Path: SCPro/DynamicalModels
% Linearized attitude dynamics for a rigid body.
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Form:
d = RHSRigidBodyLinear
xDot = RHSRigidBodyLinear( x, t, d )
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Inputs
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x (7,1) State vector [q;omega]
t (1,1) Time (s) (unused)
d (1,1) Data structure
.inertia (3,3) Inertia matrix
.torque (3,1) Torque vector
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Outputs
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xDot (:,1) d[q;omega]/dt
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AerospaceUtils: Coord/QIToBDot Common: Control/C2DZOH Math: Linear/SkewSymm
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