PreintegrationBase.cpp
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1 /* ----------------------------------------------------------------------------
2 
3  * GTSAM Copyright 2010, Georgia Tech Research Corporation,
4  * Atlanta, Georgia 30332-0415
5  * All Rights Reserved
6  * Authors: Frank Dellaert, et al. (see THANKS for the full author list)
7 
8  * See LICENSE for the license information
9 
10  * -------------------------------------------------------------------------- */
11 
23 #include "PreintegrationBase.h"
25 
26 using namespace std;
27 
28 namespace gtsam {
29 
30 //------------------------------------------------------------------------------
31 PreintegrationBase::PreintegrationBase(const std::shared_ptr<Params>& p,
32  const Bias& biasHat)
33  : p_(p), biasHat_(biasHat), deltaTij_(0.0) {
34 }
35 
36 //------------------------------------------------------------------------------
37 ostream& operator<<(ostream& os, const PreintegrationBase& pim) {
38  os << " deltaTij = " << pim.deltaTij_ << endl;
39  os << " deltaRij.ypr = (" << pim.deltaRij().ypr().transpose() << ")" << endl;
40  os << " deltaPij = " << pim.deltaPij().transpose() << endl;
41  os << " deltaVij = " << pim.deltaVij().transpose() << endl;
42  os << " gyrobias = " << pim.biasHat_.gyroscope().transpose() << endl;
43  os << " acc_bias = " << pim.biasHat_.accelerometer().transpose() << endl;
44  return os;
45 }
46 
47 //------------------------------------------------------------------------------
48 void PreintegrationBase::print(const string& s) const {
49  cout << (s.empty() ? s : s + "\n") << *this << endl;
50 }
51 
52 //------------------------------------------------------------------------------
54  biasHat_ = biasHat;
56 }
57 
58 //------------------------------------------------------------------------------
60  const Vector3& unbiasedAcc, const Vector3& unbiasedOmega,
61  OptionalJacobian<3, 3> correctedAcc_H_unbiasedAcc,
62  OptionalJacobian<3, 3> correctedAcc_H_unbiasedOmega,
63  OptionalJacobian<3, 3> correctedOmega_H_unbiasedOmega) const {
64  assert(p().body_P_sensor);
65 
66  // Compensate for sensor-body displacement if needed: we express the quantities
67  // (originally in the IMU frame) into the body frame
68  // Equations below assume the "body" frame is the CG
69 
70  // Get sensor to body rotation matrix
71  const Matrix3 bRs = p().body_P_sensor->rotation().matrix();
72 
73  // Convert angular velocity and acceleration from sensor to body frame
74  Vector3 correctedAcc = bRs * unbiasedAcc;
75  const Vector3 correctedOmega = bRs * unbiasedOmega;
76 
77  // Jacobians
78  if (correctedAcc_H_unbiasedAcc) *correctedAcc_H_unbiasedAcc = bRs;
79  if (correctedAcc_H_unbiasedOmega) *correctedAcc_H_unbiasedOmega = Z_3x3;
80  if (correctedOmega_H_unbiasedOmega) *correctedOmega_H_unbiasedOmega = bRs;
81 
82  // Centrifugal acceleration
83  const Vector3 b_arm = p().body_P_sensor->translation();
84  if (!b_arm.isZero()) {
85  // Subtract out the the centripetal acceleration from the unbiased one
86  // to get linear acceleration vector in the body frame:
87  const Matrix3 body_Omega_body = skewSymmetric(correctedOmega);
88  const Vector3 b_velocity_bs = body_Omega_body * b_arm; // magnitude: omega * arm
89  correctedAcc -= body_Omega_body * b_velocity_bs;
90 
91  // Update derivative: centrifugal causes the correlation between acc and omega!!!
92  if (correctedAcc_H_unbiasedOmega) {
93  double wdp = correctedOmega.dot(b_arm);
94  const Matrix3 diag_wdp = Vector3::Constant(wdp).asDiagonal();
95  *correctedAcc_H_unbiasedOmega = -( diag_wdp
96  + correctedOmega * b_arm.transpose()) * bRs.matrix()
97  + 2 * b_arm * unbiasedOmega.transpose();
98  }
99  }
100 
101  return make_pair(correctedAcc, correctedOmega);
102 }
103 
104 //------------------------------------------------------------------------------
106  const Vector3& measuredOmega, double dt) {
107  // NOTE(frank): integrateMeasurement always needs to compute the derivatives,
108  // even when not of interest to the caller. Provide scratch space here.
109  Matrix9 A;
110  Matrix93 B, C;
111  update(measuredAcc, measuredOmega, dt, &A, &B, &C);
112 }
113 
114 //------------------------------------------------------------------------------
117  OptionalJacobian<9, 6> H2) const {
118  Matrix96 D_biasCorrected_bias;
119  Vector9 biasCorrected = biasCorrectedDelta(bias_i,
120  H2 ? &D_biasCorrected_bias : nullptr);
121 
122  // Correct for initial velocity and gravity
123  Matrix9 D_delta_state, D_delta_biasCorrected;
124  Vector9 xi = state_i.correctPIM(biasCorrected, deltaTij_, p().n_gravity,
125  p().omegaCoriolis, p().use2ndOrderCoriolis, H1 ? &D_delta_state : nullptr,
126  H2 ? &D_delta_biasCorrected : nullptr);
127 
128  // Use retract to get back to NavState manifold
129  Matrix9 D_predict_state, D_predict_delta;
130  NavState state_j = state_i.retract(xi,
131  H1 ? &D_predict_state : nullptr,
132  H2 || H2 ? &D_predict_delta : nullptr);
133  if (H1)
134  *H1 = D_predict_state + D_predict_delta * D_delta_state;
135  if (H2)
136  *H2 = D_predict_delta * D_delta_biasCorrected * D_biasCorrected_bias;
137  return state_j;
138 }
139 
140 //------------------------------------------------------------------------------
142  const NavState& state_j,
143  const imuBias::ConstantBias& bias_i,
146  OptionalJacobian<9, 6> H3) const {
147  // Predict state at time j
148  Matrix9 D_predict_state_i;
149  Matrix96 D_predict_bias_i;
150  NavState predictedState_j = predict(
151  state_i, bias_i, H1 ? &D_predict_state_i : 0, H3 ? &D_predict_bias_i : 0);
152 
153  // Calculate error
154  Matrix9 D_error_state_j, D_error_predict;
155  Vector9 error =
156  state_j.localCoordinates(predictedState_j, H2 ? &D_error_state_j : 0,
157  H1 || H3 ? &D_error_predict : 0);
158 
159  if (H1) *H1 << D_error_predict * D_predict_state_i;
160  if (H2) *H2 << D_error_state_j;
161  if (H3) *H3 << D_error_predict * D_predict_bias_i;
162 
163  return error;
164 }
165 
166 //------------------------------------------------------------------------------
168  const Vector3& vel_i, const Pose3& pose_j, const Vector3& vel_j,
172 
173  // Note that derivative of constructors below is not identity for velocity, but
174  // a 9*3 matrix == Z_3x3, Z_3x3, state.R().transpose()
175  NavState state_i(pose_i, vel_i);
176  NavState state_j(pose_j, vel_j);
177 
178  // Predict state at time j
179  Matrix9 D_error_state_i, D_error_state_j;
180  Vector9 error = computeError(state_i, state_j, bias_i,
181  H1 || H2 ? &D_error_state_i : 0, H3 || H4 ? &D_error_state_j : 0, H5);
182 
183  // Separate out derivatives in terms of 5 arguments
184  // Note that doing so requires special treatment of velocities, as when treated as
185  // separate variables the retract applied will not be the semi-direct product in NavState
186  // Instead, the velocities in nav are updated using a straight addition
187  // This is difference is accounted for by the R().transpose calls below
188  if (H1) *H1 << D_error_state_i.leftCols<6>();
189  if (H2) *H2 << D_error_state_i.rightCols<3>() * state_i.R().transpose();
190  if (H3) *H3 << D_error_state_j.leftCols<6>();
191  if (H4) *H4 << D_error_state_j.rightCols<3>() * state_j.R().transpose();
192 
193  return error;
194 }
195 
196 //------------------------------------------------------------------------------
197 
198 } // namespace gtsam
Matrix< SCALARB, Dynamic, Dynamic, opt_B > B
Definition: bench_gemm.cpp:49
Vector3 correctedAcc(const PreintegratedImuMeasurements &pim, const Vector3 &measuredAcc, const Vector3 &measuredOmega)
Eigen::Vector3d Vector3
Definition: Vector.h:43
virtual void update(const Vector3 &measuredAcc, const Vector3 &measuredOmega, const double dt, Matrix9 *A, Matrix93 *B, Matrix93 *C)=0
static Pose3 body_P_sensor(Rot3::RzRyRx(-M_PI_2, 0.0, -M_PI_2), Point3(0.25, -0.10, 1.0))
Definition: BFloat16.h:88
Some functions to compute numerical derivatives.
Vector9 correctPIM(const Vector9 &pim, double dt, const Vector3 &n_gravity, const std::optional< Vector3 > &omegaCoriolis, bool use2ndOrderCoriolis=false, OptionalJacobian< 9, 9 > H1={}, OptionalJacobian< 9, 9 > H2={}) const
Definition: NavState.cpp:257
Matrix< SCALARA, Dynamic, Dynamic, opt_A > A
Definition: bench_gemm.cpp:48
Vector9 computeError(const NavState &state_i, const NavState &state_j, const imuBias::ConstantBias &bias_i, OptionalJacobian< 9, 9 > H1, OptionalJacobian< 9, 9 > H2, OptionalJacobian< 9, 6 > H3) const
Calculate error given navStates.
Params & p() const
const reference to params
const double dt
virtual Rot3 deltaRij() const =0
virtual Vector3 deltaPij() const =0
const Vector3 & accelerometer() const
Definition: ImuBias.h:66
void resetIntegrationAndSetBias(const Bias &biasHat)
Vector9 computeErrorAndJacobians(const Pose3 &pose_i, const Vector3 &vel_i, const Pose3 &pose_j, const Vector3 &vel_j, const imuBias::ConstantBias &bias_i, OptionalJacobian< 9, 6 > H1={}, OptionalJacobian< 9, 3 > H2={}, OptionalJacobian< 9, 6 > H3={}, OptionalJacobian< 9, 3 > H4={}, OptionalJacobian< 9, 6 > H5={}) const
virtual void resetIntegration()=0
virtual void print(const std::string &s="") const
const imuBias::ConstantBias & biasHat() const
RealScalar s
static const Vector3 measuredAcc
double deltaTij_
Time interval from i to j.
Matrix< Scalar, Dynamic, Dynamic > C
Definition: bench_gemm.cpp:50
Vector xi
Definition: testPose2.cpp:148
virtual void integrateMeasurement(const Vector3 &measuredAcc, const Vector3 &measuredOmega, const double dt)
Version without derivatives.
traits
Definition: chartTesting.h:28
Matrix3 R() const
Return rotation matrix. Induces computation in quaternion mode.
Definition: NavState.h:95
NavState retract(const Vector9 &v, OptionalJacobian< 9, 9 > H1={}, OptionalJacobian< 9, 9 > H2={}) const
retract with optional derivatives
Definition: NavState.cpp:107
Matrix3 skewSymmetric(double wx, double wy, double wz)
Definition: base/Matrix.h:400
static const Vector3 measuredOmega(w, 0, 0)
NavState predict(const NavState &state_i, const imuBias::ConstantBias &bias_i, OptionalJacobian< 9, 9 > H1={}, OptionalJacobian< 9, 6 > H2={}) const
Predict state at time j.
ofstream os("timeSchurFactors.csv")
GTSAM_EXPORT friend std::ostream & operator<<(std::ostream &os, const PreintegrationBase &pim)
std::pair< Vector3, Vector3 > correctMeasurementsBySensorPose(const Vector3 &unbiasedAcc, const Vector3 &unbiasedOmega, OptionalJacobian< 3, 3 > correctedAcc_H_unbiasedAcc={}, OptionalJacobian< 3, 3 > correctedAcc_H_unbiasedOmega={}, OptionalJacobian< 3, 3 > correctedOmega_H_unbiasedOmega={}) const
virtual Vector3 deltaVij() const =0
std::optional< Pose3 > body_P_sensor
The pose of the sensor in the body frame.
const Vector3 & gyroscope() const
Definition: ImuBias.h:71
float * p
Vector9 localCoordinates(const NavState &g, OptionalJacobian< 9, 9 > H1={}, OptionalJacobian< 9, 9 > H2={}) const
localCoordinates with optional derivatives
Definition: NavState.cpp:133
virtual Vector9 biasCorrectedDelta(const imuBias::ConstantBias &bias_i, OptionalJacobian< 9, 6 > H={}) const =0
static double error
Definition: testRot3.cpp:37
Vector3 ypr(OptionalJacobian< 3, 3 > H={}) const
Definition: Rot3.cpp:183
Bias biasHat_
Acceleration and gyro bias used for preintegration.


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autogenerated on Tue Jul 4 2023 02:35:15