摘要
介绍了亚太6E卫星综合测试方案设计与实现,从系统级验证平台、数字仿真平台、正样卫星3个方面介绍了不同状态卫星综合测试目的、测试设计、实现及测试结果,可为卫星在轨稳定运行提供数据支持。文章介绍的测试方案对新卫星平台首颗卫星、全电推进卫星、全自主运行卫星综合测试具有借鉴意义。
The design and verification of the integrated test of the Apstar-6E satellite is introduced in this paper.The test purposes,test designs,test verification and test results of the satellite are introduced from three different aspects including system-level verification platform,digital simulation platform and flight-model satellite,which can provide data supports for the stable in-orbit operation.The test schemes introduced in this paper have reference significance for integrated tests of the satellite such as the first launch satellite of the new satellite platform,the all-electric propulsion satellite and the fully autonomous operation satellite.
作者
安秀枝
范振昊
熊晓将
安然
何艳
AN Xiuzhi;FAN Zhenhao;XIONG Xiaojiang;AN Ran;HE Yan(Institute of Telecommunication and Navigation Satellites,China Academy of Space Technology,Beijing 100094,China)
出处
《航天器工程》
北大核心
2025年第1期166-173,共8页
Spacecraft Engineering
关键词
亚太6E卫星
综合测试
新卫星平台
全电推进
全自主运行
APSTAR-6E satellite
integrated test
new satellite platform
all-electric propulsion
fully autonomous operation
