By use of Gibbs vectors as kinematic variables, multi-axial spacecraft equations of rotational motion are shown to be globally and rationally feedback-equivalent to a set of unconstrained and decoupled harmonic oscillators, driven by generalized acceleration commands. Advantages over alternative formulations with Euler angles and quaternions are pointed out.
Gibbs vector kinematics and inverse dynamics for decoupled spacecraft attitude maneuvers
1986-01-01
Conference paper
No indication
English
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