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Application of the dynamic programming method to ensure of dual-channel attitude control of an asymmetric spacecraft in a rarefied atmosphere of Mars

Bakry, Ibrahim; Lyubimov, Vladislav Vasilyevich

We consider a linearized dynamic system, which determines the motion of the spacecraft relative to the center of mass in a rarefied atmosphere of Mars in the non-resonant case. This dynamic system takes into account the influence of disturbances from small aerodynamic and inertial asymmetry. The aim of this paper is to synthesis approximate optimi…