Orbit acquisition and trajectory rendezvous control of CBERS-1

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Orbit acquisition and trajectory rendezvous control of CBERS-1

Wang Xudong, / Li Xinfeng, / Xi Dunyi, / Ni Xingzhen, / Yang Jiachi, / Huang Fuming, / Yang Xiaoqin, / Tan Wei, / Zhang Rongzhi, / Li Jisheng,

Abstract

The CBERS-1 is the first Sun-synchronous orbit resource satellite cooperatively developed by China and Brazil. The CBERS-1 had been successfully launched into the designed orbit by the Chinese Long-March launch vehicle. It has been normally operated in the high-accuracy Sun-synchronous, recursive, frozen orbit designed for remote-sensing users through a series of orbit acquisition, sub-satellite-point trace acquisition and orbit maintenance manoeuvres. The paper briefly presents the mission objectives, system structure, orbit control strategy, control performance, flight software and on-orbit operations for the orbit control system of the CBERS-1, as well as its flight results.

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Document information

Title :

Orbit acquisition and trajectory rendezvous control of CBERS-1

Contributors:

Wang Xudong, (author) / Li Xinfeng, (author) / Xi Dunyi, (author) / Ni Xingzhen, (author) / Yang Jiachi, (author) / Huang Fuming, (author) / Yang Xiaoqin, (author) / Tan Wei, (author) / Zhang Rongzhi, (author) / Li Jisheng, (author)

Published in:

Proceedings of the 3rd World Congress on Intelligent Control and Automation (Cat. No.00EX393) ; 1 ; 477-480 vol.1

Publication date :

2000-01-01

Size :

271261 byte

ISBN :

0-7803-5995-X

DOI :

https://doi.org/10.1109/WCICA.2000.860012

Type of media :

Conference paper