move hover_thrust_estimator to new module (mc_hover_thrust_estimator)

* MC_HTE: unitialize with hover_thrust parameter
* MC_HTE: constrain hover thrust setter between 0.1 and 0.9
* MC_HTE: integrate with land detector and velocity controller
* MCHoverThrustEstimator: Always publish an estimate even when not fusing measurements. This is required as the land detector and the position controller need to receive a hover thrust value.

* MC_HTE: use altitude agl threshold to start the estimator
local_position.z is relative to the origin of the EKF while dist_bottom
is above ground

Co-authored-by: bresch <brescianimathieu@gmail.com>
This commit is contained in:
Daniel Agar
2020-03-11 21:20:54 -04:00
committed by GitHub
parent 4b9e6964f4
commit f9794e99f8
74 changed files with 419 additions and 141 deletions
@@ -0,0 +1,235 @@
/****************************************************************************
*
* Copyright (c) 2020 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
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* POSSIBILITY OF SUCH DAMAGE.
*
****************************************************************************/
/**
* @file hover_thrust_estimator.cpp
*
* @author Mathieu Bresciani <brescianimathieu@gmail.com>
*/
#include "MulticopterHoverThrustEstimator.hpp"
#include <mathlib/mathlib.h>
MulticopterHoverThrustEstimator::MulticopterHoverThrustEstimator() :
ModuleParams(nullptr),
WorkItem(MODULE_NAME, px4::wq_configurations::lp_default)
{
updateParams();
reset();
}
MulticopterHoverThrustEstimator::~MulticopterHoverThrustEstimator()
{
perf_free(_cycle_perf);
}
bool MulticopterHoverThrustEstimator::init()
{
if (!_vehicle_local_position_setpoint_sub.registerCallback()) {
PX4_ERR("vehicle_local_position_setpoint callback registration failed!");
return false;
}
return true;
}
void MulticopterHoverThrustEstimator::reset()
{
_hover_thrust_ekf.setHoverThrust(_param_mpc_thr_hover.get());
_hover_thrust_ekf.setHoverThrustStdDev(_param_hte_ht_err_init.get());
_hover_thrust_ekf.resetAccelNoise();
}
void MulticopterHoverThrustEstimator::updateParams()
{
const float ht_err_init_prev = _param_hte_ht_err_init.get();
ModuleParams::updateParams();
_hover_thrust_ekf.setProcessNoiseStdDev(_param_hte_ht_noise.get());
if (fabsf(_param_hte_ht_err_init.get() - ht_err_init_prev) > FLT_EPSILON) {
_hover_thrust_ekf.setHoverThrustStdDev(_param_hte_ht_err_init.get());
}
_hover_thrust_ekf.setAccelInnovGate(_param_hte_acc_gate.get());
}
void MulticopterHoverThrustEstimator::Run()
{
if (should_exit()) {
_vehicle_local_position_setpoint_sub.unregisterCallback();
exit_and_cleanup();
return;
}
// check for parameter updates
if (_parameter_update_sub.updated()) {
// clear update
parameter_update_s pupdate;
_parameter_update_sub.copy(&pupdate);
// update parameters from storage
updateParams();
}
perf_begin(_cycle_perf);
vehicle_land_detected_s vehicle_land_detected;
vehicle_status_s vehicle_status;
vehicle_local_position_s local_pos;
if (_vehicle_land_detected_sub.update(&vehicle_land_detected)) {
_landed = vehicle_land_detected.landed;
}
if (_vehicle_status_sub.update(&vehicle_status)) {
_armed = (vehicle_status.arming_state == vehicle_status_s::ARMING_STATE_ARMED);
}
if (_vehicle_local_pos_sub.update(&local_pos)) {
// This is only necessary because the landed
// flag of the land detector does not guarantee that
// the vehicle does not touch the ground anymore
// TODO: improve the landed flag
_in_air = local_pos.dist_bottom > 1.f;
}
ZeroOrderHoverThrustEkf::status status{};
if (_armed && !_landed && _in_air) {
vehicle_local_position_setpoint_s local_pos_sp;
if (_vehicle_local_position_setpoint_sub.update(&local_pos_sp)) {
const hrt_abstime now = hrt_absolute_time();
const float dt = math::constrain((now - _timestamp_last) / 1e6f, 0.002f, 0.2f);
_hover_thrust_ekf.predict(dt);
if (PX4_ISFINITE(local_pos.az) && PX4_ISFINITE(local_pos_sp.thrust[2])) {
// Inform the hover thrust estimator about the measured vertical
// acceleration (positive acceleration is up) and the current thrust (positive thrust is up)
_hover_thrust_ekf.fuseAccZ(-local_pos.az, -local_pos_sp.thrust[2], status);
}
}
} else {
if (!_armed) {
reset();
}
status.hover_thrust = _hover_thrust_ekf.getHoverThrustEstimate();
status.hover_thrust_var = _hover_thrust_ekf.getHoverThrustEstimateVar();
status.accel_noise_var = _hover_thrust_ekf.getAccelNoiseVar();
status.innov = NAN;
status.innov_var = NAN;
status.innov_test_ratio = NAN;
}
publishStatus(status);
perf_end(_cycle_perf);
}
void MulticopterHoverThrustEstimator::publishStatus(ZeroOrderHoverThrustEkf::status &status)
{
hover_thrust_estimate_s status_msg{};
status_msg.hover_thrust = status.hover_thrust;
status_msg.hover_thrust_var = status.hover_thrust_var;
status_msg.accel_innov = status.innov;
status_msg.accel_innov_var = status.innov_var;
status_msg.accel_innov_test_ratio = status.innov_test_ratio;
status_msg.accel_noise_var = status.accel_noise_var;
status_msg.timestamp = hrt_absolute_time();
_hover_thrust_ekf_pub.publish(status_msg);
}
int MulticopterHoverThrustEstimator::task_spawn(int argc, char *argv[])
{
MulticopterHoverThrustEstimator *instance = new MulticopterHoverThrustEstimator();
if (instance) {
_object.store(instance);
_task_id = task_id_is_work_queue;
if (instance->init()) {
return PX4_OK;
}
} else {
PX4_ERR("alloc failed");
}
delete instance;
_object.store(nullptr);
_task_id = -1;
return PX4_ERROR;
}
int MulticopterHoverThrustEstimator::custom_command(int argc, char *argv[])
{
return print_usage("unknown command");
}
int MulticopterHoverThrustEstimator::print_status()
{
perf_print_counter(_cycle_perf);
return 0;
}
int MulticopterHoverThrustEstimator::print_usage(const char *reason)
{
if (reason) {
PX4_WARN("%s\n", reason);
}
PRINT_MODULE_DESCRIPTION(
R"DESCR_STR(
### Description
)DESCR_STR");
PRINT_MODULE_USAGE_NAME("mc_hover_thrust_estimator", "estimator");
PRINT_MODULE_USAGE_COMMAND("start");
PRINT_MODULE_USAGE_DEFAULT_COMMANDS();
return 0;
}
extern "C" __EXPORT int mc_hover_thrust_estimator_main(int argc, char *argv[])
{
return MulticopterHoverThrustEstimator::main(argc, argv);
}