forked from Archive/PX4-Autopilot
sensors/vehicle_imu: Integrator simplify and make header only
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0b9e4a5902
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@ -32,7 +32,6 @@
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############################################################################
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px4_add_library(vehicle_imu
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Integrator.cpp
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Integrator.hpp
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VehicleIMU.cpp
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VehicleIMU.hpp
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@ -1,97 +0,0 @@
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/****************************************************************************
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*
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* Copyright (c) 2015-2020 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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#include "Integrator.hpp"
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#include <drivers/drv_hrt.h>
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using matrix::Vector3f;
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bool Integrator::put(const hrt_abstime ×tamp, const Vector3f &val)
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{
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if ((_last_integration_time == 0) || (timestamp <= _last_integration_time)) {
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/* this is the first item in the integrator */
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_last_integration_time = timestamp;
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_last_reset_time = timestamp;
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_last_val = val;
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return false;
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}
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// Use trapezoidal integration to calculate the delta integral
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const float dt = static_cast<float>(timestamp - _last_integration_time) * 1e-6f;
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const matrix::Vector3f delta_alpha = (val + _last_val) * dt * 0.5f;
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_last_val = val;
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_last_integration_time = timestamp;
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_integrated_samples++;
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// Calculate coning corrections if required
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if (_coning_comp_on) {
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// Coning compensation derived by Paul Riseborough and Jonathan Challinger,
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// following:
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// Tian et al (2010) Three-loop Integration of GPS and Strapdown INS with Coning and Sculling Compensation
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// Sourced: http://www.sage.unsw.edu.au/snap/publications/tian_etal2010b.pdf
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// Simulated: https://github.com/priseborough/InertialNav/blob/master/models/imu_error_modelling.m
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_beta += ((_last_alpha + _last_delta_alpha * (1.f / 6.f)) % delta_alpha) * 0.5f;
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_last_delta_alpha = delta_alpha;
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_last_alpha = _alpha;
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}
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// accumulate delta integrals
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_alpha += delta_alpha;
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return true;
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}
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bool Integrator::reset(Vector3f &integral, uint32_t &integral_dt)
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{
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if (integral_ready()) {
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integral = Vector3f{_alpha};
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_alpha.zero();
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integral_dt = (_last_integration_time - _last_reset_time);
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_last_reset_time = _last_integration_time;
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_integrated_samples = 0;
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// apply coning corrections if required
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if (_coning_comp_on) {
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integral += _beta;
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_beta.zero();
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_last_alpha.zero();
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}
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return true;
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}
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return false;
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}
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@ -48,7 +48,7 @@
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class Integrator
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{
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public:
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Integrator(bool coning_compensation = false) : _coning_comp_on(coning_compensation) {}
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Integrator() = default;
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~Integrator() = default;
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/**
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@ -58,29 +58,23 @@ public:
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* @param val Item to put.
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* @return true if data was accepted and integrated.
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*/
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bool put(const uint64_t ×tamp, const matrix::Vector3f &val);
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/**
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* Put an item into the integral.
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*
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* @param timestamp Timestamp of the current value.
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* @param val Item to put.
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* @param integral Current integral in case the integrator did reset, else the value will not be modified
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* @param integral_dt Get the dt in us of the current integration (only if reset).
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* @return true if putting the item triggered an integral reset and the integral should be
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* published.
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*/
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bool put(const uint64_t ×tamp, const matrix::Vector3f &val, matrix::Vector3f &integral, uint32_t &integral_dt)
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inline void put(const matrix::Vector3f &val, const float dt)
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{
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return put(timestamp, val) && reset(integral, integral_dt);
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if (dt > 0.f && dt <= (_reset_interval_min * 2.f)) {
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_alpha += integrate(val, dt);
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} else {
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reset();
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_last_val = val;
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}
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}
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/**
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* Set reset interval during runtime. This won't reset the integrator.
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*
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* @param reset_interval New reset time interval for the integrator.
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* @param reset_interval New reset time interval for the integrator in microseconds.
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*/
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void set_reset_interval(uint32_t reset_interval) { _reset_interval_min = reset_interval; }
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void set_reset_interval(uint32_t reset_interval_us) { _reset_interval_min = reset_interval_us * 1e-6f; }
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/**
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* Set required samples for reset. This won't reset the integrator.
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@ -95,29 +89,123 @@ public:
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*
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* @return true if integrator has sufficient data (minimum interval & samples satisfied) to reset.
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*/
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bool integral_ready() const { return (_integrated_samples >= _reset_samples_min) || (_last_integration_time >= (_last_reset_time + _reset_interval_min)); }
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inline bool integral_ready() const { return (_integrated_samples >= _reset_samples_min) || (_integral_dt >= _reset_interval_min); }
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void reset()
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{
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_alpha.zero();
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_integral_dt = 0;
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_integrated_samples = 0;
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}
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/* Reset integrator and return current integral & integration time
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*
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* @param integral_dt Get the dt in us of the current integration.
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* @return true if integral valid
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*/
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bool reset(matrix::Vector3f &integral, uint32_t &integral_dt);
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bool reset(matrix::Vector3f &integral, uint32_t &integral_dt)
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{
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if (integral_ready()) {
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integral = _alpha;
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integral_dt = roundf(_integral_dt * 1e6f); // seconds to microseconds
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private:
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uint64_t _last_integration_time{0}; /**< timestamp of the last integration step */
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uint64_t _last_reset_time{0}; /**< last auto-announcement of integral value */
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reset();
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matrix::Vector3f _alpha{0.f, 0.f, 0.f}; /**< integrated value before coning corrections are applied */
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matrix::Vector3f _last_alpha{0.f, 0.f, 0.f}; /**< previous value of _alpha */
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matrix::Vector3f _beta{0.f, 0.f, 0.f}; /**< accumulated coning corrections */
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matrix::Vector3f _last_val{0.f, 0.f, 0.f}; /**< previous input */
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matrix::Vector3f _last_delta_alpha{0.f, 0.f, 0.f}; /**< integral from previous previous sampling interval */
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return true;
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}
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uint32_t _reset_interval_min{1}; /**< the interval after which the content will be published and the integrator reset */
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return false;
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}
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uint8_t _integrated_samples{0};
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protected:
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inline matrix::Vector3f integrate(const matrix::Vector3f &val, const float dt)
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{
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// Use trapezoidal integration to calculate the delta integral
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_integrated_samples++;
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_integral_dt += dt;
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const matrix::Vector3f delta_alpha{(val + _last_val) *dt * 0.5f};
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_last_val = val;
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return delta_alpha;
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}
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matrix::Vector3f _alpha{0.f, 0.f, 0.f}; /**< integrated value before coning corrections are applied */
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matrix::Vector3f _last_val{0.f, 0.f, 0.f}; /**< previous input */
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float _integral_dt{0};
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float _reset_interval_min{0.005f}; /**< the interval after which the content will be published and the integrator reset */
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uint8_t _reset_samples_min{1};
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const bool _coning_comp_on{false}; /**< true to turn on coning corrections */
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uint8_t _integrated_samples{0};
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};
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class IntegratorConing : public Integrator
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{
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public:
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IntegratorConing() = default;
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~IntegratorConing() = default;
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/**
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* Put an item into the integral.
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*
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* @param timestamp Timestamp of the current value.
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* @param val Item to put.
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* @return true if data was accepted and integrated.
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*/
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inline void put(const matrix::Vector3f &val, const float dt)
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{
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if (dt > 0.f && dt <= (_reset_interval_min * 2.f)) {
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// Use trapezoidal integration to calculate the delta integral
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const matrix::Vector3f delta_alpha{integrate(val, dt)};
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// Calculate coning corrections
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// Coning compensation derived by Paul Riseborough and Jonathan Challinger,
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// following:
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// Strapdown Inertial Navigation Integration Algorithm Design Part 1: Attitude Algorithms
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// Sourced: https://arc.aiaa.org/doi/pdf/10.2514/2.4228
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// Simulated: https://github.com/priseborough/InertialNav/blob/master/models/imu_error_modelling.m
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_beta += ((_last_alpha + _last_delta_alpha * (1.f / 6.f)) % delta_alpha) * 0.5f;
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_last_delta_alpha = delta_alpha;
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_last_alpha = _alpha;
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// accumulate delta integrals
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_alpha += delta_alpha;
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} else {
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reset();
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_last_val = val;
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}
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}
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void reset()
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{
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Integrator::reset();
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_beta.zero();
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_last_alpha.zero();
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}
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/* Reset integrator and return current integral & integration time
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*
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* @param integral_dt Get the dt in us of the current integration.
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* @return true if integral valid
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*/
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bool reset(matrix::Vector3f &integral, uint32_t &integral_dt)
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{
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if (Integrator::reset(integral, integral_dt)) {
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// apply coning corrections
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integral += _beta;
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_beta.zero();
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_last_alpha.zero();
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return true;
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}
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return false;
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}
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private:
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matrix::Vector3f _beta{0.f, 0.f, 0.f}; /**< accumulated coning corrections */
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matrix::Vector3f _last_delta_alpha{0.f, 0.f, 0.f}; /**< integral from previous previous sampling interval */
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matrix::Vector3f _last_alpha{0.f, 0.f, 0.f}; /**< previous value of _alpha */
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};
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@ -1,6 +1,6 @@
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/****************************************************************************
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*
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* Copyright (c) 2020 PX4 Development Team. All rights reserved.
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* Copyright (c) 2020-2021 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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@ -249,9 +249,11 @@ void VehicleIMU::Run()
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_gyro_temperature += gyro.temperature;
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_gyro_sum_count++;
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_gyro_integrator.put(gyro.timestamp_sample, gyro_raw);
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const float dt = (gyro.timestamp_sample - _last_timestamp_sample_gyro) * 1e-6f;
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_last_timestamp_sample_gyro = gyro.timestamp_sample;
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_gyro_integrator.put(gyro_raw, dt);
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// break if interval is configured and we haven't fallen behind
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if (_intervals_configured && _gyro_integrator.integral_ready()
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&& (hrt_elapsed_time(&gyro.timestamp) < _imu_integration_interval_us) && !sensor_data_gap) {
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@ -296,9 +298,11 @@ void VehicleIMU::Run()
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_accel_temperature += accel.temperature;
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_accel_sum_count++;
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_accel_integrator.put(accel.timestamp_sample, accel_raw);
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const float dt = (accel.timestamp_sample - _last_timestamp_sample_accel) * 1e-6f;
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_last_timestamp_sample_accel = accel.timestamp_sample;
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_accel_integrator.put(accel_raw, dt);
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if (accel.clip_counter[0] > 0 || accel.clip_counter[1] > 0 || accel.clip_counter[2] > 0) {
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// rotate sensor clip counts into vehicle body frame
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@ -1,6 +1,6 @@
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/****************************************************************************
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*
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* Copyright (c) 2020 PX4 Development Team. All rights reserved.
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* Copyright (c) 2020-2021 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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@ -100,8 +100,8 @@ private:
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calibration::Accelerometer _accel_calibration{};
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calibration::Gyroscope _gyro_calibration{};
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Integrator _accel_integrator{}; // 200 Hz default
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Integrator _gyro_integrator{true}; // 200 Hz default, coning compensation enabled
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Integrator _accel_integrator{};
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IntegratorConing _gyro_integrator{};
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hrt_abstime _last_timestamp_sample_accel{0};
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hrt_abstime _last_timestamp_sample_gyro{0};
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