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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-11-08 19:51:36 +08:00
Use common rate control library
Increase ground speed trim Use rate control for pos control Controls
This commit is contained in:
@@ -13,7 +13,7 @@ param set-default GND_SPEED_I 8
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param set-default GND_SPEED_IMAX 0.125
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param set-default GND_SPEED_P 2
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param set-default GND_SPEED_THR_SC 1
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param set-default GND_SPEED_TRIM 1
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param set-default GND_SPEED_TRIM 3
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param set-default GND_THR_CRUISE 0.85
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param set-default GND_THR_MAX 1
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param set-default GND_THR_MIN 0
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@@ -31,8 +31,6 @@
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#
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############################################################################
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add_subdirectory(RoverRateControl)
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px4_add_module(
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MODULE modules__rover_pos_control
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MAIN rover_pos_control
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@@ -40,7 +38,7 @@ px4_add_module(
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RoverPositionControl.cpp
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RoverPositionControl.hpp
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DEPENDS
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RoverRateControl
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RateControl
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l1
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pid
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)
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@@ -318,14 +318,20 @@ RoverPositionControl::control_position(const matrix::Vector2d ¤t_position,
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prev_wp(1));
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_gnd_control.navigate_waypoints(prev_wp_local, curr_wp_local, curr_pos_local, ground_speed_2d);
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_act_controls.control[actuator_controls_s::INDEX_THROTTLE] = mission_throttle;
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///WIP: Convert Lateral acceleration demand to rate control reference
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float min_speed{1.0};
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matrix::Vector2f saturated_speed_2d = (ground_speed_2d.norm() < min_speed) ? ground_speed_2d :
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ground_speed_2d.normalized() * min_speed;
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float desired_r = ground_speed_2d.norm_squared() / math::abs_t(_gnd_control.nav_lateral_acceleration_demand());
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float desired_theta = (0.5f * M_PI_F) - atan2f(desired_r, _param_wheel_base.get());
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float control_effort = (desired_theta / _param_max_turn_angle.get()) * sign(
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_gnd_control.nav_lateral_acceleration_demand());
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control_effort = math::constrain(control_effort, -1.0f, 1.0f);
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_act_controls.control[actuator_controls_s::INDEX_YAW] = control_effort;
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float desired_yaw_rate = _gnd_control.nav_lateral_acceleration_demand() / saturated_speed_2d.norm();
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_rates_sp.roll = 0.0;
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_rates_sp.pitch = 0.0;
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_rates_sp.yaw = desired_yaw_rate;
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_rates_sp.thrust_body[0] = math::constrain(mission_throttle, 0.0f, 1.0f);
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_rates_sp.timestamp = hrt_absolute_time();
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_rates_sp_pub.publish(_rates_sp);
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control_rates(_vehicle_rates, _vehicle_angular_acceleration, _local_pos, _rates_sp);
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}
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}
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break;
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@@ -433,6 +439,8 @@ RoverPositionControl::control_rates(const vehicle_angular_velocity_s &rates, con
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dt = hrt_elapsed_time(&_control_rates_last_called) * 1e-6f;
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}
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_control_rates_last_called = hrt_absolute_time();
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const matrix::Vector3f current_velocity(local_pos.vx, local_pos.vy, local_pos.vz);
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const matrix::Vector3f vehicle_rates(rates.xyz[0], rates.xyz[1], rates.xyz[2]);
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const matrix::Vector3f rates_setpoint(rates_sp.roll, rates_sp.pitch, rates_sp.yaw);
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@@ -472,7 +480,7 @@ RoverPositionControl::Run()
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/* update parameters from storage */
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parameters_update();
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if (!is_finite(_steering_input)) {
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if (!PX4_ISFINITE(_steering_input)) {
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_steering_input = 0.0;
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}
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@@ -41,7 +41,6 @@
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* @author Marco Zorzi <mzorzi@student.ethz.ch>
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*/
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#include <RoverRateControl.hpp>
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#include <float.h>
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#include <drivers/drv_hrt.h>
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@@ -50,6 +49,7 @@
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#include <lib/mathlib/mathlib.h>
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#include <lib/perf/perf_counter.h>
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#include <lib/pid/pid.h>
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#include <lib/rate_control/rate_control.hpp>
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#include <px4_platform_common/px4_config.h>
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#include <px4_platform_common/defines.h>
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#include <px4_platform_common/posix.h>
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@@ -134,6 +134,9 @@ private:
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vehicle_local_position_s _local_pos{}; /**< global vehicle position */
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actuator_controls_s _act_controls{}; /**< direct control of actuators */
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vehicle_attitude_s _vehicle_att{};
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vehicle_angular_acceleration_s _vehicle_angular_acceleration{};
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vehicle_angular_velocity_s _vehicle_rates{};
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trajectory_setpoint_s _trajectory_setpoint{};
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uORB::Publication<vehicle_thrust_setpoint_s> _vehicle_thrust_setpoint_pub{ORB_ID(vehicle_thrust_setpoint)};
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uORB::Publication<vehicle_torque_setpoint_s> _vehicle_torque_setpoint_pub{ORB_ID(vehicle_torque_setpoint)};
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@@ -157,7 +160,7 @@ private:
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uint8_t _pos_reset_counter{0}; // captures the number of times the estimator has reset the horizontal position
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ECL_L1_Pos_Controller _gnd_control;
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RoverRateControl _rate_control;
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RateControl _rate_control;
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float _steering_input{0.0};
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enum UGV_POSCTRL_MODE {
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@@ -1,42 +0,0 @@
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############################################################################
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#
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# Copyright (c) 2019 PX4 Development Team. All rights reserved.
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#
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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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# are met:
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#
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# 1. Redistributions of source code must retain the above copyright
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# notice, this list of conditions and the following disclaimer.
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# 2. Redistributions in binary form must reproduce the above copyright
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# notice, this list of conditions and the following disclaimer in
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# the documentation and/or other materials provided with the
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# distribution.
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# 3. Neither the name PX4 nor the names of its contributors may be
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# used to endorse or promote products derived from this software
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# without specific prior written permission.
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#
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# THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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# "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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# LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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# FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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# COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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# INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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# BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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# OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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# AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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# LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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# ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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# POSSIBILITY OF SUCH DAMAGE.
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#
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############################################################################
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px4_add_library(RoverRateControl
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RoverRateControl.cpp
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RoverRateControl.hpp
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)
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target_compile_options(RoverRateControl PRIVATE ${MAX_CUSTOM_OPT_LEVEL})
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target_include_directories(RoverRateControl PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
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target_link_libraries(RoverRateControl PRIVATE mathlib)
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px4_add_unit_gtest(SRC RoverRateControlTest.cpp LINKLIBS RoverRateControl)
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@@ -1,104 +0,0 @@
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/****************************************************************************
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*
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* Copyright (c) 2019 PX4 Development Team. All rights reserved.
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*
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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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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file RoverRateControl.cpp
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*/
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#include <RoverRateControl.hpp>
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#include <px4_platform_common/defines.h>
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using namespace matrix;
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void RoverRateControl::setGains(const Vector3f &P, const Vector3f &I, const Vector3f &D)
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{
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_gain_p = P;
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_gain_i = I;
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_gain_d = D;
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}
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Vector3f RoverRateControl::update(const Vector3f &rate, const Vector3f &rate_sp, const Vector3f &angular_accel,
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const float dt, const bool landed)
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{
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// angular rates error
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Vector3f rate_error = rate_sp - rate;
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// PID control with feed forward
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const Vector3f torque = _gain_p.emult(rate_error) + _rate_int - _gain_d.emult(angular_accel) + _gain_ff.emult(rate_sp);
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// update integral only if we are not landed
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if (!landed) {
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updateIntegral(rate_error, dt);
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}
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return torque;
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}
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void RoverRateControl::updateIntegral(Vector3f &rate_error, const float dt)
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{
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for (int i = 0; i < 3; i++) {
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// prevent further positive control saturation
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if (_mixer_saturation_positive[i]) {
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rate_error(i) = math::min(rate_error(i), 0.f);
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}
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// prevent further negative control saturation
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if (_mixer_saturation_negative[i]) {
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rate_error(i) = math::max(rate_error(i), 0.f);
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}
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// I term factor: reduce the I gain with increasing rate error.
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// This counteracts a non-linear effect where the integral builds up quickly upon a large setpoint
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// change (noticeable in a bounce-back effect after a flip).
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// The formula leads to a gradual decrease w/o steps, while only affecting the cases where it should:
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// with the parameter set to 400 degrees, up to 100 deg rate error, i_factor is almost 1 (having no effect),
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// and up to 200 deg error leads to <25% reduction of I.
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float i_factor = rate_error(i) / math::radians(400.f);
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i_factor = math::max(0.0f, 1.f - i_factor * i_factor);
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// Perform the integration using a first order method
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float rate_i = _rate_int(i) + i_factor * _gain_i(i) * rate_error(i) * dt;
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// do not propagate the result if out of range or invalid
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if (PX4_ISFINITE(rate_i)) {
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_rate_int(i) = math::constrain(rate_i, -_lim_int(i), _lim_int(i));
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}
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}
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}
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void RoverRateControl::getRoverRateControlStatus(rate_ctrl_status_s &rate_ctrl_status)
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{
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rate_ctrl_status.rollspeed_integ = _rate_int(0);
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rate_ctrl_status.pitchspeed_integ = _rate_int(1);
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rate_ctrl_status.yawspeed_integ = _rate_int(2);
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}
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@@ -1,110 +0,0 @@
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/****************************************************************************
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*
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* Copyright (c) 2019-2021 PX4 Development Team. All rights reserved.
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*
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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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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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||||
* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file RoverRateControl.hpp
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*
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* PID 3 axis angular rate / angular velocity control.
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*/
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#pragma once
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#include <matrix/matrix/math.hpp>
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#include <mathlib/mathlib.h>
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#include <uORB/topics/rate_ctrl_status.h>
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class RoverRateControl
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{
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public:
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RoverRateControl() = default;
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~RoverRateControl() = default;
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/**
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* Set the rate control gains
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* @param P 3D vector of proportional gains for body x,y,z axis
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* @param I 3D vector of integral gains
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* @param D 3D vector of derivative gains
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*/
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void setGains(const matrix::Vector3f &P, const matrix::Vector3f &I, const matrix::Vector3f &D);
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/**
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* Set the mximum absolute value of the integrator for all axes
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* @param integrator_limit limit value for all axes x, y, z
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*/
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void setIntegratorLimit(const matrix::Vector3f &integrator_limit) { _lim_int = integrator_limit; };
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/**
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* Set direct rate to torque feed forward gain
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* @see _gain_ff
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* @param FF 3D vector of feed forward gains for body x,y,z axis
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*/
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void setFeedForwardGain(const matrix::Vector3f &FF) { _gain_ff = FF; };
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/**
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* Run one control loop cycle calculation
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* @param rate estimation of the current vehicle angular rate
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* @param rate_sp desired vehicle angular rate setpoint
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* @param dt desired vehicle angular rate setpoint
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* @return [-1,1] normalized torque vector to apply to the vehicle
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*/
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matrix::Vector3f update(const matrix::Vector3f &rate, const matrix::Vector3f &rate_sp,
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const matrix::Vector3f &angular_accel, const float dt, const bool landed);
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/**
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* Set the integral term to 0 to prevent windup
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* @see _rate_int
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*/
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void resetIntegral() { _rate_int.zero(); }
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/**
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* Get status message of controller for logging/debugging
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* @param rate_ctrl_status status message to fill with internal states
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*/
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void getRoverRateControlStatus(rate_ctrl_status_s &rate_ctrl_status);
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private:
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void updateIntegral(matrix::Vector3f &rate_error, const float dt);
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// Gains
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matrix::Vector3f _gain_p; ///< rate control proportional gain for all axes x, y, z
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matrix::Vector3f _gain_i; ///< rate control integral gain
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matrix::Vector3f _gain_d; ///< rate control derivative gain
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matrix::Vector3f _lim_int; ///< integrator term maximum absolute value
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matrix::Vector3f _gain_ff; ///< direct rate to torque feed forward gain only useful for helicopters
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// States
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matrix::Vector3f _rate_int; ///< integral term of the rate controller
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bool _mixer_saturation_positive[3] {};
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bool _mixer_saturation_negative[3] {};
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};
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@@ -1,44 +0,0 @@
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/****************************************************************************
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*
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* Copyright (C) 2019 PX4 Development Team. All rights reserved.
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||||
*
|
||||
* Redistribution and use in source and binary forms, with or without
|
||||
* modification, are permitted provided that the following conditions
|
||||
* are met:
|
||||
*
|
||||
* 1. Redistributions of source code must retain the above copyright
|
||||
* notice, this list of conditions and the following disclaimer.
|
||||
* 2. Redistributions in binary form must reproduce the above copyright
|
||||
* notice, this list of conditions and the following disclaimer in
|
||||
* the documentation and/or other materials provided with the
|
||||
* distribution.
|
||||
* 3. Neither the name PX4 nor the names of its contributors may be
|
||||
* used to endorse or promote products derived from this software
|
||||
* without specific prior written permission.
|
||||
*
|
||||
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
||||
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
||||
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
||||
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
||||
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
||||
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
||||
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
||||
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
||||
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
||||
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
||||
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
||||
* POSSIBILITY OF SUCH DAMAGE.
|
||||
*
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****************************************************************************/
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#include <gtest/gtest.h>
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#include <RoverRateControl.hpp>
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using namespace matrix;
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TEST(RoverRateControlTest, AllZeroCase)
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{
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RoverRateControl rate_control;
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Vector3f torque = rate_control.update(Vector3f(), Vector3f(), Vector3f(), 0.f, false);
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EXPECT_EQ(torque, Vector3f());
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}
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