forked from Archive/PX4-Autopilot
PreflightCheck trivial astyle fix
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@ -576,10 +576,12 @@ static bool ekf2Check(orb_advert_t *mavlink_log_pub, vehicle_status_s &vehicle_s
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// check accelerometer delta velocity bias estimates
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param_get(param_find("COM_ARM_EKF_AB"), &test_limit);
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for (uint8_t index=13; index<16; index++) {
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for (uint8_t index = 13; index < 16; index++) {
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// allow for higher uncertainty in estimates for axes that are less observable to prevent false positives
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// adjust test threshold by 3-sigma
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float test_uncertainty = 3.0f * sqrtf(fmaxf(status.covariances[index],0.0f));
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float test_uncertainty = 3.0f * sqrtf(fmaxf(status.covariances[index], 0.0f));
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if (fabsf(status.states[index]) > test_limit + test_uncertainty) {
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if (report_fail) {
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mavlink_log_critical(mavlink_log_pub, "Preflight Fail: High Accelerometer Bias");
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