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- W3166174920 abstract "Intheobservationslewingoflongbaselineinterferometersformedbymultiplefree-e yingspacecraftinformation, it is required to rotate the entire formation about a given axis and to synchronize individual spacecraft rotation with formation rotation. Using a particle model for spacecraft formation dynamics and a rigid-body model for spacecraft attitude dynamics, control laws are derived for this mode of operation in the absence of a gravitational e eld and disturbances. A simplie ed control law suitablefor implementation isalso obtained. It is shown thatunder mild conditionstheformation alignmenterrordecaystozeroexponentiallywith time. Computersimulationstudies are made for a free-e ying spacecraft triad in a triangular formation. The results show that the developed control laws are effective in synchronized formation rotation." @default.
- W3166174920 created "2021-06-22" @default.
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- W3166174920 date "1997-08-11" @default.
- W3166174920 modified "2023-10-17" @default.
- W3166174920 title "Synchronized formation rotation and attitude control of multiple free-flying spacecraft" @default.
- W3166174920 cites W2201949337 @default.
- W3166174920 doi "https://doi.org/10.2514/6.1997-3753" @default.
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