Gibbs vector kinematics and inverse dynamics for decoupled spacecraft attitude maneuversBy 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.
Document ID
19860035033
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dwyer, T. A. W., III (Illinois, University Urbana, United States)