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AP_NavEKF: update params for copter
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@ -50,9 +50,9 @@ NavEKF::NavEKF(const AP_AHRS *ahrs, AP_Baro &baro) :
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#endif
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#endif
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{
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{
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// Tuning parameters
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// Tuning parameters
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_gpsHorizVelNoise = 0.3f; // GPS horizontal velocity noise : m/s
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_gpsHorizVelNoise = 0.7f; // GPS horizontal velocity noise : m/s
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_gpsVertVelNoise = 0.3f; // GPS vertical velocity noise : m/s
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_gpsVertVelNoise = 0.3f; // GPS vertical velocity noise : m/s
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_gpsHorizPosNoise = 2.0f; // GPS horizontal position noise m
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_gpsHorizPosNoise = 1.5f; // GPS horizontal position noise m
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_gpsVertPosNoise = 2.0f; // GPS or Baro vertical position noise : m
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_gpsVertPosNoise = 2.0f; // GPS or Baro vertical position noise : m
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_gpsVelVarAccScale = 0.2f; // scale factor applied to velocity variance due to Vdot
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_gpsVelVarAccScale = 0.2f; // scale factor applied to velocity variance due to Vdot
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_gpsPosVarAccScale = 0.2f; // scale factor applied to position variance due to Vdot
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_gpsPosVarAccScale = 0.2f; // scale factor applied to position variance due to Vdot
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@ -62,7 +62,7 @@ NavEKF::NavEKF(const AP_AHRS *ahrs, AP_Baro &baro) :
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_windStateNoise = 0.1f; // RMS rate of change of wind : (m/s^2)
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_windStateNoise = 0.1f; // RMS rate of change of wind : (m/s^2)
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_wndVarHgtRateScale = 0.5f; // scale factor applied to wind process noise from height rate
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_wndVarHgtRateScale = 0.5f; // scale factor applied to wind process noise from height rate
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_gyrNoise = 1.4544411e-2f; // gyro process noise : rad/s
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_gyrNoise = 1.4544411e-2f; // gyro process noise : rad/s
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_accNoise = 0.5f; // accelerometer process noise : m/s^2
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_accNoise = 0.02f; // accelerometer process noise : m/s^2
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_dAngBiasNoise = 5.0e-7f; // gyro bias state noise : rad/s^2
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_dAngBiasNoise = 5.0e-7f; // gyro bias state noise : rad/s^2
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_magEarthNoise = 3.0e-4f; // earth magnetic field process noise : gauss/sec
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_magEarthNoise = 3.0e-4f; // earth magnetic field process noise : gauss/sec
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_magBodyNoise = 3.0e-4f; // body magnetic field process noise : gauss/sec
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_magBodyNoise = 3.0e-4f; // body magnetic field process noise : gauss/sec
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