Path: FormationFlying/IntegratedSim
% Right-hand-side of the spacecraft dynamic equations for the DFF system.
Includes position, velocity, orientation, body rate, mass.
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Inputs
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x (:,1) State vector
jD (1,1) Time in Julian Date
prop (.) Not used
control (.) Data structure with force and torque
scData (.) Data structure of spacecraft data
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Outputs
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xDot (:,1) State vector derivative
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AerospaceUtils: Coord/QIToBDot SC: BasicOrbit/FOrbCart Common: Control/C2DZOH Math: Linear/Cross Math: Linear/Mag Math: Linear/SkewSymm
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