Path: SC/Dynamics
% Rigid body right-hand-side. -------------------------------------------------------------------------- Form: xDot = FRB( x, t, inr, invInr, tExt ) -------------------------------------------------------------------------- ------ Inputs ------ x (7,1) The state vector [q;w] t (1,1) Time (unused) inr (3,3) Inertia invInr (3,3) Inverse inertia tExt (3,1) External torque ------- Outputs ------- xDot (7,1) The derivative of the state vector -------------------------------------------------------------------------- See also RBModel --------------------------------------------------------------------------
AerospaceUtils: Coord/QIToBDot SC: Dynamics/RBModel
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