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SUPPORT SITE |
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SUPPORT SITE |
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Path: SpacecraftEstimation/StellarAttDet
% Propagates the quaternion assuming constant rate.
For use by UKF.
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Form:
x = IntGyroQuaternion( fun, x, dT, t, d )
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Inputs
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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
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Outputs
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x (6,1) [delta Q; delta bias]
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Common: Quaternion/QMult Common: Quaternion/QPose Math: Linear/Unit SpacecraftEstimation: StellarAttDet/AttProp
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