Path: SCPro/DynamicalModels
% Right-hand-side of the spacecraft dynamical equations.
This function includes position, orientation
and 4 reaction wheels. It also includes time varying inertia.
This right hand side is primarily to analyze control during deployment.
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Inputs
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x (:,1) State vector
t (1,1) Time
d (.) Data structure for the simulation
.uRWA (3,4) Reaction wheel unit vectors
.inrRWA (1,1) Reaction wheel inertia
.tRWA (4,1) Reaction wheel torque
.funIandD (1,:) Disturbance and inertia model
.tExt (3,1) Other external torques
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Outputs
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xDot (:,1) State vector derivative
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