神舟七号飞船伴随卫星轨道控制及在轨飞行结果  

Orbit Control and Flight Results of ShenzhouⅦCompanion Microsatellite

作　　者：余勇[1] 张锐[1] 陈宏宇[1] 朱振才[1] 左霖[1] 赵灵峰[1] 吴会英[1] 

机构地区：[1]上海微小卫星工程中心

出　　处：《载人航天》2010年第4期14-18,共5页Manned Spaceflight

摘　　要：阐述神舟七号飞船伴随卫星轨道接近及绕飞试验阶段(从与飞船分离到形成绕飞轨道)的高可靠、高精度轨道控制方案,介绍试验任务目标、轨道控制策略、轨道控制系统、轨控参数计算、星上自主轨控管理系统设计,通过在轨飞行试验验证轨道控制考察和系统设计的正确性。A highly reliable and accurate orbit control system design scheme is presented for the proximity operations and companion flying orbit maneuvers of BX-1 micro-sat during its Shenzhou VII flight mission. The paper presents the flight mission object, orbit control strategies, control system structure, control parameter optimization, on-board autonomous maneuver control procedures. The orbit control concept and system design have been demonstrated by on-board flight test.

关 键 词：伴随卫星 非合作目标 轨道控制 在轨飞行结果 

分 类 号：V448.2[航空宇航科学与技术—飞行器设计]