mirror of https://github.com/ArduPilot/ardupilot
AP_NavEKF: fixed minimum deltat to be 100us
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@ -4066,7 +4066,7 @@ void NavEKF::readIMUData()
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const AP_InertialSensor &ins = _ahrs->get_ins();
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const AP_InertialSensor &ins = _ahrs->get_ins();
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dtIMUavg = 1.0f/ins.get_sample_rate();
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dtIMUavg = 1.0f/ins.get_sample_rate();
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dtIMUactual = max(ins.get_delta_time(),1.0e-3f);
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dtIMUactual = max(ins.get_delta_time(),1.0e-4f);
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// the imu sample time is used as a common time reference throughout the filter
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// the imu sample time is used as a common time reference throughout the filter
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imuSampleTime_ms = hal.scheduler->millis();
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imuSampleTime_ms = hal.scheduler->millis();
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