forked from Archive/PX4-Autopilot
WIP: Debugging of the Eigen quaternion tests. A bunch of the issues were incomplete porting, but the assertion is real.
This commit is contained in:
Lorenz Meier
parent
4466b5680a
commit
90ecc942ce
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@ -3,8 +3,8 @@
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#
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MODULE_COMMAND = tests
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MODULE_STACKSIZE = 12000
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MAXOPTIMIZATION = -Os
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MODULE_STACKSIZE = 60000
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MAXOPTIMIZATION = -O0
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SRCS = test_adc.c \
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test_bson.c \
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@ -37,7 +37,7 @@ SRCS = test_adc.c \
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ifeq ($(PX4_TARGET_OS), nuttx)
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SRCS += test_time.c
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EXTRACXXFLAGS = -Wframe-larger-than=2500
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EXTRACXXFLAGS = -Wframe-larger-than=6000
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else
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EXTRACXXFLAGS =
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endif
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@ -40,6 +40,7 @@
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#include <cmath>
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#include <px4_eigen.h>
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#include <mathlib/mathlib.h>
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#include <float.h>
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#include <stdio.h>
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#include <stdlib.h>
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@ -56,7 +57,7 @@ namespace Eigen
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typedef Matrix<float, 10, 1> Vector10f;
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}
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static constexpr size_t OPERATOR_ITERATIONS = 60000;
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static constexpr size_t OPERATOR_ITERATIONS = 30000;
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#define TEST_OP(_title, _op) \
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{ \
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@ -64,7 +65,7 @@ static constexpr size_t OPERATOR_ITERATIONS = 60000;
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for (size_t j = 0; j < OPERATOR_ITERATIONS; j++) { \
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_op; \
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} \
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printf(_title ": %.6fus\n", static_cast<double>(hrt_absolute_time() - t0) / OPERATOR_ITERATIONS); \
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printf("-O0 " _title ": %.6fus\n", static_cast<double>(hrt_absolute_time() - t0) / OPERATOR_ITERATIONS); \
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}
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#define VERIFY_OP(_title, _op, __OP_TEST__) \
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@ -105,13 +106,37 @@ void printEigen(const Eigen::MatrixBase<T> &b)
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* @brief
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* Construct new Eigen::Quaternion from euler angles
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**/
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template<typename T>
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Eigen::Quaternion<T> quatFromEuler(const T roll, const T pitch, const T yaw)
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// template<typename T>
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// Eigen::Quaternion<T> quatFromEuler(const T roll, const T pitch, const T yaw)
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// {
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// Eigen::AngleAxis<T> rollAngle(roll, Eigen::Matrix<T, 3, 1>::UnitZ());
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// Eigen::AngleAxis<T> yawAngle(yaw, Eigen::Matrix<T, 3, 1>::UnitY());
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// Eigen::AngleAxis<T> pitchAngle(pitch, Eigen::Matrix<T, 3, 1>::UnitX());
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// return yawAngle * pitchAngle * rollAngle;
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// }
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Eigen::Quaternionf quatFromEuler(const float roll, const float pitch, const float yaw);
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Eigen::Quaternionf quatFromEuler(const float roll, const float pitch, const float yaw)
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{
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Eigen::AngleAxis<T> rollAngle(roll, Eigen::Matrix<T, 3, 1>::UnitZ());
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Eigen::AngleAxis<T> yawAngle(yaw, Eigen::Matrix<T, 3, 1>::UnitY());
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Eigen::AngleAxis<T> pitchAngle(pitch, Eigen::Matrix<T, 3, 1>::UnitX());
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return rollAngle * yawAngle * pitchAngle;
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Eigen::AngleAxisf rollAngle(roll, Eigen::Vector3f::UnitZ());
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Eigen::AngleAxisf yawAngle(yaw, Eigen::Vector3f::UnitY());
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Eigen::AngleAxisf pitchAngle(pitch, Eigen::Vector3f::UnitX());
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return yawAngle * pitchAngle * rollAngle;
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}
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/**
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* @brief
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* Construct new Eigen::Matrix3f from euler angles
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**/
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template<typename T>
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Eigen::Matrix3f matrixFromEuler(const T roll, const T pitch, const T yaw)
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{
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Eigen::AngleAxis<T> rollAngle(roll, Eigen::Vector3f::UnitZ());
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Eigen::AngleAxis<T> yawAngle(yaw, Eigen::Vector3f::UnitY());
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Eigen::AngleAxis<T> pitchAngle(pitch, Eigen::Vector3f::UnitX());
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Eigen::Quaternionf q = yawAngle * pitchAngle * rollAngle;
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return q.toRotationMatrix();
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}
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@ -277,28 +302,102 @@ int test_eigen(int argc, char *argv[])
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}
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/* QUATERNION TESTS CURRENTLY FAILING
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warnx("pre-quat");
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usleep(500000);
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/* QUATERNION TESTS */
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{
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// test conversion rotation matrix to quaternion and back
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Eigen::Matrix3f R_orig;
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// against existing PX4 mathlib
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math::Matrix<3, 3> R_orig;
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Eigen::Matrix3f R;
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Eigen::Quaternionf q;
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float diff = 0.1f;
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float tol = 0.00001f;
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float tol;
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warnx("Quaternion transformation methods test.");
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warnx("testing known values..");
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// test against some known values
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tol = 0.001f;
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Eigen::Quaternionf q_true = {1.0f, 0.0f, 0.0f, 0.0f};
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if (!q.isApprox(q_true, tol)) {
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warnx("Quaternion 1.0f, 0.0f, 0.0f, 0.0f error: w: %8.4f", q.w());
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rc = 1;
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}
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usleep(510000);
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warnx("post-first");
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q_true = quatFromEuler(0.3f, 0.2f, 0.1f);
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q = {0.9833f, 0.1436f, 0.1060f, 0.0343f};
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usleep(510000);
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warnx("post-2");
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if (!q.isApprox(q_true, tol)) {
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warnx("Quaternion 0.9833f, 0.1436f, 0.1060f, 0.0343f error: w: %8.6f, %8.6f", q.w(), q_true.w());
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rc = 1;
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}
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usleep(510000);
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warnx("post-3");
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Eigen::Quaternionf q_true2 = quatFromEuler(-1.5f, -0.2f, 0.5f);
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Eigen::Quaternionf q2 = {0.7222f, -0.6391f, -0.2386f, 0.1142f};
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usleep(510000);
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warnx("post-4");
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if (!q2.isApprox(q_true2, tol)) {
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warnx("Quaternion 0.9833f, 0.1436f, 0.1060f, 0.0343f error: w: %8.6f, %8.6f", q2.w(), q_true2.w());
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rc = 1;
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}
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q = {0.6830f, 0.1830f, -0.6830f, 0.1830f};
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usleep(510000);
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warnx("post-5");
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q_true = quatFromEuler(M_PI_2_F, -M_PI_2_F, -M_PI_F / 3);
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usleep(510000);
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warnx("post-6");
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for (size_t i = 0; i < 4; i++) {
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if (!q.isApprox(q_true, tol)) {
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warnx("Quaternion method 'eulerAngles()' outside tolerance!");
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warnx("%8.4f, %8.4f, %8.4f, %8.4f, w: %8.4f",
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q.vec()(1), q.vec()(2), q.vec()(3), q.vec()(4), q.w());
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rc = 1;
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}
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}
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usleep(510000);
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warnx("post-7");
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warnx("testing transformation range (this will take a while)");
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tol = 0.00001f;
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for (float roll = -M_PI_F; roll <= M_PI_F; roll += diff) {
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for (float pitch = -M_PI_2_F; pitch <= M_PI_2_F; pitch += diff) {
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for (float yaw = -M_PI_F; yaw <= M_PI_F; yaw += diff) {
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R_orig.eulerAngles(roll, pitch, yaw);
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q = R_orig; //from_dcm
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Eigen::AngleAxisf rollAngle(roll, Eigen::Vector3f::UnitX());
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Eigen::AngleAxisf pitchAngle(pitch, Eigen::Vector3f::UnitY());
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Eigen::AngleAxisf yawAngle(yaw, Eigen::Vector3f::UnitZ());
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R_orig.from_euler(roll, pitch, yaw);
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q = yawAngle * pitchAngle * rollAngle;
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R = q.toRotationMatrix();
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for (size_t i = 0; i < 3; i++) {
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for (size_t j = 0; j < 3; j++) {
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if (fabsf(R_orig(i, j) - R(i, j)) > tol) {
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warnx("Quaternion method 'from_dcm' or 'toRotationMatrix' outside tolerance!");
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warnx("Quaternion constructor or 'toRotationMatrix' outside tolerance!\n %d, %d: %8.4f vs. %8.4f", i, j, R_orig(i, j), R(i, j));
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rc = 1;
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}
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}
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@ -306,50 +405,6 @@ int test_eigen(int argc, char *argv[])
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}
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}
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}
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// test against some known values
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tol = 0.0001f;
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Eigen::Quaternionf q_true = {1.0f, 0.0f, 0.0f, 0.0f};
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R_orig.setIdentity();
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q = R_orig;
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for (size_t i = 0; i < 4; i++) {
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if (!q.isApprox(q_true, tol)) {
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warnx("Quaternion method 'from_dcm()' outside tolerance!");
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rc = 1;
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}
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}
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q_true = quatFromEuler(0.3f, 0.2f, 0.1f);
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q = {0.9833f, 0.1436f, 0.1060f, 0.0343f};
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for (size_t i = 0; i < 4; i++) {
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if (!q.isApprox(q_true, tol)) {
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warnx("Quaternion method 'eulerAngles()' outside tolerance!");
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rc = 1;
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}
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}
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q_true = quatFromEuler(-1.5f, -0.2f, 0.5f);
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q = {0.7222f, -0.6391f, -0.2386f, 0.1142f};
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for (size_t i = 0; i < 4; i++) {
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if (!q.isApprox(q_true, tol)) {
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warnx("Quaternion method 'eulerAngles()' outside tolerance!");
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rc = 1;
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}
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}
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q_true = quatFromEuler(M_PI_2_F, -M_PI_2_F, -M_PI_F / 3);
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q = {0.6830f, 0.1830f, -0.6830f, 0.1830f};
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for (size_t i = 0; i < 4; i++) {
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if (!q.isApprox(q_true, tol)) {
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warnx("Quaternion method 'eulerAngles()' outside tolerance!");
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rc = 1;
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}
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}
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}
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{
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@ -360,29 +415,11 @@ int test_eigen(int argc, char *argv[])
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Eigen::Quaternionf q;
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Eigen::Matrix3f R;
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float diff = 0.1f;
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float tol = 0.00001f;
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float tol;
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warnx("Quaternion vector rotation method test.");
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for (float roll = -M_PI_F; roll <= M_PI_F; roll += diff) {
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for (float pitch = -M_PI_2_F; pitch <= M_PI_2_F; pitch += diff) {
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for (float yaw = -M_PI_F; yaw <= M_PI_F; yaw += diff) {
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R.eulerAngles(roll, pitch, yaw);
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q = quatFromEuler(roll, pitch, yaw);
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vector_r = R * vector;
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vector_q = q._transformVector(vector);
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for (int i = 0; i < 3; i++) {
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if (fabsf(vector_r(i) - vector_q(i)) > tol) {
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warnx("Quaternion method 'rotate' outside tolerance");
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rc = 1;
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}
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}
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}
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}
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}
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// test some values calculated with matlab
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// test some values calculated with matlab
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tol = 0.0001f;
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q = quatFromEuler(M_PI_2_F, 0.0f, 0.0f);
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vector_q = q._transformVector(vector);
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@ -391,6 +428,9 @@ int test_eigen(int argc, char *argv[])
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for (size_t i = 0; i < 3; i++) {
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if (fabsf(vector_true(i) - vector_q(i)) > tol) {
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warnx("Quaternion method 'rotate' outside tolerance");
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warnx("%8.4f, %8.4f, %8.4f, true: %8.4f, %8.4f, %8.4f",
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(double)vector_q(1), (double)vector_q(2), (double)vector_q(3),
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(double)vector_true(1), (double)vector_true(2), (double)vector_true(3));
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rc = 1;
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}
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}
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@ -402,6 +442,9 @@ int test_eigen(int argc, char *argv[])
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for (size_t i = 0; i < 3; i++) {
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if (fabsf(vector_true(i) - vector_q(i)) > tol) {
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warnx("Quaternion method 'rotate' outside tolerance");
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warnx("%8.4f, %8.4f, %8.4f, true: %8.4f, %8.4f, %8.4f",
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(double)vector_q(1), (double)vector_q(2), (double)vector_q(3),
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(double)vector_true(1), (double)vector_true(2), (double)vector_true(3));
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rc = 1;
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}
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}
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@ -413,6 +456,9 @@ int test_eigen(int argc, char *argv[])
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for (size_t i = 0; i < 3; i++) {
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if (fabsf(vector_true(i) - vector_q(i)) > tol) {
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warnx("Quaternion method 'rotate' outside tolerance");
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warnx("%8.4f, %8.4f, %8.4f, true: %8.4f, %8.4f, %8.4f",
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(double)vector_q(1), (double)vector_q(2), (double)vector_q(3),
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(double)vector_true(1), (double)vector_true(2), (double)vector_true(3));
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rc = 1;
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}
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}
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@ -424,10 +470,36 @@ int test_eigen(int argc, char *argv[])
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for (size_t i = 0; i < 3; i++) {
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if (fabsf(vector_true(i) - vector_q(i)) > tol) {
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warnx("Quaternion method 'rotate' outside tolerance");
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warnx("%8.4f, %8.4f, %8.4f, true: %8.4f, %8.4f, %8.4f",
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(double)vector_q(1), (double)vector_q(2), (double)vector_q(3),
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(double)vector_true(1), (double)vector_true(2), (double)vector_true(3));
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rc = 1;
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}
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}
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warnx("testing transformation range (this will take a while)");
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tol = 0.00001f;
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Eigen::Vector3f vectorR = {1.0f, 1.0f, 1.0f};
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for (float roll = -M_PI_F; roll <= M_PI_F; roll += diff) {
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for (float pitch = -M_PI_2_F; pitch <= M_PI_2_F; pitch += diff) {
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for (float yaw = -M_PI_F; yaw <= M_PI_F; yaw += diff) {
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R = matrixFromEuler(roll, pitch, yaw);
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q = quatFromEuler(roll, pitch, yaw);
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vector_r = R * vectorR;
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vector_q = q._transformVector(vectorR);
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for (int i = 0; i < 3; i++) {
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if (fabsf(vector_r(i) - vector_q(i)) > tol) {
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warnx("Quaternion method 'rotate' outside tolerance");
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rc = 1;
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}
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}
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}
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}
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}
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}
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*/
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return rc;
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}
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@ -49,7 +49,7 @@
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#include "tests.h"
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#define TEST_OP(_title, _op) { unsigned int n = 60000; hrt_abstime t0, t1; t0 = hrt_absolute_time(); for (unsigned int j = 0; j < n; j++) { _op; }; t1 = hrt_absolute_time(); PX4_INFO(_title ": %.6fus", (double)(t1 - t0) / n); }
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#define TEST_OP(_title, _op) { unsigned int n = 30000; hrt_abstime t0, t1; t0 = hrt_absolute_time(); for (unsigned int j = 0; j < n; j++) { _op; }; t1 = hrt_absolute_time(); PX4_INFO(_title ": %.6fus", (double)(t1 - t0) / n); }
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using namespace math;
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