Path: SC/Dynamics
% Linearized attitude dynamics for a rigid body. -------------------------------------------------------------------------- Form: d = RHSRigidBodyLinear xDot = RHSRigidBodyLinear( x, t, d ) -------------------------------------------------------------------------- ------- Inputs ------- 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 ------- Outputs ------- xDot (:,1) d[q;omega]/dt --------------------------------------------------------------------------
AerospaceUtils: Coord/QIToBDot
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