forked from Archive/PX4-Autopilot
EKF: Fix travis clang build error
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@ -156,8 +156,8 @@ void Ekf::predictCovariance()
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// inhibit learning of imu acccel bias if the manoeuvre levels are too high to protect against the effect of sensor nonlinearities or bad accel data is detected
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float alpha = 1.0f - math::constrain((dt / _params.acc_bias_learn_tc), 0.0f, 1.0f);
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_ang_rate_mag_filt = fmax(_imu_sample_delayed.delta_ang.norm(), alpha * _ang_rate_mag_filt);
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_accel_mag_filt = fmax(_imu_sample_delayed.delta_vel.norm(), alpha * _accel_mag_filt);
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_ang_rate_mag_filt = fmaxf(_imu_sample_delayed.delta_ang.norm(), alpha * _ang_rate_mag_filt);
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_accel_mag_filt = fmaxf(_imu_sample_delayed.delta_vel.norm(), alpha * _accel_mag_filt);
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if (_ang_rate_mag_filt > dt * _params.acc_bias_learn_gyr_lim
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|| _accel_mag_filt > dt * _params.acc_bias_learn_acc_lim
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|| _bad_vert_accel_detected) {
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@ -94,7 +94,7 @@ void Ekf::fuseDrag()
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// Estimate the derivative of specific force wrt airspeed along the X axis
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// Limit lower value to prevent arithmetic exceptions
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float Kacc = fmax(1e-1f,rho * BC_inv_x * airSpd);
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float Kacc = fmaxf(1e-1f,rho * BC_inv_x * airSpd);
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SH_ACC[0] = sq(q0) + sq(q1) - sq(q2) - sq(q3);
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SH_ACC[1] = vn - vwn;
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@ -164,7 +164,7 @@ void Ekf::fuseDrag()
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// Estimate the derivative of specific force wrt airspeed along the X axis
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// Limit lower value to prevent arithmetic exceptions
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float Kacc = fmax(1e-1f,rho * BC_inv_y * airSpd);
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float Kacc = fmaxf(1e-1f,rho * BC_inv_y * airSpd);
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SH_ACC[0] = sq(q0) - sq(q1) + sq(q2) - sq(q3);
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SH_ACC[1] = vn - vwn;
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