mirror of https://github.com/ArduPilot/ardupilot
AP_NavEKF: tuning change to accel bias learning
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@ -110,7 +110,7 @@ extern const AP_HAL::HAL& hal;
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// initial imu bias uncertainty (deg/sec)
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#define INIT_GYRO_BIAS_UNCERTAINTY 0.1f
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#define INIT_ACCEL_BIAS_UNCERTAINTY 0.5f
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#define INIT_ACCEL_BIAS_UNCERTAINTY 0.3f
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// Define tuning parameters
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const AP_Param::GroupInfo NavEKF::var_info[] PROGMEM = {
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@ -389,7 +389,7 @@ NavEKF::NavEKF(const AP_AHRS *ahrs, AP_Baro &baro) :
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magFailTimeLimit_ms(10000), // number of msec before a magnetometer failing innovation consistency checks is declared failed (msec)
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magVarRateScale(0.05f), // scale factor applied to magnetometer variance due to angular rate
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gyroBiasNoiseScaler(2.0f), // scale factor applied to imu gyro bias learning before the vehicle is armed
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accelBiasNoiseScaler(1.4f), // scale factor applied to imu accel bias learning before the vehicle is armed
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accelBiasNoiseScaler(1.0f), // scale factor applied to imu accel bias learning before the vehicle is armed
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msecGpsAvg(200), // average number of msec between GPS measurements
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msecHgtAvg(100), // average number of msec between height measurements
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msecMagAvg(100), // average number of msec between magnetometer measurements
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