mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-05-01 20:24:08 +08:00
This is a non-functional change required to select accel bias estimation per axis selection. The intent is then to disable the learning before takeoff of the components that are poorly observable.
184 lines
6.5 KiB
C++
184 lines
6.5 KiB
C++
/****************************************************************************
|
|
*
|
|
* Copyright (c) 2019 ECL 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 <math.h>
|
|
#include <memory>
|
|
#include "EKF/ekf.h"
|
|
#include "sensor_simulator/sensor_simulator.h"
|
|
#include "sensor_simulator/ekf_wrapper.h"
|
|
|
|
class EkfInitializationTest : public ::testing::Test {
|
|
public:
|
|
EkfInitializationTest(): ::testing::Test(),
|
|
_ekf{std::make_shared<Ekf>()},
|
|
_sensor_simulator(_ekf),
|
|
_ekf_wrapper(_ekf) {};
|
|
|
|
std::shared_ptr<Ekf> _ekf;
|
|
SensorSimulator _sensor_simulator;
|
|
EkfWrapper _ekf_wrapper;
|
|
|
|
const float _init_tilt_period = 1.0; // seconds
|
|
|
|
// GTests is calling this
|
|
void SetUp() override
|
|
{
|
|
_ekf->init(0);
|
|
}
|
|
|
|
// Use this method to clean up any memory, network etc. after each test
|
|
void TearDown() override
|
|
{
|
|
}
|
|
|
|
void initializedOrienationIsMatchingGroundTruth(Quatf true_quaternion)
|
|
{
|
|
const Quatf quat_est = _ekf->getQuaternion();
|
|
EXPECT_TRUE(matrix::isEqual(quat_est, true_quaternion));
|
|
}
|
|
|
|
void validStateAfterOrientationInitialization()
|
|
{
|
|
quaternionVarianceBigEnoughAfterOrientationInitialization();
|
|
velocityAndPositionCloseToZero();
|
|
velocityAndPositionVarianceBigEnoughAfterOrientationInitialization();
|
|
}
|
|
|
|
void quaternionVarianceBigEnoughAfterOrientationInitialization()
|
|
{
|
|
const matrix::Vector<float, 4> quat_variance = _ekf_wrapper.getQuaternionVariance();
|
|
const float quat_variance_limit = 0.0001f;
|
|
EXPECT_TRUE(quat_variance(1) > quat_variance_limit) << "quat_variance(1)" << quat_variance(1);
|
|
EXPECT_TRUE(quat_variance(2) > quat_variance_limit) << "quat_variance(2)" << quat_variance(2);
|
|
EXPECT_TRUE(quat_variance(3) > quat_variance_limit) << "quat_variance(3)" << quat_variance(3);
|
|
}
|
|
|
|
void velocityAndPositionCloseToZero()
|
|
{
|
|
const Vector3f pos = _ekf->getPosition();
|
|
const Vector3f vel = _ekf->getVelocity();
|
|
|
|
EXPECT_TRUE(matrix::isEqual(pos, Vector3f{}, 0.001f));
|
|
EXPECT_TRUE(matrix::isEqual(vel, Vector3f{}, 0.001f));
|
|
}
|
|
|
|
void velocityAndPositionVarianceBigEnoughAfterOrientationInitialization()
|
|
{
|
|
const Vector3f pos_var = _ekf->getPositionVariance();
|
|
const Vector3f vel_var = _ekf->getVelocityVariance();
|
|
|
|
const float pos_variance_limit = 0.2f;
|
|
EXPECT_TRUE(pos_var(0) > pos_variance_limit) << "pos_var(0)" << pos_var(0);
|
|
EXPECT_TRUE(pos_var(1) > pos_variance_limit) << "pos_var(1)" << pos_var(1);
|
|
EXPECT_TRUE(pos_var(2) > pos_variance_limit) << "pos_var(2)" << pos_var(2);
|
|
|
|
const float vel_variance_limit = 0.4f;
|
|
EXPECT_TRUE(vel_var(0) > vel_variance_limit) << "vel_var(0)" << vel_var(0);
|
|
EXPECT_TRUE(vel_var(1) > vel_variance_limit) << "vel_var(1)" << vel_var(1);
|
|
EXPECT_TRUE(vel_var(2) > vel_variance_limit) << "vel_var(2)" << vel_var(2);
|
|
}
|
|
};
|
|
|
|
TEST_F(EkfInitializationTest, initializeWithZeroTilt)
|
|
{
|
|
const float pitch = math::radians(0.0f);
|
|
const float roll = math::radians(0.0f);
|
|
const Eulerf euler_angles_sim(roll, pitch, 0.0f);
|
|
const Quatf quat_sim(euler_angles_sim);
|
|
|
|
_sensor_simulator.simulateOrientation(quat_sim);
|
|
_sensor_simulator.runSeconds(_init_tilt_period);
|
|
|
|
initializedOrienationIsMatchingGroundTruth(quat_sim);
|
|
validStateAfterOrientationInitialization();
|
|
}
|
|
|
|
TEST_F(EkfInitializationTest, initializeHeadingWithZeroTilt)
|
|
{
|
|
const float pitch = math::radians(0.0f);
|
|
const float roll = math::radians(0.0f);
|
|
const float yaw = math::radians(90.0f);
|
|
const Eulerf euler_angles_sim(roll, pitch, yaw);
|
|
const Quatf quat_sim(euler_angles_sim);
|
|
|
|
_sensor_simulator.simulateOrientation(quat_sim);
|
|
_sensor_simulator.runSeconds(_init_tilt_period);
|
|
|
|
initializedOrienationIsMatchingGroundTruth(quat_sim);
|
|
validStateAfterOrientationInitialization();
|
|
}
|
|
|
|
TEST_F(EkfInitializationTest, initializeWithTilt)
|
|
{
|
|
const float pitch = math::radians(30.0f);
|
|
const float roll = math::radians(60.0f);
|
|
const Eulerf euler_angles_sim(roll, pitch, 0.0f);
|
|
const Quatf quat_sim(euler_angles_sim);
|
|
|
|
_sensor_simulator.simulateOrientation(quat_sim);
|
|
_sensor_simulator.runSeconds(_init_tilt_period);
|
|
|
|
initializedOrienationIsMatchingGroundTruth(quat_sim);
|
|
validStateAfterOrientationInitialization();
|
|
}
|
|
|
|
TEST_F(EkfInitializationTest, initializeWithPitch90)
|
|
{
|
|
const float pitch = math::radians(90.0f);
|
|
const float roll = math::radians(0.0f);
|
|
const Eulerf euler_angles_sim(roll, pitch, 0.0f);
|
|
const Quatf quat_sim(euler_angles_sim);
|
|
|
|
_sensor_simulator.simulateOrientation(quat_sim);
|
|
_sensor_simulator.runSeconds(_init_tilt_period);
|
|
|
|
initializedOrienationIsMatchingGroundTruth(quat_sim);
|
|
// TODO: Quaternion Variance is smaller in this case than in the other cases
|
|
validStateAfterOrientationInitialization();
|
|
}
|
|
|
|
TEST_F(EkfInitializationTest, initializeWithRoll90)
|
|
{
|
|
const float pitch = math::radians(0.0f);
|
|
const float roll = math::radians(90.0f);
|
|
const Eulerf euler_angles_sim(roll, pitch, 0.0f);
|
|
const Quatf quat_sim(euler_angles_sim);
|
|
|
|
_sensor_simulator.simulateOrientation(quat_sim);
|
|
_sensor_simulator.runSeconds(_init_tilt_period);
|
|
|
|
initializedOrienationIsMatchingGroundTruth(quat_sim);
|
|
validStateAfterOrientationInitialization();
|
|
}
|