gtsam/gtsam_unstable/timing/timeInertialNavFactor_Globa...

111 lines
4.3 KiB
C++

/* ----------------------------------------------------------------------------
* GTSAM Copyright 2010, Georgia Tech Research Corporation,
* Atlanta, Georgia 30332-0415
* All Rights Reserved
* Authors: Frank Dellaert, et al. (see THANKS for the full author list)
* See LICENSE for the license information
* -------------------------------------------------------------------------- */
/**
* @file testInertialNavFactor_GlobalVelocity.cpp
* @brief Unit test for the InertialNavFactor_GlobalVelocity
* @author Vadim Indelman, Stephen Williams
*/
#include <iostream>
#include <gtsam/navigation/ImuBias.h>
#include <gtsam_unstable/slam/InertialNavFactor_GlobalVelocity.h>
#include <gtsam/geometry/Pose3.h>
#include <gtsam/nonlinear/Values.h>
#include <gtsam/base/numericalDerivative.h>
#include <gtsam/base/LieVector.h>
#include <gtsam/inference/Key.h>
using namespace std;
using namespace gtsam;
gtsam::Rot3 world_R_ECEF(
0.31686, 0.51505, 0.79645,
0.85173, -0.52399, 0,
0.41733, 0.67835, -0.60471);
gtsam::Vector ECEF_omega_earth((Vector(3) << 0.0, 0.0, 7.292115e-5));
gtsam::Vector world_omega_earth(world_R_ECEF.matrix() * ECEF_omega_earth);
/* ************************************************************************* */
gtsam::Pose3 predictionErrorPose(const Pose3& p1, const LieVector& v1, const imuBias::ConstantBias& b1, const Pose3& p2, const LieVector& v2, const InertialNavFactor_GlobalVelocity<Pose3, LieVector, imuBias::ConstantBias>& factor) {
return Pose3::Expmap(factor.evaluateError(p1, v1, b1, p2, v2).head(6));
}
gtsam::LieVector predictionErrorVel(const Pose3& p1, const LieVector& v1, const imuBias::ConstantBias& b1, const Pose3& p2, const LieVector& v2, const InertialNavFactor_GlobalVelocity<Pose3, LieVector, imuBias::ConstantBias>& factor) {
return LieVector::Expmap(factor.evaluateError(p1, v1, b1, p2, v2).tail(3));
}
#include <gtsam/linear/GaussianFactorGraph.h>
/* ************************************************************************* */
int main() {
gtsam::Key PoseKey1(11);
gtsam::Key PoseKey2(12);
gtsam::Key VelKey1(21);
gtsam::Key VelKey2(22);
gtsam::Key BiasKey1(31);
double measurement_dt(0.1);
Vector world_g((Vector(3) << 0.0, 0.0, 9.81));
Vector world_rho((Vector(3) << 0.0, -1.5724e-05, 0.0)); // NED system
gtsam::Vector ECEF_omega_earth((Vector(3) << 0.0, 0.0, 7.292115e-5));
gtsam::Vector world_omega_earth(world_R_ECEF.matrix() * ECEF_omega_earth);
SharedGaussian model(noiseModel::Isotropic::Sigma(9, 0.1));
// Second test: zero angular motion, some acceleration - generated in matlab
Vector measurement_acc((Vector(3) << 6.501390843381716, -6.763926150509185, -2.300389940090343));
Vector measurement_gyro((Vector(3) << 0.1, 0.2, 0.3));
InertialNavFactor_GlobalVelocity<Pose3, LieVector, imuBias::ConstantBias> f(PoseKey1, VelKey1, BiasKey1, PoseKey2, VelKey2, measurement_acc, measurement_gyro, measurement_dt, world_g, world_rho, world_omega_earth, model);
Rot3 R1(0.487316618, 0.125253866, 0.86419557,
0.580273724, 0.693095498, -0.427669306,
-0.652537293, 0.709880342, 0.265075427);
Point3 t1(2.0,1.0,3.0);
Pose3 Pose1(R1, t1);
LieVector Vel1 = Vector((Vector(3) << 0.5,-0.5,0.4));
Rot3 R2(0.473618898, 0.119523052, 0.872582019,
0.609241153, 0.67099888, -0.422594037,
-0.636011287, 0.731761397, 0.244979388);
Point3 t2 = t1.compose( Point3(Vel1*measurement_dt) );
Pose3 Pose2(R2, t2);
Vector dv = measurement_dt * (R1.matrix() * measurement_acc + world_g);
LieVector Vel2 = Vel1.compose( dv );
imuBias::ConstantBias Bias1;
Values values;
values.insert(PoseKey1, Pose1);
values.insert(PoseKey2, Pose2);
values.insert(VelKey1, Vel1);
values.insert(VelKey2, Vel2);
values.insert(BiasKey1, Bias1);
Ordering ordering;
ordering.push_back(PoseKey1);
ordering.push_back(VelKey1);
ordering.push_back(BiasKey1);
ordering.push_back(PoseKey2);
ordering.push_back(VelKey2);
GaussianFactorGraph graph;
gttic_(LinearizeTiming);
for(size_t i = 0; i < 100000; ++i) {
GaussianFactor::shared_ptr g = f.linearize(values);
graph.push_back(g);
}
gttoc_(LinearizeTiming);
tictoc_finishedIteration_();
tictoc_print_();
}
/* ************************************************************************* */