SunEarthMagAttDet:

Path: SpacecraftEstimation/AttitudeEstimation

% Attitude determination using a sun, earth and magnetic field vectors.
 Uses an IMU base. angInc comes from the IMU. This uses the Unscented Kalman
 Filter (UKF).
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   Form:
           ukf = SunEarthMagAttDet    % default data structure
   [q, b, ukf] = SunEarthMagAttDet( angInc, q, b, ukf, r, dT, sensorData )
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   ------
   Inputs
   ------
   angInc      (n,1)	Angular increments
   q         	(4,1)	Attitude quaternion
   b         	(3,1)	Bias
   ukf        	(.)   UKF data structure
   r           (.)   Measurement data structure
   dT          (1,1)	Time step
   sensorData	(.) 	Sensor data structure

   -------
   Outputs
   -------
   q           (4,1)	Attitude quaternion
   b         	(3,1)	Bias
   ukf       	(.)  	UKF data structure

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  See also UKFUpdate, MeasurementsSunMagUKF, QFromDQ, DSTM, RHSGyroUKF
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Children:

Common: Estimation/KFInitialize
Common: Estimation/UKFUpdate
Common: Estimation/UKFWeight
Common: Quaternion/QFromDQ
SpacecraftEstimation: SensorMeas/MeasurementsSunMagUKF
SpacecraftEstimation: StellarAttDet/AttProp
SpacecraftEstimation: StellarAttDet/DSTM

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