亚太6E卫星综合测试方案设计与验证  

Integrated Test Scheme Design and Verification of APSTAR-6E Satellite

作　　者：安秀枝 范振昊[1] 熊晓将[1] 安然[1] 何艳[1] AN Xiuzhi;FAN Zhenhao;XIONG Xiaojiang;AN Ran;HE Yan(Institute of Telecommunication and Navigation Satellites,China Academy of Space Technology,Beijing 100094,China)

机构地区：[1]中国空间技术研究院通信与导航卫星总体部,北京100094

出　　处：《航天器工程》2025年第1期166-173,共8页Spacecraft Engineering

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.

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 

分 类 号：V416[航空宇航科学与技术—航空宇航推进理论与工程]