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KIAM Preprint № 142, Moscow, 2019
Authors: Shestopyorov A.I., Tkachev S. S.
Linear quadratic control for spacecraft large-angle maneuvers
Abstract:
The inertial stabilization problem of a spacecraft moving in a geostationary orbit is considered. Linear quadratic control laws which realize large-angle maneuvers are obtained by means of corresponding selection of algebraic Riccati equation stabilizing solutions.
Keywords:
inertial stabilization, PD-regulator, linear quadratic control, algebraic Riccati equation
Publication language: russian,  страниц: 18
Research direction:
Theoretical and applied problems of mechanics
Russian source text:
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