中国空间站GNC系统设计与在轨验证  

Design and on-orbit verification of the guidance,navigation and control system of the China space station

作　　者：张军[1,2] 张志方[1,2] 刘成瑞[1,2] 张锦江[1] 冯帅[1] 林瀚峥[1,2] 李公军 刘文静[1,2] 张录晨[1] 蔡彪 ZHANG Jun;ZHANG ZhiFang;LIU ChengRui;ZHANG JinJiang;FENG Shuai;LIN HanZheng;LI GongJun;LIU WenJing;ZHANG LuChen;CAI Biao(Beijing Institute of Control Engineering,Beijing 100190,China;National Laboratory of Space Intelligent Control,Beijing 100190,China)

机构地区：[1]北京控制工程研究所,北京100190 [2]空间智能控制技术重点实验室,北京100190

出　　处：《中国科学：技术科学》2022年第9期1355-1374,共20页Scientia Sinica(Technologica)

摘　　要：空间站作为我国研制的最大规模航天器,是我国载人航天三步走战略的最后一步的建设目标.本文详细介绍了我国空间站组合体制导、导航与控制方案设计涉及的主要内容与关键技术,以及系统在轨验证情况.首先给出了GNC系统的任务要求;其次给出了系统的配置与飞行方案,并对系统的关键技术及地面设计过程进行了说明;最后对在轨飞行数据进行了分析,验证了系统设计的正确性,表明系统设计合理,可以满足空间站组合体控制的任务要求.As the largest spacecraft developed in China,the Chinese space station is the last step of the three-step strategy of the manned space project of China.This paper introduces in detail the main contents and key technologies involved in the design of the guidance,navigation,and control(GNC)system of the Chinese space station,as well as the on-orbit verification system.First,the mission requirements of the GNC system are listed.Second,the configuration and flight scheme of the system are stated,and the key technologies and ground test process are explained.Finally,the on-orbit flight data are analyzed to validate the system,demonstrating that its design can meet the mission requirements of the combination of space station.

关 键 词：空间站 组合体 制导、导航与控制 方案 在轨验证 

分 类 号：V476.1[航空宇航科学与技术—飞行器设计]