Path: SC/Actuator
% Computes the moment arms for a set of thrusters. -------------------------------------------------------------------------- Form: m = MomArm( r, u, c ) -------------------------------------------------------------------------- ------ Inputs ------ r (3,:) Position vectors u (3,:) Unit vectors in the force direction c (3,1) Center-of-mass location ------- Outputs ------- m (3,:) Moment arms --------------------------------------------------------------------------
Math: Linear/Cross
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