steering output (range -1 to +1) that the I term will generate
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// @Range: 0.000 1.000
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// @Increment: 0.01
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// @User: Standard
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// @Param: _STR_RAT_D
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// @DisplayName: Steering control D gain
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// @Description: Steering control D gain. Compensates for short-term change in desired turn rate vs actual
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// @Range: 0.000 0.400
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// @Increment: 0.001
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// @User: Standard
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// @Param: _STR_RAT_FF
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// @DisplayName: Steering control feed forward
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// @Description: Steering control feed forward
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// @Range: 0.000 3.000
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// @Increment: 0.001
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// @User: Standard
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// @Param: _STR_RAT_FILT
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// @DisplayName: Steering control filter frequency
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// @Description: Steering control input filter. Lower values reduce noise but add delay.
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// @Range: 0.000 100.000
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// @Increment: 0.1
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// @Units: Hz
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// @User: Standard
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AP_SUBGROUPINFO(_steer_rate_pid, "_STR_RAT_", 1, AR_AttitudeControl, AC_PID),
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// @Param: _SPEED_P
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// @DisplayName: Speed control P gain
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// @Description: Speed control P gain. Converts the error between the desired speed (in m/s) and actual speed to a motor output (in the range -1 to +1)
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// @Range: 0.010 2.000
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// @Increment: 0.01
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// @User: Standard
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// @Param: _SPEED_I
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// @DisplayName: Speed control I gain
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// @Description: Speed control I gain. Corrects long term error between the desired speed (in m/s) and actual speed
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// @Range: 0.000 2.000
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// @User: Standard
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// @Param: _SPEED_IMAX
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// @DisplayName: Speed control I gain maximum
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// @Description: Speed control I gain maximum. Constraings the maximum motor output (range -1 to +1) that the I term will generate
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// @Range: 0.000 1.000
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// @Increment: 0.01
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// @User: Standard
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// @Param: _SPEED_D
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// @DisplayName: Speed control D gain
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// @Description: Speed control D gain. Compensates for short-term change in desired speed vs actual
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// @Range: 0.000 0.400
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// @Increment: 0.001
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// @User: Standard
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// @Param: _SPEED_FF
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// @DisplayName: Speed control feed forward
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// @Description: Speed control feed forward
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// @Range: 0.000 0.500
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// @Increment: 0.001
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// @User: Standard
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// @Param: _SPEED_FILT
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// @DisplayName: Speed control filter frequency
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// @Description: Speed control input filter. Lower values reduce noise but add delay.
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// @Range: 0.000 100.000
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// @Increment: 0.1
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// @Units: Hz
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// @User: Standard
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AP_SUBGROUPINFO(_throttle_speed_pid, "_SPEED_", 2, AR_AttitudeControl, AC_PID),
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// @Param: _ACCEL_MAX
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// @DisplayName: Speed control acceleration (and deceleration) maximum in m/s/s
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// @Description: Speed control acceleration (and deceleration) maximum in m/s/s. 0 to disable acceleration limiting
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// @Range: 0.0 10.0
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// @Increment: 0.1
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// @Units: m/s/s
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// @User: Standard
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AP_GROUPINFO("_ACCEL_MAX", 3, AR_AttitudeControl, _throttle_accel_max, AR_ATTCONTROL_THR_ACCEL_MAX),
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// @Param: _BRAKE
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// @DisplayName: Speed control brake enable/disable
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// @Description: Speed control brake enable/disable. Allows sending a reversed output to the motors to slow the vehicle.
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// @Values: 0:Disable,1:Enable
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// @User: Standard
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AP_GROUPINFO("_BRAKE", 4, AR_AttitudeControl, _brake_enable, 0),
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// @Param: _STOP_SPEED
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// @DisplayName: Speed control stop speed
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// @Description: Speed control stop speed. Motor outputs to zero once vehicle speed falls below this value
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// @Range: 0.00 0.50
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// @Increment: 0.01
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// @Units: m/s
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// @User: Standard
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AP_GROUPINFO("_STOP_SPEED", 5, AR_AttitudeControl, _stop_speed, AR_ATTCONTROL_STOP_SPEED_DEFAULT),
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// @Param: _STR_ANG_P
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// @DisplayName: Steering control angle P gain
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// @Description: Steering control angle P gain. Converts the error between the desired heading/yaw (in radians) and actual heading/yaw to a desired turn rate (in rad/sec)
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// @Range: 1.000 10.000
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// @Increment: 0.1
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// @User: Standard
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AP_SUBGROUPINFO(_steer_angle_p, "_STR_ANG_", 6, AR_AttitudeControl, AC_P),
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// @Param: _STR_ACC_MAX
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// @DisplayName: Steering control angular acceleration maximum
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// @Description: Steering control angular acceleartion maximum (in deg/s/s). 0 to disable acceleration limiting
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// @Range: 0 1000
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// @Increment: 0.1
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// @Units: deg/s/s
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// @User: Standard
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AP_GROUPINFO("_STR_ACC_MAX", 7, AR_AttitudeControl, _steer_accel_max, AR_ATTCONTROL_STEER_ACCEL_MAX),
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// @Param: _STR_RAT_MAX
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// @DisplayName: Steering control rotation rate maximum
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// @Description: Steering control rotation rate maximum in deg/s. 0 to remove rate limiting
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// @Range: 0 1000
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// @Increment: 0.1
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// @Units: deg/s
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// @User: Standard
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AP_GROUPINFO("_STR_RAT_MAX", 8, AR_AttitudeControl, _steer_rate_max, AR_ATTCONTROL_STEER_RATE_MAX),
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AP_GROUPEND
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};
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AR_AttitudeControl::AR_AttitudeControl(AP_AHRS &ahrs) :
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_ahrs(ahrs),
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_steer_angle_p(AR_ATTCONTROL_STEER_ANG_P),
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_steer_rate_pid(AR_ATTCONTROL_STEER_RATE_P, AR_ATTCONTROL_STEER_RATE_I, AR_ATTCONTROL_STEER_RATE_D, AR_ATTCONTROL_STEER_RATE_IMAX, AR_ATTCONTROL_STEER_RATE_FILT, AR_ATTCONTROL_DT, AR_ATTCONTROL_STEER_RATE_FF),
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_throttle_speed_pid(AR_ATTCONTROL_THR_SPEED_P, AR_ATTCONTROL_THR_SPEED_I, AR_ATTCONTROL_THR_SPEED_D, AR_ATTCONTROL_THR_SPEED_IMAX, AR_ATTCONTROL_THR_SPEED_FILT, AR_ATTCONTROL_DT)
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{
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AP_Param::setup_object_defaults(this, var_info);
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}
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// return a steering servo output from -1.0 to +1.0 given a desired lateral acceleration rate in m/s/s.
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// positive lateral acceleration is to the right.
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float AR_AttitudeControl::get_steering_out_lat_accel(float desired_accel, bool skid_steering, bool vect_thrust, bool motor_limit_left, bool motor_limit_right, bool reversed)
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{
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// record desired accel for reporting purposes
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_steer_lat_accel_last_ms = AP_HAL::millis();
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_desired_lat_accel = desired_accel;
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// get speed forward
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float speed;
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if (!get_forward_speed(speed)) {
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// we expect caller will not try to control heading using rate control without a valid speed estimate
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// on failure to get speed we do not attempt to steer
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return 0.0f;
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}
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// only use positive speed. Use reverse flag instead of negative speeds.
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speed = fabsf(speed);
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// enforce minimum speed to stop oscillations when first starting to move
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if (speed < AR_ATTCONTROL_STEER_SPEED_MIN) {
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speed = AR_ATTCONTROL_STEER_SPEED_MIN;
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}
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// Calculate the desired steering rate given desired_accel and speed
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float desired_rate = desired_accel / speed;
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// invert rate if we are going backwards
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if (reversed) {
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desired_rate *= -1.0f;
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}
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return get_steering_out_rate(desired_rate, skid_steering, vect_thrust, motor_limit_left, motor_limit_right, reversed);
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}
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// return a steering servo output from -1 to +1 given a heading in radians
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float AR_AttitudeControl::get_steering_out_heading(float heading_rad, bool skid_steering, bool vect_thrust, bool motor_limit_left, bool motor_limit_right, bool reversed)
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{
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// calculate heading error (in radians)
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const float yaw_error = wrap_PI(heading_rad - _ahrs.yaw);
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// Calculate the desired turn rate (in radians) from the angle error (also in radians)
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float desired_rate = _steer_angle_p.get_p(yaw_error);
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if (reversed) {
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desired_rate = -desired_rate;
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}
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return get_steering_out_rate(desired_rate, skid_steering, vect_thrust, motor_limit_left, motor_limit_right, reversed);
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}
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// return a steering servo output from -1 to +1 given a
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// desired yaw rate in radians/sec. Positive yaw is to the right.
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float AR_AttitudeControl::get_steering_out_rate(float desired_rate, bool skid_steering, bool vect_thrust, bool motor_limit_left, bool motor_limit_right, bool reversed)
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{
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// calculate dt
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const uint32_t now = AP_HAL::millis();
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float dt = (now - _steer_turn_last_ms) / 1000.0f;
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if ((_steer_turn_last_ms == 0) || (dt > (AR_ATTCONTROL_TIMEOUT_MS / 1000.0f))) {
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dt = 0.0f;
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_steer_rate_pid.reset_filter();
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// reset desired turn rate to actual turn rate for accel limiting
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_desired_turn_rate = _ahrs.get_yaw_rate_earth();
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} else {
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_steer_rate_pid.set_dt(dt);
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}
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_steer_turn_last_ms = now;
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// acceleration limit desired turn rate
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const float change_max = radians(_steer_accel_max) * dt;
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if (is_positive(dt) && is_positive(change_max)) {
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desired_rate = constrain_float(desired_rate, _desired_turn_rate - change_max, _desired_turn_rate + change_max);
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}
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_desired_turn_rate = desired_rate;
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// rate limit desired turn rate
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if (is_positive(_steer_rate_max)) {
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_desired_turn_rate = constrain_float(_desired_turn_rate, -_steer_rate_max, _steer_rate_max);
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}
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float scaler = 1.0f;
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bool low_speed = false;
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// scaler to linearize output because turn rate increases as vehicle speed increases
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// on non-skid steering and non-vectored thrust vehicles
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if (!skid_steering && !vect_thrust) {
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// get speed forward
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float speed;
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if (!get_forward_speed(speed)) {
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// we expect caller will not try to control heading using rate control without a valid speed estimate
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// on failure to get speed we do not attempt to steer
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return 0.0f;
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}
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// only use positive speed. Use reverse flag instead of negative speeds.
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speed = fabsf(speed);
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// enforce minimum speed to stop oscillations when first starting to move
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if (speed < AR_ATTCONTROL_STEER_SPEED_MIN) {
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low_speed = true;
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speed = AR_ATTCONTROL_STEER_SPEED_MIN;
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}
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scaler = 1.0f / fabsf(speed);
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}
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// Calculate the steering rate error (rad/sec) and apply gain scaler
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// We do this in earth frame to allow for rover leaning over in hard corners
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float yaw_rate_earth = _ahrs.get_yaw_rate_earth();
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// check if reversing
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if (reversed) {
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yaw_rate_earth *= -1.0f;
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}
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const float rate_error = (desired_rate - yaw_rate_earth) * scaler;
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// record desired rate for logging purposes only
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_steer_rate_pid.set_desired_rate(desired_rate);
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// pass error to PID controller
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_steer_rate_pid.set_input_filter_all(rate_error);
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// get feed-forward
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const float ff = _steer_rate_pid.get_ff(desired_rate * scaler);
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// get p
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const float p = _steer_rate_pid.get_p();
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// get i unless non-skid-steering rover at low speed or steering output has hit a limit
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float i = _steer_rate_pid.get_integrator();
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if ((!low_speed || skid_steering) && ((is_negative(rate_error) && !motor_limit_left) || (is_positive(rate_error) && !motor_limit_right))) {
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i = _steer_rate_pid.get_i();
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}
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// get d
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const float d = _steer_rate_pid.get_d();
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// constrain and return final output
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return constrain_float(ff + p + i + d, -1.0f, 1.0f);
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}
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// get latest desired turn rate in rad/sec (recorded during calls to get_steering_out_rate)
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float AR_AttitudeControl::get_desired_turn_rate() const
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{
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// return zero if no recent calls to turn rate controller
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if ((_steer_turn_last_ms == 0) || ((AP_HAL::millis() - _steer_turn_last_ms) > AR_ATTCONTROL_TIMEOUT_MS)) {
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return 0.0f;
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}
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return _desired_turn_rate;
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}
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// get latest desired lateral acceleration in m/s/s (recorded during calls to get_steering_out_lat_accel)
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float AR_AttitudeControl::get_desired_lat_accel() const
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{
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// return zero if no recent calls to lateral acceleration controller
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if ((_steer_lat_accel_last_ms == 0) || ((AP_HAL::millis() - _steer_lat_accel_last_ms) > AR_ATTCONTROL_TIMEOUT_MS)) {
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return 0.0f;
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}
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return _desired_lat_accel;
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}
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// get actual lateral acceleration in m/s/s. returns true on success
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bool AR_AttitudeControl::get_lat_accel(float &lat_accel) const
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{
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float speed;
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if (!get_forward_speed(speed)) {
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return false;
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}
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lat_accel = speed * _ahrs.get_yaw_rate_earth();
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return true;
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}
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// return a throttle output from -1 to +1 given a desired speed in m/s (use negative speeds to travel backwards)
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// motor_limit should be true if motors have hit their upper or lower limits
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// cruise speed should be in m/s, cruise throttle should be a number from -1 to +1
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float AR_AttitudeControl::get_throttle_out_speed(float desired_speed, bool motor_limit_low, bool motor_limit_high, float cruise_speed, float cruise_throttle)
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{
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// get speed forward
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float speed;
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if (!get_forward_speed(speed)) {
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// we expect caller will not try to control heading using rate control without a valid speed estimate
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// on failure to get speed we do not attempt to steer
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return 0.0f;
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}
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// calculate dt
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const uint32_t now = AP_HAL::millis();
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float dt = (now - _speed_last_ms) / 1000.0f;
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if ((_speed_last_ms == 0) || (dt > (AR_ATTCONTROL_TIMEOUT_MS / 1000.0f))) {
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dt = 0.0f;
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_throttle_speed_pid.reset_filter();
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} else {
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_throttle_speed_pid.set_dt(dt);
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}
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_speed_last_ms = now;
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// record desired speed for next iteration
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_desired_speed = desired_speed;
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// calculate speed error and pass to PID controller
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const float speed_error = desired_speed - speed;
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_throttle_speed_pid.set_input_filter_all(speed_error);
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// record desired speed for logging purposes only
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_throttle_speed_pid.set_desired_rate(desired_speed);
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// get feed-forward
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const float ff = _throttle_speed_pid.get_ff(desired_speed);
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// get p
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const float p = _throttle_speed_pid.get_p();
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// get i unless moving at low speed or motors have hit a limit
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float i = _throttle_speed_pid.get_integrator();
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if ((is_negative(speed_error) && !motor_limit_low && !_throttle_limit_low) || (is_positive(speed_error) && !motor_limit_high && !_throttle_limit_high)) {
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i = _throttle_speed_pid.get_i();
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}
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// get d
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const float d = _throttle_speed_pid.get_d();
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// calculate base throttle (protect against divide by zero)
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float throttle_base = 0.0f;
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if (is_positive(cruise_speed) && is_positive(cruise_throttle)) {
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throttle_base = desired_speed * (cruise_throttle / cruise_speed);
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}
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// calculate final output
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float throttle_out = (ff+p+i+d+throttle_base);
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// clear local limit flags used to stop i-term build-up as we stop reversed outputs going to motors
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_throttle_limit_low = false;
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_throttle_limit_high = false;
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// protect against reverse output being sent to the motors unless braking has been enabled
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if (!_brake_enable) {
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// if both desired speed and actual speed are positive, do not allow negative values
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if ((desired_speed >= 0.0f) && (throttle_out <= 0.0f)) {
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throttle_out = 0.0f;
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_throttle_limit_low = true;
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}
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if ((desired_speed <= 0.0f) && (throttle_out >= 0.0f)) {
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throttle_out = 0.0f;
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_throttle_limit_high = true;
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}
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}
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// final output throttle in range -1 to 1
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return throttle_out;
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}
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// return a throttle output from -1 to +1 to perform a controlled stop. returns true once the vehicle has stopped
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float AR_AttitudeControl::get_throttle_out_stop(bool motor_limit_low, bool motor_limit_high, float cruise_speed, float cruise_throttle, bool &stopped)
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{
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// get current system time
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const uint32_t now = AP_HAL::millis();
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// if we were stopped in the last 300ms, assume we are still stopped
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bool _stopped = (_stop_last_ms != 0) && (now - _stop_last_ms) < 300;
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// get speed forward
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float speed;
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if (!get_forward_speed(speed)) {
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|
// could not get speed so assume stopped
|
|
_stopped = true;
|
|
} else {
|
|
// if desired speed is zero and vehicle drops below _stop_speed consider it stopped
|
|
if (is_zero(_desired_speed) && fabsf(speed) <= fabsf(_stop_speed)) {
|
|
_stopped = true;
|
|
}
|
|
}
|
|
|
|
// set stopped status for caller
|
|
stopped = _stopped;
|
|
|
|
// if stopped return zero
|
|
if (stopped) {
|
|
// update last time we thought we were stopped
|
|
_stop_last_ms = now;
|
|
return 0.0f;
|
|
} else {
|
|
// clear stopped system time
|
|
_stop_last_ms = 0;
|
|
// run speed controller to bring vehicle to stop
|
|
return get_throttle_out_speed(0.0f, motor_limit_low, motor_limit_high, cruise_speed, cruise_throttle);
|
|
}
|
|
}
|
|
|
|
// get forward speed in m/s (earth-frame horizontal velocity but only along vehicle x-axis). returns true on success
|
|
bool AR_AttitudeControl::get_forward_speed(float &speed) const
|
|
{
|
|
Vector3f velocity;
|
|
if (!_ahrs.get_velocity_NED(velocity)) {
|
|
// use less accurate GPS, assuming entire length is along forward/back axis of vehicle
|
|
if (AP::gps().status() >= AP_GPS::GPS_OK_FIX_3D) {
|
|
if (labs(wrap_180_cd(_ahrs.yaw_sensor - AP::gps().ground_course_cd())) <= 9000) {
|
|
speed = AP::gps().ground_speed();
|
|
} else {
|
|
speed = -AP::gps().ground_speed();
|
|
}
|
|
return true;
|
|
} else {
|
|
return false;
|
|
}
|
|
}
|
|
// calculate forward speed velocity into body frame
|
|
speed = velocity.x*_ahrs.cos_yaw() + velocity.y*_ahrs.sin_yaw();
|
|
return true;
|
|
}
|
|
|
|
// get latest desired speed recorded during call to get_throttle_out_speed. For reporting purposes only
|
|
float AR_AttitudeControl::get_desired_speed() const
|
|
{
|
|
// return zero if no recent calls to speed controller
|
|
if ((_speed_last_ms == 0) || ((AP_HAL::millis() - _speed_last_ms) > AR_ATTCONTROL_TIMEOUT_MS)) {
|
|
return 0.0f;
|
|
}
|
|
return _desired_speed;
|
|
}
|
|
|
|
// get acceleration limited desired speed
|
|
float AR_AttitudeControl::get_desired_speed_accel_limited(float desired_speed) const
|
|
{
|
|
// return input value if no recent calls to speed controller
|
|
const uint32_t now = AP_HAL::millis();
|
|
if ((_speed_last_ms == 0) || ((now - _speed_last_ms) > AR_ATTCONTROL_TIMEOUT_MS) || !is_positive(_throttle_accel_max)) {
|
|
return desired_speed;
|
|
}
|
|
|
|
// calculate dt
|
|
const float dt = (now - _speed_last_ms) / 1000.0f;
|
|
|
|
// acceleration limit desired speed
|
|
const float speed_change_max = _throttle_accel_max * dt;
|
|
return constrain_float(desired_speed, _desired_speed - speed_change_max, _desired_speed + speed_change_max);
|
|
}
|
|
|
|
// get minimum stopping distance (in meters) given a speed (in m/s)
|
|
float AR_AttitudeControl::get_stopping_distance(float speed)
|
|
{
|
|
// get maximum vehicle deceleration
|
|
const float accel_max = get_accel_max();
|
|
|
|
// avoid divide by zero
|
|
if ((accel_max <= 0.0f) || is_zero(speed)) {
|
|
return 0.0f;
|
|
}
|
|
|
|
// assume linear deceleration
|
|
return 0.5f * sq(speed) / accel_max;
|
|
}
|