Dynamics of the satellite angular momenta is modeled by ordinary differential equations with additive white noise. A feedback controller er is desired to maintain tolerable satellite momenta and to economize ze the fuel consumption. The stochastic optimal control problem is transformed into an equivalent deterministic optimization problem involving a parabolic partial differential equation. Necessary optimality y conditions are used to develop a computation algorithm. Results regarding optimal controls, expected costs, and confinement probabilities in different noisy environments are presented.
Optimal Precession Control of Randomly Perturbed Spin-Stabilized Satellite
IEEE Transactions on Aerospace and Electronic Systems ; AES-13 , 2 ; 172-178
1977-03-01
1728456 byte
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch