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Dynamics of Spacecraft Guidance and Spin-up of the Gyrodine’s Rotors at Pulse-width Control

Sergey Somov
Attitude motion of a flexible spacecraft at pulse-width control by the jet engines’ thrust in process of a spatial attitude guidance and on-next spin-up rotors of six gyrodines, is considered. Results on the analysis of the spacecraft guidance, nutation and flexible oscillations are represented. Guidelines according to the logic in sequence of the gyrodine’s rotors spin-up for reduction of the nutation oscillations’ influence, are presented.
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