航天器工程2025，Vol.34Issue(1)：87-94,8.DOI:10.3969/j.issn.1673-8748.2025.01.015
亚太6E卫星姿轨控系统关键技术设计与验证
Design and Verification of Key Technology for Attitude and Orbit Control System of APSTAR-6E Satellite
摘要
Abstract
The APSTAR-6E satellite is a broadband communication satellite in geostationary orbit and the first full electric propulsion satellite in China.It is equipped with two types of electric thrusters including Ion and Hallelectric thruster for orbit control.In response to the characteris-tics of orbit control using full electric propulsion,the control system has designed an orbit control strategyusing electric propulsion system to complete orbit transfer,fixed point capture and sta-tion-keeping in GEO.The Attitude and Orbit Control System(AOCS)product configuration,working mode and key technologies related to electric propulsion orbit control for APSTAR-6E satellite including autonomous flight design of AOCS,application technology of Thruster Point Assembly Mechanism(TPAM),electric propulsion orbit raising and electric propulsion station-keeping technologyare introduced in this paper,the implementation status of control system indi-cators is also providedbased on the data of satellite in orbit.关键词
亚太6E卫星/控制系统/电推进/自主控制Key words
APSTAR-6E satellite/Attitude and Orbit Control System(AOCS)/electric propul-sion/autonomous control分类
航空航天引用本文复制引用
李巍,马雪,刘蕊,王玉峰..亚太6E卫星姿轨控系统关键技术设计与验证[J].航天器工程,2025,34(1):87-94,8.
