IntGyroQuaternion:

Path: SpacecraftEstimation/StellarAttDet

% Propagates the quaternion assuming constant rate.
 For use by UKF.
--------------------------------------------------------------------------
   Form:
   x = IntGyroQuaternion( fun, x, dT, t, d )
--------------------------------------------------------------------------

   ------
   Inputs
   ------
   fun          (1,:)     Not used
   x            (3,1)     [delta Q; delta bias]
   dT           (1,1)     Time step
   t            (1,1)     Time (not used)
   d            (1,1)     Data structure
                          .q (4,1) Quaternion
                          .w (3,1) angular velocity
                          .b (3,1) bias error

   -------
   Outputs
   -------
   x            (6,1)     [delta Q; delta bias]

--------------------------------------------------------------------------

Children:

SpacecraftEstimation: StellarAttDet/AttProp
Common: Quaternion/QMult
Common: Quaternion/QPose
Common: Quaternion/QUnit
Math: Linear/DupVect
Math: Linear/Mag
Math: Linear/SkewSymm
Math: Linear/Unit

Back to the SpacecraftEstimation Module page