现役运载火箭控制系统闭环测试研究  

Closed-Loop Test for the Control System of Launch Vehicles in Service

作　　者：杜建峰 石志华 马晓峰 张桃源 张鲲鹏 梁玉琴 姚春燕 DU Jianfeng;SHI Zhihua;MA Xiaofeng;ZHANG Taoyuan;ZHANG Kunpeng;LIANG Yuqin;YAO Chunyan(Shanghai Aerospace Control Technology Institute,Shanghai 201109,China)

机构地区：[1]上海航天控制技术研究所,上海201109

出　　处：《上海航天（中英文）》2020年第S02期144-148,共5页Aerospace Shanghai（Chinese&English）

摘　　要：为了提高运载火箭控制系统在综合试验和集成试验中测试覆盖性和测试有效性,在现有测试方案的基础上,针对箭上产品不同的状态设计了3种控制系统总检查闭环测试方案。对3种方案开展了影响域分析,提出了一种适合运载火箭控制系统闭环测试的方案。In order to improve the coverage and effectiveness of the launch vehicle control system in comprehensive tests and integration tests,three kinds of general inspection closed-loop test schemes for the control system are designed based on existing test schemes according to the different states of products on rocket. An influence domain analysis of the three schemes is carried out,and a scheme suitable for the closed-loop test of the launch vehicle control system is proposed.

关 键 词：运载火箭 控制系统 闭环测试 地面测试 

分 类 号：V249.332[航空宇航科学与技术—飞行器设计]