create new multicopter rate controller module (mc_rate_control) split out of mc_att_control

This commit is contained in:
Daniel Agar
2019-11-19 17:03:11 -05:00
committed by GitHub
parent b64abf48b2
commit 84fe64b1c2
80 changed files with 1231 additions and 775 deletions
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############################################################################
#
# Copyright (c) 2019 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_library(RateControl
RateControl.cpp
)
target_include_directories(RateControl
PUBLIC
${CMAKE_CURRENT_SOURCE_DIR}
)
target_link_libraries(RateControl PRIVATE mathlib)
px4_add_unit_gtest(SRC RateControlTest.cpp LINKLIBS RateControl)
@@ -0,0 +1,133 @@
/****************************************************************************
*
* Copyright (c) 2019 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 RateControl.cpp
*/
#include <RateControl.hpp>
#include <px4_platform_common/defines.h>
using namespace matrix;
void RateControl::setGains(const Vector3f &P, const Vector3f &I, const Vector3f &D)
{
_gain_p = P;
_gain_i = I;
_gain_d = D;
}
void RateControl::setDTermCutoff(const float loop_rate, const float cutoff, const bool force)
{
// only do expensive filter update if the cutoff changed
if (force || fabsf(_lp_filters_d.get_cutoff_freq() - cutoff) > 0.01f) {
_lp_filters_d.set_cutoff_frequency(loop_rate, cutoff);
_lp_filters_d.reset(_rate_prev);
}
}
void RateControl::setSaturationStatus(const MultirotorMixer::saturation_status &status)
{
_mixer_saturation_positive[0] = status.flags.roll_pos;
_mixer_saturation_positive[1] = status.flags.pitch_pos;
_mixer_saturation_positive[2] = status.flags.yaw_pos;
_mixer_saturation_negative[0] = status.flags.roll_neg;
_mixer_saturation_negative[1] = status.flags.pitch_neg;
_mixer_saturation_negative[2] = status.flags.yaw_neg;
}
Vector3f RateControl::update(const Vector3f &rate, const Vector3f &rate_sp, const float dt, const bool landed)
{
// angular rates error
Vector3f rate_error = rate_sp - rate;
// prepare D-term based on low-pass filtered rates
const Vector3f rate_filtered(_lp_filters_d.apply(rate));
Vector3f rate_d;
if (dt > FLT_EPSILON) {
rate_d = (rate_filtered - _rate_prev_filtered) / dt;
}
// PID control with feed forward
const Vector3f torque = _gain_p.emult(rate_error) + _rate_int - _gain_d.emult(rate_d) + _gain_ff.emult(rate_sp);
_rate_prev = rate;
_rate_prev_filtered = rate_filtered;
// update integral only if we are not landed
if (!landed) {
updateIntegral(rate_error, dt);
}
return torque;
}
void RateControl::updateIntegral(Vector3f &rate_error, const float dt)
{
for (int i = 0; i < 3; i++) {
// prevent further positive control saturation
if (_mixer_saturation_positive[i]) {
rate_error(i) = math::min(rate_error(i), 0.f);
}
// prevent further negative control saturation
if (_mixer_saturation_negative[i]) {
rate_error(i) = math::max(rate_error(i), 0.f);
}
// I term factor: reduce the I gain with increasing rate error.
// This counteracts a non-linear effect where the integral builds up quickly upon a large setpoint
// change (noticeable in a bounce-back effect after a flip).
// The formula leads to a gradual decrease w/o steps, while only affecting the cases where it should:
// with the parameter set to 400 degrees, up to 100 deg rate error, i_factor is almost 1 (having no effect),
// and up to 200 deg error leads to <25% reduction of I.
float i_factor = rate_error(i) / math::radians(400.f);
i_factor = math::max(0.0f, 1.f - i_factor * i_factor);
// Perform the integration using a first order method
float rate_i = _rate_int(i) + i_factor * _gain_i(i) * rate_error(i) * dt;
// do not propagate the result if out of range or invalid
if (PX4_ISFINITE(rate_i)) {
_rate_int(i) = math::constrain(rate_i, -_lim_int(i), _lim_int(i));
}
}
}
void RateControl::getRateControlStatus(rate_ctrl_status_s &rate_ctrl_status)
{
rate_ctrl_status.rollspeed_integ = _rate_int(0);
rate_ctrl_status.pitchspeed_integ = _rate_int(1);
rate_ctrl_status.yawspeed_integ = _rate_int(2);
}
@@ -0,0 +1,128 @@
/****************************************************************************
*
* Copyright (c) 2019 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 RateControl.hpp
*
* PID 3 axis angular rate / angular velocity control.
*/
#pragma once
#include <matrix/matrix/math.hpp>
#include <mathlib/math/filter/LowPassFilter2pVector3f.hpp>
#include <lib/mixer/mixer.h>
#include <uORB/topics/rate_ctrl_status.h>
class RateControl
{
public:
RateControl() = default;
~RateControl() = default;
/**
* Set the rate control gains
* @param P 3D vector of proportional gains for body x,y,z axis
* @param I 3D vector of integral gains
* @param D 3D vector of derivative gains
*/
void setGains(const matrix::Vector3f &P, const matrix::Vector3f &I, const matrix::Vector3f &D);
/**
* Set the mximum absolute value of the integrator for all axes
* @param integrator_limit limit value for all axes x, y, z
*/
void setIntegratorLimit(const matrix::Vector3f &integrator_limit) { _lim_int = integrator_limit; };
/**
* Set update frequency and low-pass filter cutoff that is applied to the derivative term
* @param loop_rate [Hz] rate with which update function is called
* @param cutoff [Hz] cutoff frequency for the low-pass filter on the dervative term
* @param force flag to force an expensive update even if the cutoff didn't change
*/
void setDTermCutoff(const float loop_rate, const float cutoff, const bool force);
/**
* Set direct rate to torque feed forward gain
* @see _gain_ff
* @param FF 3D vector of feed forward gains for body x,y,z axis
*/
void setFeedForwardGain(const matrix::Vector3f &FF) { _gain_ff = FF; };
/**
* Set saturation status
* @param status message from mixer reporting about saturation
*/
void setSaturationStatus(const MultirotorMixer::saturation_status &status);
/**
* Run one control loop cycle calculation
* @param rate estimation of the current vehicle angular rate
* @param rate_sp desired vehicle angular rate setpoint
* @param dt desired vehicle angular rate setpoint
* @return [-1,1] normalized torque vector to apply to the vehicle
*/
matrix::Vector3f update(const matrix::Vector3f &rate, const matrix::Vector3f &rate_sp, const float dt,
const bool landed);
/**
* Set the integral term to 0 to prevent windup
* @see _rate_int
*/
void resetIntegral() { _rate_int.zero(); }
/**
* Get status message of controller for logging/debugging
* @param rate_ctrl_status status message to fill with internal states
*/
void getRateControlStatus(rate_ctrl_status_s &rate_ctrl_status);
private:
void updateIntegral(matrix::Vector3f &rate_error, const float dt);
// Gains
matrix::Vector3f _gain_p; ///< rate control proportional gain for all axes x, y, z
matrix::Vector3f _gain_i; ///< rate control integral gain
matrix::Vector3f _gain_d; ///< rate control derivative gain
matrix::Vector3f _lim_int; ///< integrator term maximum absolute value
matrix::Vector3f _gain_ff; ///< direct rate to torque feed forward gain only useful for helicopters
// States
matrix::Vector3f _rate_prev; ///< angular rates of previous update
matrix::Vector3f _rate_prev_filtered; ///< low-pass filtered angular rates of previous update
matrix::Vector3f _rate_int; ///< integral term of the rate controller
math::LowPassFilter2pVector3f _lp_filters_d{0.f, 0.f}; ///< low-pass filters for D-term (roll, pitch & yaw)
bool _mixer_saturation_positive[3] {};
bool _mixer_saturation_negative[3] {};
};
@@ -0,0 +1,44 @@
/****************************************************************************
*
* Copyright (C) 2019 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.
*
****************************************************************************/
#include <gtest/gtest.h>
#include <RateControl.hpp>
using namespace matrix;
TEST(RateControlTest, AllZeroCase)
{
RateControl rate_control;
Vector3f torque = rate_control.update(Vector3f(), Vector3f(), 0.f, false);
EXPECT_EQ(torque, Vector3f());
}