mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-03 15:28:53 +08:00
FW att controller: wheel controller: separate from ecl_controller
Signed-off-by: Silvan Fuhrer <silvan@auterion.com>
This commit is contained in:
@@ -41,7 +41,7 @@ px4_add_module(
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ecl_controller.cpp
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ecl_controller.cpp
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fw_pitch_controller.cpp
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fw_pitch_controller.cpp
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fw_roll_controller.cpp
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fw_roll_controller.cpp
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ecl_wheel_controller.cpp
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fw_wheel_controller.cpp
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fw_yaw_controller.cpp
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fw_yaw_controller.cpp
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DEPENDS
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DEPENDS
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px4_work_queue
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px4_work_queue
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@@ -36,7 +36,7 @@
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#include <drivers/drv_hrt.h>
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#include <drivers/drv_hrt.h>
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#include "fw_pitch_controller.h"
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#include "fw_pitch_controller.h"
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#include "fw_roll_controller.h"
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#include "fw_roll_controller.h"
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#include "ecl_wheel_controller.h"
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#include "fw_wheel_controller.h"
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#include "fw_yaw_controller.h"
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#include "fw_yaw_controller.h"
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#include <lib/mathlib/mathlib.h>
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#include <lib/mathlib/mathlib.h>
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#include <lib/parameters/param.h>
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#include <lib/parameters/param.h>
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@@ -162,7 +162,7 @@ private:
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RollController _roll_ctrl;
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RollController _roll_ctrl;
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PitchController _pitch_ctrl;
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PitchController _pitch_ctrl;
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YawController _yaw_ctrl;
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YawController _yaw_ctrl;
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ECL_WheelController _wheel_ctrl;
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WheelController _wheel_ctrl;
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void parameters_update();
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void parameters_update();
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void vehicle_manual_poll(const float yaw_body);
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void vehicle_manual_poll(const float yaw_body);
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+24
-38
@@ -1,6 +1,6 @@
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/****************************************************************************
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/****************************************************************************
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*
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*
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* Copyright (c) 2013-2016 Estimation and Control Library (ECL). All rights reserved.
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* Copyright (c) 2020-2023 PX4 Development Team. All rights reserved.
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*
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*
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* Redistribution and use in source and binary forms, with or without
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* modification, are permitted provided that the following conditions
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@@ -32,13 +32,11 @@
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****************************************************************************/
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****************************************************************************/
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/**
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/**
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* @file ecl_wheel_controller.cpp
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* @file fw_wheel_controller.cpp
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* Implementation of a simple PID wheel controller for heading tracking.
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* Implementation of a simple PID wheel controller for heading tracking.
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*
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* Authors and acknowledgements in header.
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*/
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*/
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#include "ecl_wheel_controller.h"
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#include "fw_wheel_controller.h"
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#include <float.h>
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#include <float.h>
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#include <lib/geo/geo.h>
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#include <lib/geo/geo.h>
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#include <mathlib/mathlib.h>
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#include <mathlib/mathlib.h>
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@@ -46,68 +44,56 @@
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using matrix::wrap_pi;
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using matrix::wrap_pi;
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float ECL_WheelController::control_bodyrate(const float dt, const ECL_ControlData &ctl_data)
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float WheelController::control_bodyrate(float dt, float body_z_rate, float groundspeed, float groundspeed_scaler)
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{
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{
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/* Do not calculate control signal with bad inputs */
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/* Do not calculate control signal with bad inputs */
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if (!(PX4_ISFINITE(ctl_data.body_z_rate) &&
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if (!(PX4_ISFINITE(body_z_rate) &&
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PX4_ISFINITE(ctl_data.groundspeed) &&
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PX4_ISFINITE(groundspeed) &&
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PX4_ISFINITE(ctl_data.groundspeed_scaler))) {
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PX4_ISFINITE(groundspeed_scaler))) {
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return math::constrain(_last_output, -1.0f, 1.0f);
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return math::constrain(_last_output, -1.f, 1.f);
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}
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}
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/* input conditioning */
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const float rate_error = _body_rate_setpoint - body_z_rate;
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float min_speed = 1.0f;
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/* Calculate body angular rate error */
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if (_k_i > 0.f && groundspeed > 1.f) { // only start integrating when above 1m/s
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const float rate_error = _body_rate_setpoint - ctl_data.body_z_rate; //body angular rate error
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if (_k_i > 0.0f && ctl_data.groundspeed > min_speed) {
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float id = rate_error * dt * groundspeed_scaler;
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float id = rate_error * dt * ctl_data.groundspeed_scaler;
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if (_last_output < -1.f) {
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/*
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* anti-windup: do not allow integrator to increase if actuator is at limit
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*/
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if (_last_output < -1.0f) {
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/* only allow motion to center: increase value */
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/* only allow motion to center: increase value */
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id = math::max(id, 0.0f);
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id = math::max(id, 0.f);
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} else if (_last_output > 1.0f) {
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} else if (_last_output > 1.f) {
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/* only allow motion to center: decrease value */
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/* only allow motion to center: decrease value */
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id = math::min(id, 0.0f);
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id = math::min(id, 0.f);
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}
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}
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/* add and constrain */
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_integrator = math::constrain(_integrator + id * _k_i, -_integrator_max, _integrator_max);
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_integrator = math::constrain(_integrator + id * _k_i, -_integrator_max, _integrator_max);
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}
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}
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/* Apply PI rate controller and store non-limited output */
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/* Apply PI rate controller and store non-limited output */
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_last_output = _body_rate_setpoint * _k_ff * ctl_data.groundspeed_scaler +
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_last_output = _body_rate_setpoint * _k_ff * groundspeed_scaler +
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ctl_data.groundspeed_scaler * ctl_data.groundspeed_scaler * (rate_error * _k_p + _integrator);
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groundspeed_scaler * groundspeed_scaler * (rate_error * _k_p + _integrator);
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return math::constrain(_last_output, -1.0f, 1.0f);
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return math::constrain(_last_output, -1.f, 1.f);
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}
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}
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float ECL_WheelController::control_attitude(const float dt, const ECL_ControlData &ctl_data)
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float WheelController::control_attitude(float yaw_setpoint, float yaw)
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{
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{
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/* Do not calculate control signal with bad inputs */
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/* Do not calculate control signal with bad inputs */
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if (!(PX4_ISFINITE(ctl_data.yaw_setpoint) &&
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if (!(PX4_ISFINITE(yaw_setpoint) &&
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PX4_ISFINITE(ctl_data.yaw))) {
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PX4_ISFINITE(yaw))) {
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return _body_rate_setpoint;
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return _body_rate_setpoint;
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}
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}
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/* Calculate the error */
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const float yaw_error = wrap_pi(yaw_setpoint - yaw);
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float yaw_error = wrap_pi(ctl_data.yaw_setpoint - ctl_data.yaw);
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/* Apply P controller: rate setpoint from current error and time constant */
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_body_rate_setpoint = yaw_error / _tc; // assume 0 pitch and roll angle, thus jacobian is simply identity matrix
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_euler_rate_setpoint = yaw_error / _tc;
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_body_rate_setpoint = _euler_rate_setpoint; // assume 0 pitch and roll angle, thus jacobian is simply identity matrix
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/* limit the rate */
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if (_max_rate > 0.01f) {
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if (_max_rate > 0.01f) {
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if (_body_rate_setpoint > 0.0f) {
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if (_body_rate_setpoint > 0.f) {
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_body_rate_setpoint = (_body_rate_setpoint > _max_rate) ? _max_rate : _body_rate_setpoint;
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_body_rate_setpoint = (_body_rate_setpoint > _max_rate) ? _max_rate : _body_rate_setpoint;
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} else {
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} else {
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+32
-28
@@ -1,6 +1,6 @@
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/****************************************************************************
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/****************************************************************************
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*
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*
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* Copyright (c) 2020-2022 PX4 Development Team. All rights reserved.
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* Copyright (c) 2020-2023 PX4 Development Team. All rights reserved.
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*
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*
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* Redistribution and use in source and binary forms, with or without
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* modification, are permitted provided that the following conditions
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@@ -32,44 +32,48 @@
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****************************************************************************/
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****************************************************************************/
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/**
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/**
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* @file ecl_wheel_controller.h
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* @file fw_wheel_controller.h
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* Definition of a simple orthogonal coordinated turn yaw PID controller.
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* Definition of a simple wheel controller.
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*
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* @author Lorenz Meier <lm@inf.ethz.ch>
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* @author Thomas Gubler <thomasgubler@gmail.com>
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* @author Andreas Antener <andreas@uaventure.com>
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*
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* Acknowledgements:
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*
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* The control design is based on a design
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* by Paul Riseborough and Andrew Tridgell, 2013,
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* which in turn is based on initial work of
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* Jonathan Challinger, 2012.
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*/
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*/
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#ifndef ECL_HEADING_CONTROLLER_H
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#ifndef FW_WHEEL_CONTROLLER_H
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#define ECL_HEADING_CONTROLLER_H
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#define FW_WHEEL_CONTROLLER_H
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#include "ecl_controller.h"
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class WheelController
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class ECL_WheelController :
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public ECL_Controller
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{
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{
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public:
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public:
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ECL_WheelController() = default;
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WheelController() = default;
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~ECL_WheelController() = default;
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~WheelController() = default;
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/**
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/**
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* @brief Calculates wheel body rate setpoint.
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* @brief Calculates wheel body rate setpoint.
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*
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*
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* @param dt Time step [s]
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* @param yaw_setpoint yaw setpoint [rad]
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* @param ctrl_data Various control inputs (attitude, body rates, attitdue stepoints, euler rate setpoints, current speeed)
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* @param yaw estimated yaw [rad]
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* @return Wheel body rate setpoint [rad/s]
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* @return Wheel body rate setpoint [rad/s]
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*/
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*/
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float control_attitude(const float dt, const ECL_ControlData &ctl_data) override;
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float control_attitude(float yaw_setpoint, float yaw);
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float control_bodyrate(const float dt, const ECL_ControlData &ctl_data);
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float control_bodyrate(float dt, float body_z_rate, float groundspeed, float groundspeed_scaler);
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float control_euler_rate(const float dt, const ECL_ControlData &ctl_data, float bodyrate_ff) { (void)ctl_data; return 0; }
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void set_time_constant(float time_constant) { _tc = time_constant; }
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void set_k_p(float k_p) { _k_p = k_p; }
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void set_k_i(float k_i) { _k_i = k_i; }
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void set_k_ff(float k_ff) { _k_ff = k_ff; }
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void set_integrator_max(float max) { _integrator_max = max; }
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void set_max_rate(float max_rate) { _max_rate = max_rate; }
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void reset_integrator() { _integrator = 0.f; }
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private:
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float _tc;
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float _k_p;
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float _k_i;
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float _k_ff;
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float _integrator_max;
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float _max_rate;
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float _last_output;
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float _integrator;
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float _body_rate_setpoint;
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};
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};
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#endif // ECL_HEADING_CONTROLLER_H
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#endif // FW_WHEEL_CONTROLLER_H
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