The stability properties of a class of gyrostat systems with rotor spin rates regulated by feedback control are discussed. The concepts of proportional and rate feedback are generalized to the multiple rotor case, with the spin rate feedback gain matrix assumed to be positive definite, and that of position feedback positive semidefinite. In the past, gyrostat stability analyses have emphasized the idealized limiting case of inifinite feedback gains corresponding to a constant-speed rotor, or, in a few cases, studies of the idealized frictionless free-rotor case. The aim of this work is to study the relationship between stability results using these idealized models and the stability results obtained using the more realistic feedback controlled rotor model for the full range of feedback gains. The state space is divided into two subspaces, one of which is free of damping due to feedback (perhaps zero-dimensional), and this subspace exhibits certain appealing mathematical properties. It is shown that for the controlled systems to be asymptotically stable, a necessary and sufficient condition is that the corresponding restrained system be in the Lagrange region (stable according to Liapunov's direct method) and that the damping-free subspace be zero-dimensional (pervasive damping). Two sufficient conditions for instability are also proved. As a special case, the stability of gravity gradient gyrostat satellites with one symmetric rotor spinning around an axis fixed in the main rigid body are analyzed in detail, and numerical examples are given.
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