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...

詳細記述

書誌詳細

出版年:	Applied Sciences
主要な著者:	Wen Guo, Xuefeng Tao, Min Hu, Wen Xue
フォーマット:	論文
言語:	英語
出版事項:	MDPI AG 2025-07-01
主題:	continuous low thrust tangential acceleration orbit determination radar observation
オンライン･アクセス:	https://www.mdpi.com/2076-3417/15/14/8064