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Smooth yaw in auto mode by limiting acceleration #24766

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46 changes: 20 additions & 26 deletions src/modules/flight_mode_manager/tasks/Auto/FlightTaskAuto.cpp
Original file line number Diff line number Diff line change
Expand Up @@ -70,7 +70,10 @@ bool FlightTaskAuto::activate(const trajectory_setpoint_s &last_setpoint)

_position_smoothing.reset(accel_prev, vel_prev, pos_prev);

_yaw_sp_prev = PX4_ISFINITE(last_setpoint.yaw) ? last_setpoint.yaw : _yaw;
_yaw_setpoint_previous = last_setpoint.yaw;
_heading_smoothing.reset(PX4_ISFINITE(last_setpoint.yaw) ? last_setpoint.yaw : _yaw,
PX4_ISFINITE(last_setpoint.yawspeed) ? last_setpoint.yawspeed : 0.f);

_updateTrajConstraints();
_is_emergency_braking_active = false;
_time_last_cruise_speed_override = 0;
Expand Down Expand Up @@ -190,16 +193,14 @@ bool FlightTaskAuto::update()
// no valid heading -> generate heading in this flight task
// Generate heading along trajectory if possible, otherwise hold the previous yaw setpoint
if (!_generateHeadingAlongTraj()) {
_yaw_setpoint = PX4_ISFINITE(_yaw_sp_prev) ? _yaw_sp_prev : _yaw;
_yaw_setpoint = _yaw_setpoint_previous;
}
}

// update previous type
_type_previous = _type;

// If the FlightTask generates a yaw or a yawrate setpoint that exceeds this value
// it will see its setpoint constrained here
_limitYawRate();
_smoothYaw();

_constraints.want_takeoff = _checkTakeoff();

Expand Down Expand Up @@ -257,7 +258,7 @@ void FlightTaskAuto::_prepareLandSetpoints()

if (sticks_xy.longerThan(FLT_EPSILON)) {
// Ensure no unintended yawing when nudging horizontally during initial heading alignment
_land_heading = _yaw_sp_prev;
_land_heading = _yaw_setpoint_previous;
}

rcHelpModifyYaw(_land_heading);
Expand Down Expand Up @@ -300,39 +301,32 @@ void FlightTaskAuto::_prepareLandSetpoints()
_gear.landing_gear = landing_gear_s::GEAR_DOWN;
}

void FlightTaskAuto::_limitYawRate()
void FlightTaskAuto::_smoothYaw()
{
const float yawrate_max = math::radians(_param_mpc_yawrauto_max.get());
_heading_smoothing.setMaxHeadingRate(yawrate_max);
_heading_smoothing.setMaxHeadingAccel(math::radians(_param_mpc_yawrauto_acc.get()));

_yaw_sp_aligned = true;

if (PX4_ISFINITE(_yaw_setpoint) && PX4_ISFINITE(_yaw_sp_prev)) {
// Limit the rate of change of the yaw setpoint
const float dyaw_desired = matrix::wrap_pi(_yaw_setpoint - _yaw_sp_prev);
const float dyaw_max = yawrate_max * _deltatime;
const float dyaw = math::constrain(dyaw_desired, -dyaw_max, dyaw_max);
const float yaw_setpoint_sat = matrix::wrap_pi(_yaw_sp_prev + dyaw);
if (PX4_ISFINITE(_yaw_setpoint)) {
const float yaw_sp_unsmoothed = _yaw_setpoint;
_heading_smoothing.update(_yaw_setpoint, _deltatime);
_yaw_setpoint = _heading_smoothing.getSmoothedHeading();
_yawspeed_setpoint = _heading_smoothing.getSmoothedHeadingRate();

// The yaw setpoint is aligned when it is within tolerance
_yaw_sp_aligned = fabsf(matrix::wrap_pi(_yaw_setpoint - yaw_setpoint_sat)) < math::radians(_param_mis_yaw_err.get());

_yaw_setpoint = yaw_setpoint_sat;
_yaw_sp_aligned = fabsf(matrix::wrap_pi(yaw_sp_unsmoothed - _yaw_setpoint)) < math::radians(_param_mis_yaw_err.get());

if (!PX4_ISFINITE(_yawspeed_setpoint) && (_deltatime > FLT_EPSILON)) {
// Create a feedforward using the filtered derivative
_yawspeed_filter.setParameters(_deltatime, .2f);
_yawspeed_filter.update(dyaw / _deltatime);
_yawspeed_setpoint = _yawspeed_filter.getState();
}
} else {
_heading_smoothing.reset(_yaw, 0.f);
}

_yaw_sp_prev = PX4_ISFINITE(_yaw_setpoint) ? _yaw_setpoint : _yaw;
_yaw_setpoint_previous = _yaw_setpoint;

if (PX4_ISFINITE(_yawspeed_setpoint)) {
// The yaw setpoint is aligned when its rate is not saturated
_yaw_sp_aligned = _yaw_sp_aligned && (fabsf(_yawspeed_setpoint) < yawrate_max);

_yawspeed_setpoint = math::constrain(_yawspeed_setpoint, -yawrate_max, yawrate_max);
}
}

Expand Down Expand Up @@ -725,7 +719,7 @@ void FlightTaskAuto::_ekfResetHandlerVelocityZ(float delta_vz)

void FlightTaskAuto::_ekfResetHandlerHeading(float delta_psi)
{
_yaw_sp_prev += delta_psi;
_yaw_setpoint_previous += delta_psi;
}

void FlightTaskAuto::_checkEmergencyBraking()
Expand Down
8 changes: 5 additions & 3 deletions src/modules/flight_mode_manager/tasks/Auto/FlightTaskAuto.hpp
Original file line number Diff line number Diff line change
Expand Up @@ -47,6 +47,7 @@
#include <uORB/topics/vehicle_status.h>
#include <lib/geo/geo.h>
#include <lib/mathlib/math/filter/AlphaFilter.hpp>
#include <lib/motion_planning/HeadingSmoothing.hpp>
#include <lib/motion_planning/PositionSmoothing.hpp>
#include <lib/stick_yaw/StickYaw.hpp>
#include <lib/weather_vane/WeatherVane.hpp>
Expand Down Expand Up @@ -136,8 +137,8 @@ class FlightTaskAuto : public FlightTask
State _current_state{State::none};
float _target_acceptance_radius{0.0f}; /**< Acceptances radius of the target */

float _yaw_sp_prev{NAN};
AlphaFilter<float> _yawspeed_filter;
float _yaw_setpoint_previous{NAN}; /**< Used because _yaw_setpoint is overwritten in multiple places */
HeadingSmoothing _heading_smoothing;
bool _yaw_sp_aligned{false};

PositionSmoothing _position_smoothing;
Expand All @@ -156,6 +157,7 @@ class FlightTaskAuto : public FlightTask
(ParamFloat<px4::params::NAV_MC_ALT_RAD>)
_param_nav_mc_alt_rad, //vertical acceptance radius at which waypoints are updated
(ParamInt<px4::params::MPC_YAW_MODE>) _param_mpc_yaw_mode, // defines how heading is executed,
(ParamFloat<px4::params::MPC_YAWRAUTO_ACC>) _param_mpc_yawrauto_acc,
(ParamFloat<px4::params::MPC_YAWRAUTO_MAX>) _param_mpc_yawrauto_max,
(ParamFloat<px4::params::MIS_YAW_ERR>) _param_mis_yaw_err, // yaw-error threshold
(ParamFloat<px4::params::MPC_ACC_HOR>) _param_mpc_acc_hor, // acceleration in flight
Expand Down Expand Up @@ -201,7 +203,7 @@ class FlightTaskAuto : public FlightTask

matrix::Vector3f _initial_land_position;

void _limitYawRate(); /**< Limits the rate of change of the yaw setpoint. */
void _smoothYaw(); /**< Smoothen the yaw setpoint. */
bool _evaluateTriplets(); /**< Checks and sets triplets. */
bool _isFinite(const position_setpoint_s &sp); /**< Checks if all waypoint triplets are finite. */
bool _evaluateGlobalReference(); /**< Check is global reference is available. */
Expand Down
15 changes: 11 additions & 4 deletions src/modules/flight_mode_manager/tasks/Orbit/FlightTaskOrbit.cpp
Original file line number Diff line number Diff line change
Expand Up @@ -179,8 +179,8 @@ bool FlightTaskOrbit::activate(const trajectory_setpoint_s &last_setpoint)
_orbit_velocity = 1.f;
_center = _position;
_initial_heading = _yaw;
_slew_rate_yaw.setForcedValue(_yaw);
_slew_rate_yaw.setSlewRate(math::radians(_param_mpc_yawrauto_max.get()));
_heading_smoothing.reset(PX4_ISFINITE(last_setpoint.yaw) ? last_setpoint.yaw : _yaw,
PX4_ISFINITE(last_setpoint.yawspeed) ? last_setpoint.yawspeed : 0.f);
_slew_rate_velocity.setSlewRate(_param_mpc_acc_hor.get());

// need a valid position and velocity
Expand Down Expand Up @@ -238,7 +238,14 @@ bool FlightTaskOrbit::update()
}

// Apply yaw smoothing
_yaw_setpoint = _slew_rate_yaw.update(_yaw_setpoint, _deltatime);
_heading_smoothing.setMaxHeadingRate(math::radians(_param_mpc_yawrauto_max.get()));
_heading_smoothing.setMaxHeadingAccel(math::radians(_param_mpc_yawrauto_acc.get()));
_heading_smoothing.update(_yaw_setpoint, _deltatime);
_yaw_setpoint = _heading_smoothing.getSmoothedHeading();

if (_in_circle_approach) { // don't override feed-forward which is already calculated for circling
_yawspeed_setpoint = _heading_smoothing.getSmoothedHeadingRate();
}

// publish information to UI
sendTelemetry();
Expand Down Expand Up @@ -362,7 +369,7 @@ void FlightTaskOrbit::_generate_circle_yaw_setpoints()
case orbit_status_s::ORBIT_YAW_BEHAVIOUR_UNCONTROLLED:
// no yaw setpoint
_yaw_setpoint = NAN;
_yawspeed_setpoint = NAN;
_yawspeed_setpoint = 0.f; // No yaw setpoint is invalid -> just brake to 0°/s
break;

case orbit_status_s::ORBIT_YAW_BEHAVIOUR_HOLD_FRONT_TANGENT_TO_CIRCLE:
Expand Down
Original file line number Diff line number Diff line change
Expand Up @@ -45,6 +45,7 @@
#include <uORB/PublicationMulti.hpp>
#include <uORB/topics/orbit_status.h>
#include <lib/slew_rate/SlewRateYaw.hpp>
#include <lib/motion_planning/HeadingSmoothing.hpp>
#include <lib/motion_planning/PositionSmoothing.hpp>
#include <lib/motion_planning/VelocitySmoothing.hpp>
#include <lib/slew_rate/SlewRate.hpp>
Expand Down Expand Up @@ -127,7 +128,7 @@ class FlightTaskOrbit : public FlightTaskManualAltitudeSmoothVel
bool _started_clockwise{true};
bool _currently_orbiting{false};
float _initial_heading = 0.f; /**< the heading of the drone when the orbit command was issued */
SlewRateYaw<float> _slew_rate_yaw;
HeadingSmoothing _heading_smoothing;
SlewRate<float> _slew_rate_velocity;

orb_advert_t _mavlink_log_pub{nullptr};
Expand All @@ -138,6 +139,7 @@ class FlightTaskOrbit : public FlightTaskManualAltitudeSmoothVel
(ParamInt<px4::params::MC_ORBIT_YAW_MOD>) _param_mc_orbit_yaw_mod,
(ParamFloat<px4::params::MPC_XY_CRUISE>) _param_mpc_xy_cruise, /**< cruise speed for circle approach */
(ParamFloat<px4::params::MPC_YAWRAUTO_MAX>) _param_mpc_yawrauto_max,
(ParamFloat<px4::params::MPC_YAWRAUTO_ACC>) _param_mpc_yawrauto_acc,
(ParamFloat<px4::params::MPC_XY_TRAJ_P>) _param_mpc_xy_traj_p,
(ParamFloat<px4::params::NAV_MC_ALT_RAD>)
_param_nav_mc_alt_rad, //vertical acceptance radius at which waypoints are updated
Expand Down
4 changes: 2 additions & 2 deletions src/modules/mc_pos_control/multicopter_autonomous_params.c
Original file line number Diff line number Diff line change
Expand Up @@ -145,7 +145,7 @@ PARAM_DEFINE_FLOAT(MPC_XY_ERR_MAX, 2.f);
* @increment 5
* @group Multicopter Attitude Control
*/
PARAM_DEFINE_FLOAT(MPC_YAWRAUTO_MAX, 45.f);
PARAM_DEFINE_FLOAT(MPC_YAWRAUTO_MAX, 60.f);

/**
* Maximum yaw acceleration in autonomous modes
Expand All @@ -160,7 +160,7 @@ PARAM_DEFINE_FLOAT(MPC_YAWRAUTO_MAX, 45.f);
* @increment 5
* @group Multicopter Attitude Control
*/
PARAM_DEFINE_FLOAT(MPC_YAWRAUTO_ACC, 60.f);
PARAM_DEFINE_FLOAT(MPC_YAWRAUTO_ACC, 20.f);

/**
* Heading behavior in autonomous modes
Expand Down
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