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EKF angle constants in degrees for readability (#465)
* EKF angle constants in degrees for readability * EKF make FILTER_UPDATE_PERIOD_MS static constexpr and add FILTER_UPDATE_PERIOD_S * EKF controlOpticalFlowFusion() use constants and update comments * EKF controlMagFusion() use angle in degrees * EKF move earth spin rate to geo and update usage * EKF: Fix numerical constant error and clean up comments Comments do not need to contain numerical values when the code makes these clear.
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committed by
Paul Riseborough
parent
cebdc3d829
commit
41953ab582
+3
-3
@@ -55,7 +55,7 @@ void Ekf::initialiseCovariance()
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}
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// calculate average prediction time step in sec
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float dt = 0.001f * (float)FILTER_UPDATE_PERIOD_MS;
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float dt = FILTER_UPDATE_PERIOD_S;
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// define the initial angle uncertainty as variances for a rotation vector
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Vector3f rot_vec_var;
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@@ -150,7 +150,7 @@ void Ekf::predictCovariance()
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float dvy_b = _state.accel_bias(1);
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float dvz_b = _state.accel_bias(2);
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float dt = math::constrain(_imu_sample_delayed.delta_ang_dt, 0.0005f * FILTER_UPDATE_PERIOD_MS, 0.002f * FILTER_UPDATE_PERIOD_MS);
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float dt = math::constrain(_imu_sample_delayed.delta_ang_dt, 0.5f * FILTER_UPDATE_PERIOD_S, 2.0f * FILTER_UPDATE_PERIOD_S);
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float dt_inv = 1.0f / dt;
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// compute noise variance for stationary processes
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@@ -907,7 +907,7 @@ void Ekf::resetWindCovariance()
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// calculate the uncertainty in wind speed and direction using the uncertainty in airspeed and sideslip angle
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// used to calculate the initial wind speed
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float R_spd = sq(math::constrain(_params.eas_noise, 0.5f, 5.0f) * math::constrain(_airspeed_sample_delayed.eas2tas, 0.9f, 10.0f));
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float R_yaw = sq(0.1745f);
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float R_yaw = sq(math::radians(10.0f));
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// calculate the variance and covariance terms for the wind states
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float cos_yaw = cosf(yaw);
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