Path: SC/Dynamics
% Attitude simulation of a rigid body. Since version 1. -------------------------------------------------------------------------- Form: xDot = ASim( x, t, inertia, torque ) -------------------------------------------------------------------------- ------ Inputs ------ x (7,1) [Attitude quaternion; attitude rate] t Time inertia (3,3) Inertia matrix torque (3,1) External torque ------- Outputs ------- xDot (7,1) Derivative of the state, x --------------------------------------------------------------------------
AerospaceUtils: Coord/QIToBDot SC: Dynamics/RBModel Common: Control/C2DZOH Math: Linear/Cross Math: Linear/SkewSymm
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