fw atune: add fixed-wing auto-tuning module

This commit is contained in:
bresch
2021-10-01 17:09:55 +02:00
committed by Mathieu Bresciani
parent 8dfdb1e3db
commit 55f0860c31
7 changed files with 1048 additions and 2 deletions
+6
View File
@@ -16,6 +16,12 @@ ekf2 start &
fw_att_control start
fw_pos_control_l1 start
airspeed_selector start
#
# Start attitude control auto-tuner
#
fw_autotune_attitude_control start
#
# Start Land Detector.
#
+2
View File
@@ -24,9 +24,11 @@ mc_att_control start vtol
flight_mode_manager start
mc_pos_control start vtol
mc_hover_thrust_estimator start
mc_autotune_attitude_control start
fw_att_control start vtol
fw_pos_control_l1 start vtol
fw_autotune_attitude_control start vtol
# Start Land Detector
# Multicopter for now until we have something for VTOL
@@ -0,0 +1,47 @@
############################################################################
#
# Copyright (c) 2020-2021 PX4 Development Team. All rights reserved.
#
# 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.
#
############################################################################
px4_add_module(
MODULE fw_autotune_attitude_control
MAIN fw_autotune_attitude_control
COMPILE_FLAGS
${MAX_CUSTOM_OPT_LEVEL}
SRCS
fw_autotune_attitude_control.cpp
fw_autotune_attitude_control.hpp
DEPENDS
hysteresis
mathlib
px4_work_queue
SystemIdentification
)
File diff suppressed because it is too large Load Diff
@@ -0,0 +1,202 @@
/****************************************************************************
*
* Copyright (c) 2020-2021 PX4 Development Team. All rights reserved.
*
* 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.
*
****************************************************************************/
/**
* @file fw_autotune_attitude_control.hpp
*
* @author Mathieu Bresciani <mathieu@auterion.com>
*/
#pragma once
#include <drivers/drv_hrt.h>
#include <lib/mathlib/math/filter/AlphaFilter.hpp>
#include <lib/perf/perf_counter.h>
#include <lib/pid_design/pid_design.hpp>
#include <lib/system_identification/system_identification.hpp>
#include <px4_platform_common/defines.h>
#include <px4_platform_common/module.h>
#include <px4_platform_common/module_params.h>
#include <px4_platform_common/posix.h>
#include <px4_platform_common/px4_work_queue/WorkItem.hpp>
#include <uORB/Publication.hpp>
#include <uORB/Subscription.hpp>
#include <uORB/SubscriptionCallback.hpp>
#include <uORB/topics/actuator_controls.h>
#include <uORB/topics/actuator_controls_status.h>
#include <uORB/topics/manual_control_setpoint.h>
#include <uORB/topics/parameter_update.h>
#include <uORB/topics/autotune_attitude_control_status.h>
#include <uORB/topics/vehicle_angular_velocity.h>
#include <uORB/topics/vehicle_status.h>
#include <mathlib/mathlib.h>
using namespace time_literals;
class FwAutotuneAttitudeControl : public ModuleBase<FwAutotuneAttitudeControl>, public ModuleParams,
public px4::WorkItem
{
public:
FwAutotuneAttitudeControl(bool is_vtol);
~FwAutotuneAttitudeControl() override;
/** @see ModuleBase */
static int task_spawn(int argc, char *argv[]);
/** @see ModuleBase */
static int custom_command(int argc, char *argv[]);
/** @see ModuleBase */
static int print_usage(const char *reason = nullptr);
bool init();
/** @see ModuleBase::print_status() */
int print_status() override;
private:
enum Axes : int32_t {
roll = (1 << 0),
pitch = (1 << 1),
yaw = (1 << 2)
};
void Run() override;
void reset();
void checkFilters();
void updateStateMachine(hrt_abstime now);
bool registerActuatorControlsCallback();
void stopAutotune();
void copyGains(int index);
bool areGainsGood() const;
void saveGainsToParams();
void backupAndSaveGainsToParams();
void revertParamGains();
const matrix::Vector3f getIdentificationSignal();
uORB::SubscriptionCallbackWorkItem _actuator_controls_sub;
uORB::SubscriptionCallbackWorkItem _parameter_update_sub{this, ORB_ID(parameter_update)};
uORB::Subscription _actuator_controls_status_sub;
uORB::Subscription _manual_control_setpoint_sub{ORB_ID(manual_control_setpoint)};
uORB::Subscription _vehicle_angular_velocity_sub{ORB_ID(vehicle_angular_velocity)};
uORB::Subscription _vehicle_status_sub{ORB_ID(vehicle_status)};
uORB::PublicationData<autotune_attitude_control_status_s> _autotune_attitude_control_status_pub{ORB_ID(autotune_attitude_control_status)};
SystemIdentification _sys_id;
enum class state {
idle = autotune_attitude_control_status_s::STATE_IDLE,
init = autotune_attitude_control_status_s::STATE_INIT,
roll = autotune_attitude_control_status_s::STATE_ROLL,
roll_pause = autotune_attitude_control_status_s::STATE_ROLL_PAUSE,
pitch = autotune_attitude_control_status_s::STATE_PITCH,
pitch_pause = autotune_attitude_control_status_s::STATE_PITCH_PAUSE,
yaw = autotune_attitude_control_status_s::STATE_YAW,
yaw_pause = autotune_attitude_control_status_s::STATE_YAW_PAUSE,
apply = autotune_attitude_control_status_s::STATE_APPLY,
test = autotune_attitude_control_status_s::STATE_TEST,
verification = autotune_attitude_control_status_s::STATE_VERIFICATION,
complete = autotune_attitude_control_status_s::STATE_COMPLETE,
fail = autotune_attitude_control_status_s::STATE_FAIL,
wait_for_disarm = autotune_attitude_control_status_s::STATE_WAIT_FOR_DISARM
} _state{state::idle};
hrt_abstime _state_start_time{0};
uint8_t _steps_counter{0};
uint8_t _max_steps{5};
int8_t _signal_sign{0};
bool _armed{false};
matrix::Vector3f _kiff{};
matrix::Vector3f _rate_k{};
matrix::Vector3f _rate_i{};
matrix::Vector3f _rate_ff{};
float _attitude_p{0.f};
matrix::Vector3f _att_p{};
matrix::Vector3f _control_power{};
bool _gains_backup_available{false}; // true if a backup of the parameters has been done
/**
* Scale factor applied to the input data to have the same input/output range
* When input and output scales are a lot different, some elements of the covariance
* matrix will collapse much faster than other ones, creating an ill-conditionned matrix
*/
float _input_scale{1.f};
hrt_abstime _last_run{0};
hrt_abstime _last_publish{0};
float _interval_sum{0.f};
float _interval_count{0.f};
float _sample_interval_avg{0.01f};
float _filter_sample_rate{1.f};
bool _are_filters_initialized{false};
AlphaFilter<float> _signal_filter; ///< used to create a wash-out filter
perf_counter_t _cycle_perf{perf_alloc(PC_ELAPSED, MODULE_NAME": cycle time")};
DEFINE_PARAMETERS(
(ParamInt<px4::params::FW_AT_AXES>) _param_fw_at_axes,
(ParamBool<px4::params::FW_AT_START>) _param_fw_at_start,
(ParamFloat<px4::params::FW_AT_SYSID_AMP>) _param_fw_at_sysid_amp,
(ParamInt<px4::params::FW_AT_APPLY>) _param_fw_at_apply,
(ParamFloat<px4::params::IMU_GYRO_CUTOFF>) _param_imu_gyro_cutoff,
(ParamFloat<px4::params::FW_RR_P>) _param_fw_rr_p,
(ParamFloat<px4::params::FW_RR_I>) _param_fw_rr_i,
(ParamFloat<px4::params::FW_RR_FF>) _param_fw_rr_ff,
(ParamFloat<px4::params::FW_R_TC>) _param_fw_r_tc,
(ParamFloat<px4::params::FW_PR_P>) _param_fw_pr_p,
(ParamFloat<px4::params::FW_PR_I>) _param_fw_pr_i,
(ParamFloat<px4::params::FW_PR_FF>) _param_fw_pr_ff,
(ParamFloat<px4::params::FW_P_TC>) _param_fw_p_tc,
(ParamFloat<px4::params::FW_YR_P>) _param_fw_yr_p,
(ParamFloat<px4::params::FW_YR_I>) _param_fw_yr_i,
(ParamFloat<px4::params::FW_YR_FF>) _param_fw_yr_ff
)
static constexpr float _publishing_dt_s = 100e-3f;
static constexpr hrt_abstime _publishing_dt_hrt = 100_ms;
};
@@ -0,0 +1,105 @@
/****************************************************************************
*
* Copyright (c) 2020-2021 PX4 Development Team. All rights reserved.
*
* 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.
*
****************************************************************************/
/**
* @file fw_autotune_attitude_control_params.c
*
* Parameters used by the attitude auto-tuner
*
* @author Mathieu Bresciani <mathieu@auterion.com>
*/
/**
* Start the autotuning sequence
*
* WARNING: this will inject steps to the rate controller
* and can be dangerous. Only activate if you know what you
* are doing, and in a safe environment.
*
* Any motion of the remote stick will abord the signal
* injection and reset this parameter
* Best is to perform the identification in position or
* hold mode.
* Increase the amplitude of the injected signal using
* FW_AT_SYSID_AMP for more signal/noise ratio
*
* @boolean
* @group Autotune
*/
PARAM_DEFINE_INT32(FW_AT_START, 0);
/**
* Amplitude of the injected signal
*
* This parameter scales the signal sent to the
* rate controller during system identification.
*
* @min 0.1
* @max 6.0
* @decimal 1
* @group Autotune
*/
PARAM_DEFINE_FLOAT(FW_AT_SYSID_AMP, 1.0);
/**
* Controls when to apply the new gains
*
* After the auto-tuning sequence is completed,
* a new set of gains is available and can be applied
* immediately or after landing.
*
* @value 0 Do not apply the new gains (logging only)
* @value 1 Apply the new gains after disarm
* @value 2 Apply the new gains in air
* @group Autotune
*/
PARAM_DEFINE_INT32(FW_AT_APPLY, 2);
/**
* Tuning axes selection
*
* Defines which axes will be tuned during the auto-tuning sequence
*
* Set bits in the following positions to enable:
* 0 : Roll
* 1 : Pitch
* 2 : Yaw
*
* @bit 0 roll
* @bit 1 pitch
* @bit 2 yaw
* @min 1
* @max 7
* @group Autotune
*/
PARAM_DEFINE_INT32(FW_AT_AXES, 3);
+1 -2
View File
@@ -598,8 +598,7 @@ void MavlinkReceiver::handle_message_command_both(mavlink_message_t *msg, const
switch (vehicle_status.vehicle_type) {
case vehicle_status_s::VEHICLE_TYPE_FIXED_WING:
/* atune_start = param_find("FW_AT_START"); */
atune_start = PARAM_INVALID;
atune_start = param_find("FW_AT_START");
break;