|
SUPPORT SITE |
|
|
|
SUPPORT SITE |
|
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
Back to the SC Module page