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- W4320037587 abstract "Because of the aerodynamic drag force, satellites formation with different area-mass-ratio will diverge during the life time in orbit. To maintain the configuration of the formation, this paper proposed a control strategy with high engineering practicability and fuel economy. By reversely calculating the rate of orbit decay from the time interval between formation maintenance control and the distance variation between satellites, the velocity increment of a unilateral limit cycle is decided without the estimation of the atmosphere density. Besides, the method adapted the uncertainty of the evolution of the atmosphere while the only-lifting control of the orbit will save the fuel of the satellite and reduce the frequency of the maintenance control. The simulation result demonstrates the validity of the method." @default.
- W4320037587 created "2023-02-12" @default.
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- W4320037587 date "2023-01-01" @default.
- W4320037587 modified "2023-10-18" @default.
- W4320037587 title "Study on the Formation Maintenance Control of the Satellites with Different Area-Mass-Ratio Considering Atmosphere Density Evolution" @default.
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- W4320037587 doi "https://doi.org/10.1007/978-981-19-6613-2_118" @default.
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