空间站舱内飞行器总体设计及试验方案研究  

Overall Design and Experimental Scheme of Inboard Nano Satellite of Space Station

作　　者：师帅 李九人 张海联 张高飞 曹永奎 SHI Shuai;LI Jiuren;ZHANG Hailian;ZHANG Gaofei;CAO Yongkui(Department of Precision Instrument,Tsinghua University,Beijing100084,China;China Astronaut Research and Training Center,Beijing 100094,China)

机构地区：[1]清华大学精密仪器系,北京100084 [2]中国航天员科研训练中心,北京100094

出　　处：《载人航天》2018年第2期163-170,共8页Manned Spaceflight

基　　金：载人航天预先研究项目(010701)

摘　　要：针对我国对能在空间站内部运动、完成飞行试验与在轨服务任务的舱内飞行器的研制需求,设计了一种舱内飞行器总体方案,提出了关键指标要求及子系统层级的舱内飞行器实现方案。在此基础上,对飞行器各系统包括结构、电源、综合电子、通信、GNC等进行了设计与校核。最后,对舱内飞行器的在轨算法试验和地面测试仿真方案进行了分析与设计。方案可行性通过舱内自主交会数值仿真得到了验证。Inboard Nano Satellite(INS)which operates inside Space Station serves as a favorable plat-form for flight test and on orbit servicing.Based on the analysis of the INS development requirements,the architecture,mission objectives and peif'ormance requirements,the overall scheme of INS were dis-cussed and the key indicators as well as the system design were proposed.On this basis,various systems including the structure,power,integrated electronic system,communication and GNC were designed and validated.Furthermore,the contents of the on-orbit algorithm test and ground simulation and experiments of the INS were analyzed and designed,and the INS autonomous rendezvous was simulated.

关 键 词：舱内飞行器 飞行器系统设计 在轨试验方案 自主交会 

分 类 号：V474.292[航空宇航科学与技术—飞行器设计]