Initial Values Determination of Thrust Parameters for Continuously Low-Thrust Maneuvering Spacecraft

Continuous low thrust is widely used in orbit transfer maneuvers. If the unknown maneuvers are not correctly compensated, the orbiting accuracy will be seriously affected. We propose a rapid method for pre-identifying thrust acceleration based on single-arc orbit determination in order to determine...

Whakaahuatanga katoa

I tiakina i:
Ngā taipitopito rārangi puna kōrero
Ngā kaituhi matua: Wen Guo, Xuefeng Tao, Min Hu, Wen Xue
Hōputu: Tuhinga
Reo:Ingarihi
I whakaputaina: MDPI AG 2025-07-01
Rangatū:Applied Sciences
Ngā marau:
Urunga tuihono:https://www.mdpi.com/2076-3417/15/14/8064
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