RYGCAttDet:

Path: SpacecraftEstimation/AttitudeEstimation

% An attitude determination system using roll/yaw gyrocompassing.
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   Form:
   [q, p] = RYGCAttDet( angInc, q, dT, b, p, Q, r, m, mGyro )
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   ------
   Inputs
   ------
   angInc       (n,1)     Angular increments
   q            (3,1)     Attitude vector
   dT           (1,1)     Time step
   b            (3,1)     Bias
   p            (3,3)     State covariance matrix
   Q            (3,3)     State noise covariance
   r            (1,1)     Measurement noise
   m            (2,1)     [roll;pitch] (rad)
   mGyro        (3,3)     Gyro unit vectors

   -------
   Outputs
   -------
   q            (4,1)     Attitude quaternion
   p            (3,3)     State covariance matrix

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Children:

SpacecraftEstimation: AttitudeEstimation/EKFSSG
SpacecraftEstimation: AttitudeEstimation/YawRollGyroCompassing

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