From aceca6b2a929482ba1c32c553dc98478ea40dfb8 Mon Sep 17 00:00:00 2001 From: Lorenz Meier Date: Sun, 15 Mar 2015 10:39:21 +0100 Subject: Fix gyro offset calculation --- .../ekf_att_pos_estimator_main.cpp | 14 +++++++------- .../ekf_att_pos_estimator/estimator_22states.cpp | 20 +++++++++++++------- 2 files changed, 20 insertions(+), 14 deletions(-) diff --git a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp index 6ca10e56a..c16e72ea0 100644 --- a/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp +++ b/src/modules/ekf_att_pos_estimator/ekf_att_pos_estimator_main.cpp @@ -784,14 +784,14 @@ void AttitudePositionEstimatorEKF::publishAttitude() _att.pitch = euler(1); _att.yaw = euler(2); - _att.rollspeed = _ekf->angRate.x - _ekf->states[10] / _ekf->dtIMU; - _att.pitchspeed = _ekf->angRate.y - _ekf->states[11] / _ekf->dtIMU; - _att.yawspeed = _ekf->angRate.z - _ekf->states[12] / _ekf->dtIMU; + _att.rollspeed = _ekf->angRate.x - _ekf->states[10] / _ekf->dtIMUfilt; + _att.pitchspeed = _ekf->angRate.y - _ekf->states[11] / _ekf->dtIMUfilt; + _att.yawspeed = _ekf->angRate.z - _ekf->states[12] / _ekf->dtIMUfilt; // gyro offsets - _att.rate_offsets[0] = _ekf->states[10] / _ekf->dtIMU; - _att.rate_offsets[1] = _ekf->states[11] / _ekf->dtIMU; - _att.rate_offsets[2] = _ekf->states[12] / _ekf->dtIMU; + _att.rate_offsets[0] = _ekf->states[10] / _ekf->dtIMUfilt; + _att.rate_offsets[1] = _ekf->states[11] / _ekf->dtIMUfilt; + _att.rate_offsets[2] = _ekf->states[12] / _ekf->dtIMUfilt; /* lazily publish the attitude only once available */ if (_att_pub > 0) { @@ -1069,7 +1069,7 @@ void AttitudePositionEstimatorEKF::print_status() // 16-18: Earth Magnetic Field Vector - gauss (North, East, Down) // 19-21: Body Magnetic Field Vector - gauss (X,Y,Z) - printf("dtIMU: %8.6f IMUmsec: %d\n", (double)_ekf->dtIMU, (int)IMUmsec); + printf("dtIMU: %8.6f filt: %8.6f IMUmsec: %d\n", (double)_ekf->dtIMU, (double)_ekf->dtIMUfilt, (int)IMUmsec); printf("baro alt: %8.4f GPS alt: %8.4f\n", (double)_baro.altitude, (double)(_gps.alt / 1e3f)); printf("baro ref offset: %8.4f baro GPS offset: %8.4f\n", (double)_baro_ref_offset, (double)_baro_gps_offset); diff --git a/src/modules/ekf_att_pos_estimator/estimator_22states.cpp b/src/modules/ekf_att_pos_estimator/estimator_22states.cpp index c313e83af..4fac83db2 100644 --- a/src/modules/ekf_att_pos_estimator/estimator_22states.cpp +++ b/src/modules/ekf_att_pos_estimator/estimator_22states.cpp @@ -210,7 +210,7 @@ void AttPosEKF::InitialiseParameters() yawVarScale = 1.0f; windVelSigma = 0.1f; - dAngBiasSigma = 5.0e-7f; + dAngBiasSigma = 5.0e-7; dVelBiasSigma = 1e-4f; magEarthSigma = 3.0e-4f; magBodySigma = 3.0e-4f; @@ -414,9 +414,10 @@ void AttPosEKF::CovariancePrediction(float dt) // calculate covariance prediction process noise for (uint8_t i= 0; i<4; i++) processNoise[i] = 1.0e-9f; for (uint8_t i= 4; i<10; i++) processNoise[i] = 1.0e-9f; - for (uint8_t i=10; i<=12; i++) processNoise[i] = dt * dAngBiasSigma; // scale gyro bias noise when on ground to allow for faster bias estimation - for (uint8_t i=10; i<=12; i++) processNoise[i] = dt * dAngBiasSigma; + float gyroBiasScale = (_onGround) ? 2.0f : 1.0f; + + for (uint8_t i=10; i<=12; i++) processNoise[i] = dt * dAngBiasSigma * gyroBiasScale; processNoise[13] = dVelBiasSigma; if (!inhibitWindStates) { for (uint8_t i=14; i<=15; i++) processNoise[i] = dt * windVelSigma; @@ -2706,6 +2707,11 @@ void AttPosEKF::ConstrainStates() // 16-18: Earth Magnetic Field Vector - gauss (North, East, Down) // 19-21: Body Magnetic Field Vector - gauss (X,Y,Z) + // Constrain dtIMUfilt + if (!isfinite(dtIMUfilt) || (fabsf(dtIMU - dtIMUfilt) > 0.01f)) { + dtIMUfilt = dtIMU; + } + // Constrain quaternion for (size_t i = 0; i <= 3; i++) { states[i] = ConstrainFloat(states[i], -1.0f, 1.0f); @@ -2727,11 +2733,11 @@ void AttPosEKF::ConstrainStates() // Angle bias limit - set to 8 degrees / sec for (size_t i = 10; i <= 12; i++) { - states[i] = ConstrainFloat(states[i], -0.12f * dtIMU, 0.12f * dtIMU); + states[i] = ConstrainFloat(states[i], -0.16f * dtIMUfilt, 0.16f * dtIMUfilt); } // Constrain delta velocity bias - states[13] = ConstrainFloat(states[13], -1.0f * dtIMU, 1.0f * dtIMU); + states[13] = ConstrainFloat(states[13], -1.0f * dtIMUfilt, 1.0f * dtIMUfilt); // Wind velocity limits - assume 120 m/s max velocity for (size_t i = 14; i <= 15; i++) { @@ -2795,8 +2801,8 @@ bool AttPosEKF::GyroOffsetsDiverged() // Protect against division by zero if (delta_len > 0.0f) { - float cov_mag = ConstrainFloat((P[10][10] + P[11][11] + P[12][12]), 1e-12f, 1e-8f); - delta_len_scaled = (5e-7 / (double)cov_mag) * (double)delta_len / (double)dtIMU; + float cov_mag = ConstrainFloat((P[10][10] + P[11][11] + P[12][12]), 1e-12f, 1e-2f); + delta_len_scaled = (5e-7 / (double)cov_mag) * (double)delta_len / (double)dtIMUfilt; } bool diverged = (delta_len_scaled > 1.0f); -- cgit v1.2.3