25 #include <boost/make_shared.hpp> 32 PreintegrationBase::PreintegrationBase(
const boost::shared_ptr<Params>&
p,
34 : p_(p), biasHat_(biasHat), deltaTij_(0.0) {
39 os <<
" deltaTij = " << pim.
deltaTij_ << endl;
40 os <<
" deltaRij.ypr = (" << pim.
deltaRij().
ypr().transpose() <<
")" << endl;
41 os <<
" deltaPij = " << pim.
deltaPij().transpose() << endl;
42 os <<
" deltaVij = " << pim.
deltaVij().transpose() << endl;
50 cout << (s.empty() ? s : s +
"\n") << *
this << endl;
65 assert(
p().body_P_sensor);
76 const Vector3 correctedOmega = bRs * unbiasedOmega;
79 if (correctedAcc_H_unbiasedAcc) *correctedAcc_H_unbiasedAcc = bRs;
80 if (correctedAcc_H_unbiasedOmega) *correctedAcc_H_unbiasedOmega = Z_3x3;
81 if (correctedOmega_H_unbiasedOmega) *correctedOmega_H_unbiasedOmega = bRs;
85 if (!b_arm.isZero()) {
88 const Matrix3 body_Omega_body =
skewSymmetric(correctedOmega);
89 const Vector3 b_velocity_bs = body_Omega_body * b_arm;
90 correctedAcc -= body_Omega_body * b_velocity_bs;
93 if (correctedAcc_H_unbiasedOmega) {
94 double wdp = correctedOmega.dot(b_arm);
95 const Matrix3 diag_wdp = Vector3::Constant(wdp).asDiagonal();
96 *correctedAcc_H_unbiasedOmega = -( diag_wdp
97 + correctedOmega * b_arm.transpose()) * bRs.matrix()
98 + 2 * b_arm * unbiasedOmega.transpose();
102 return make_pair(correctedAcc, correctedOmega);
112 update(measuredAcc, measuredOmega, dt, &A, &B, &C);
119 Matrix96 D_biasCorrected_bias;
121 H2 ? &D_biasCorrected_bias :
nullptr);
124 Matrix9 D_delta_state, D_delta_biasCorrected;
126 p().omegaCoriolis,
p().use2ndOrderCoriolis, H1 ? &D_delta_state :
nullptr,
127 H2 ? &D_delta_biasCorrected :
nullptr);
130 Matrix9 D_predict_state, D_predict_delta;
132 H1 ? &D_predict_state :
nullptr,
133 H2 || H2 ? &D_predict_delta :
nullptr);
135 *H1 = D_predict_state + D_predict_delta * D_delta_state;
137 *H2 = D_predict_delta * D_delta_biasCorrected * D_biasCorrected_bias;
150 Matrix96 D_predict_bias_i;
152 state_i, bias_i, H1 ? &D_predict_state_i : 0, H3 ? &D_predict_bias_i : 0);
155 Matrix9 D_error_state_j, D_error_predict;
158 H1 || H3 ? &D_error_predict : 0);
160 if (H1) *H1 << D_error_predict* D_predict_state_i;
161 if (H2) *H2 << D_error_state_j;
162 if (H3) *H3 << D_error_predict* D_predict_bias_i;
180 Matrix9 D_error_state_i, D_error_state_j;
182 H1 || H2 ? &D_error_state_i : 0, H3 || H4 ? &D_error_state_j : 0, H5);
189 if (H1) *H1 << D_error_state_i.leftCols<6>();
190 if (H2) *H2 << D_error_state_i.rightCols<3>() * state_i.
R().transpose();
191 if (H3) *H3 << D_error_state_j.leftCols<6>();
192 if (H4) *H4 << D_error_state_j.rightCols<3>() * state_j.
R().transpose();
const imuBias::ConstantBias & biasHat() const
Vector3 correctedAcc(const PreintegratedImuMeasurements &pim, const Vector3 &measuredAcc, const Vector3 &measuredOmega)
Vector9 correctPIM(const Vector9 &pim, double dt, const Vector3 &n_gravity, const boost::optional< Vector3 > &omegaCoriolis, bool use2ndOrderCoriolis=false, OptionalJacobian< 9, 9 > H1=boost::none, OptionalJacobian< 9, 9 > H2=boost::none) const
Vector9 localCoordinates(const NavState &g, OptionalJacobian< 9, 9 > H1=boost::none, OptionalJacobian< 9, 9 > H2=boost::none) const
localCoordinates with optional derivatives
virtual void update(const Vector3 &measuredAcc, const Vector3 &measuredOmega, const double dt, Matrix9 *A, Matrix93 *B, Matrix93 *C)=0
const Vector3 & accelerometer() const
Some functions to compute numerical derivatives.
Vector3 ypr(OptionalJacobian< 3, 3 > H=boost::none) const
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.
Matrix< SCALARB, Dynamic, Dynamic > B
std::pair< Vector3, Vector3 > correctMeasurementsBySensorPose(const Vector3 &unbiasedAcc, const Vector3 &unbiasedOmega, OptionalJacobian< 3, 3 > correctedAcc_H_unbiasedAcc=boost::none, OptionalJacobian< 3, 3 > correctedAcc_H_unbiasedOmega=boost::none, OptionalJacobian< 3, 3 > correctedOmega_H_unbiasedOmega=boost::none) const
NavState predict(const NavState &state_i, const imuBias::ConstantBias &bias_i, OptionalJacobian< 9, 9 > H1=boost::none, OptionalJacobian< 9, 6 > H2=boost::none) const
Predict state at time j.
virtual Rot3 deltaRij() const =0
virtual Vector3 deltaPij() const =0
NavState retract(const Vector9 &v, OptionalJacobian< 9, 9 > H1=boost::none, OptionalJacobian< 9, 9 > H2=boost::none) const
retract with optional derivatives
void resetIntegrationAndSetBias(const Bias &biasHat)
virtual void resetIntegration()=0
Params & p() const
const reference to params
static const Vector3 measuredAcc
boost::optional< Pose3 > body_P_sensor
The pose of the sensor in the body frame.
double deltaTij_
Time interval from i to j.
Matrix< Scalar, Dynamic, Dynamic > C
const Vector3 & gyroscope() const
virtual void integrateMeasurement(const Vector3 &measuredAcc, const Vector3 &measuredOmega, const double dt)
Version without derivatives.
Matrix3 skewSymmetric(double wx, double wy, double wz)
static const Vector3 measuredOmega(w, 0, 0)
ofstream os("timeSchurFactors.csv")
GTSAM_EXPORT friend std::ostream & operator<<(std::ostream &os, const PreintegrationBase &pim)
virtual Vector3 deltaVij() const =0
Matrix3 R() const
Return rotation matrix. Induces computation in quaternion mode.
virtual Vector9 biasCorrectedDelta(const imuBias::ConstantBias &bias_i, OptionalJacobian< 9, 6 > H=boost::none) const =0
virtual void print(const std::string &s="") const
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=boost::none, OptionalJacobian< 9, 3 > H2=boost::none, OptionalJacobian< 9, 6 > H3=boost::none, OptionalJacobian< 9, 3 > H4=boost::none, OptionalJacobian< 9, 6 > H5=boost::none) const
Bias biasHat_
Acceleration and gyro bias used for preintegration.