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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-22 13:23:34 +08:00
ekf2: migrate mag declination to SymForce
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@@ -47,6 +47,7 @@
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#include "python/ekf_derivation/generated/compute_mag_z_innov_var_and_h.h"
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#include "python/ekf_derivation/generated/compute_yaw_321_innov_var_and_h.h"
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#include "python/ekf_derivation/generated/compute_yaw_312_innov_var_and_h.h"
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#include "python/ekf_derivation/generated/compute_mag_declination_innov_innov_var_and_h.h"
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#include <mathlib/mathlib.h>
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@@ -333,63 +334,24 @@ bool Ekf::fuseYaw(const float innovation, const float variance, estimator_aid_so
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bool Ekf::fuseDeclination(float decl_sigma)
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{
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// assign intermediate state variables
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const float magN = _state.mag_I(0);
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const float magE = _state.mag_I(1);
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// minimum North field strength before calculation becomes badly conditioned (T)
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constexpr float N_field_min = 0.001f;
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// observation variance (rad**2)
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const float R_DECL = sq(decl_sigma);
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// Calculate intermediate variables
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if (fabsf(magN) < sq(N_field_min)) {
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// calculation is badly conditioned close to +-90 deg declination
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return false;
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}
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Vector24f H;
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float innovation;
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float innovation_variance;
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const float HK0 = ecl::powf(magN, -2);
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const float HK1 = HK0*ecl::powf(magE, 2) + 1.0F;
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const float HK2 = 1.0F/HK1;
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const float HK3 = 1.0F/magN;
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const float HK4 = HK2*HK3;
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const float HK5 = HK3*magE;
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const float HK6 = HK5*P(16,17) - P(17,17);
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const float HK7 = ecl::powf(HK1, -2);
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const float HK8 = HK5*P(16,16) - P(16,17);
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const float innovation_variance = -HK0*HK6*HK7 + HK7*HK8*magE/ecl::powf(magN, 3) + R_DECL;
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float HK9;
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sym::ComputeMagDeclinationInnovInnovVarAndH(getStateAtFusionHorizonAsVector(), P, getMagDeclination(), R_DECL, FLT_EPSILON, &innovation, &innovation_variance, &H);
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if (innovation_variance > R_DECL) {
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HK9 = HK4/innovation_variance;
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} else {
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if (innovation_variance < R_DECL) {
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// variance calculation is badly conditioned
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return false;
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}
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// Calculate the observation Jacobian
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// Note only 2 terms are non-zero which can be used in matrix operations for calculation of Kalman gains and covariance update to significantly reduce cost
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// Note Hfusion indices do not match state indices
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SparseVector24f<16,17> Hfusion;
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Hfusion.at<16>() = -HK0*HK2*magE;
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Hfusion.at<17>() = HK4;
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SparseVector24f<16,17> Hfusion(H);
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// Calculate the Kalman gains
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Vector24f Kfusion;
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for (unsigned row = 0; row <= 15; row++) {
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Kfusion(row) = -HK9*(HK5*P(row,16) - P(row,17));
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}
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Kfusion(16) = -HK8*HK9;
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Kfusion(17) = -HK6*HK9;
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for (unsigned row = 18; row <= 23; row++) {
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Kfusion(row) = -HK9*(HK5*P(16,row) - P(17,row));
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}
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const float innovation = math::constrain(atan2f(magE, magN) - getMagDeclination(), -0.5f, 0.5f);
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Vector24f Kfusion = P * Hfusion / innovation_variance;
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const bool is_fused = measurementUpdate(Kfusion, Hfusion, innovation);
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@@ -321,6 +321,22 @@ def compute_yaw_312_innov_var_and_h_alternate(
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return (innov_var, H.T)
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def compute_mag_declination_innov_innov_var_and_h(
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state: VState,
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P: MState,
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meas: sf.Scalar,
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R: sf.Scalar,
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epsilon: sf.Scalar
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) -> (sf.Scalar, VState):
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meas_pred = sf.atan2(state[State.iy], state[State.ix], epsilon=epsilon)
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innov = meas_pred - meas
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H = sf.V1(meas_pred).jacobian(state)
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innov_var = (H * P * H.T + R)[0,0]
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return (innov, innov_var, H.T)
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print("Derive EKF2 equations...")
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generate_px4_function(compute_airspeed_innov_and_innov_var, output_names=["innov", "innov_var"])
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generate_px4_function(compute_airspeed_h_and_k, output_names=["H", "K"])
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@@ -335,3 +351,4 @@ generate_px4_function(compute_yaw_321_innov_var_and_h, output_names=["innov_var"
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generate_px4_function(compute_yaw_321_innov_var_and_h_alternate, output_names=["innov_var", "H"])
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generate_px4_function(compute_yaw_312_innov_var_and_h, output_names=["innov_var", "H"])
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generate_px4_function(compute_yaw_312_innov_var_and_h_alternate, output_names=["innov_var", "H"])
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generate_px4_function(compute_mag_declination_innov_innov_var_and_h, output_names=["innov", "innov_var", "H"])
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+74
@@ -0,0 +1,74 @@
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// -----------------------------------------------------------------------------
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// This file was autogenerated by symforce from template:
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// backends/cpp/templates/function/FUNCTION.h.jinja
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// Do NOT modify by hand.
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// -----------------------------------------------------------------------------
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#pragma once
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#include <matrix/math.hpp>
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namespace sym {
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/**
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* This function was autogenerated from a symbolic function. Do not modify by hand.
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*
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* Symbolic function: compute_mag_declination_innov_innov_var_and_h
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*
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* Args:
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* state: Matrix24_1
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* P: Matrix24_24
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* meas: Scalar
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* R: Scalar
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* epsilon: Scalar
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*
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* Outputs:
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* innov: Scalar
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* innov_var: Scalar
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* H: Matrix24_1
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*/
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template <typename Scalar>
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void ComputeMagDeclinationInnovInnovVarAndH(const matrix::Matrix<Scalar, 24, 1>& state,
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const matrix::Matrix<Scalar, 24, 24>& P,
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const Scalar meas, const Scalar R, const Scalar epsilon,
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Scalar* const innov = nullptr,
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Scalar* const innov_var = nullptr,
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matrix::Matrix<Scalar, 24, 1>* const H = nullptr) {
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// Total ops: 23
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// Input arrays
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// Intermediate terms (4)
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const Scalar _tmp0 =
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epsilon * ((((state(16, 0)) > 0) - ((state(16, 0)) < 0)) + Scalar(0.5)) + state(16, 0);
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const Scalar _tmp1 =
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Scalar(1.0) / (std::pow(_tmp0, Scalar(2)) + std::pow(state(17, 0), Scalar(2)));
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const Scalar _tmp2 = _tmp1 * state(17, 0);
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const Scalar _tmp3 = _tmp0 * _tmp1;
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// Output terms (3)
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if (innov != nullptr) {
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Scalar& _innov = (*innov);
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_innov = -meas + std::atan2(state(17, 0), _tmp0);
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}
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if (innov_var != nullptr) {
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Scalar& _innov_var = (*innov_var);
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_innov_var = R - _tmp2 * (-P(16, 16) * _tmp2 + P(17, 16) * _tmp3) +
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_tmp3 * (-P(16, 17) * _tmp2 + P(17, 17) * _tmp3);
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}
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if (H != nullptr) {
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matrix::Matrix<Scalar, 24, 1>& _H = (*H);
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_H.setZero();
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_H(16, 0) = -_tmp2;
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_H(17, 0) = _tmp3;
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}
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} // NOLINT(readability/fn_size)
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// NOLINTNEXTLINE(readability/fn_size)
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} // namespace sym
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