运载火箭快速测试发射关键技术
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摘要
介绍了运载火箭领域快速测试发射技术的发展历程,同时梳理美国、日本快速响应运载火箭在快速测试发射技术上所取得的最新进展.针对国外运载火箭的研制情况,对电气系统智能化机内测试技术、先进地面测发控技术、智能化故障诊断技术、并行测试技术等快速测试发射技术进行分析,研究了其技术优势及需解决的关键技术难题,为未来我国运载火箭技术发展提供参考.
The developing course of the rapid test technology of launch vehicle was introduced,and reviewed the latest progress in the United States and Japan.According to the development situation of rapid test technology in foreign countries,measuring and testing technology of electrical intelligent machine,advanced test launch control technology,intelligent fault diagnosis technology,parallel test technology,and other rapid test launch technology were analyzed.On the basis of the analysis,technical advantages and key technical problems were introduced,which were providing reference for the future development of the China's launch vehicle technology.
The developing course of the rapid test technology of launch vehicle was introduced,and reviewed the latest progress in the United States and Japan.According to the development situation of rapid test technology in foreign countries,measuring and testing technology of electrical intelligent machine,advanced test launch control technology,intelligent fault diagnosis technology,parallel test technology,and other rapid test launch technology were analyzed.On the basis of the analysis,technical advantages and key technical problems were introduced,which were providing reference for the future development of the China's launch vehicle technology.
引文
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[2]秦旭东,容易,王小军,等.基于划代研究的中国运载火箭未来发展趋势分析[J].导弹与航天运载技术,2014(1):1-4.Qin Xudong,Rong Yi,Wang Xiaojun,et al.Development tendency analysis based on the research of Chinese launch vehicles generation[J].Missiles and Space Vehicles,2014(1):1-4.(in Chinese)
[3]李明泽,陈景鹏,白国玉,等.航天快速发射需求研究[J].现代电子技术,2014,37(19):125-127.Li Mingze,Chen Jingpeng,Bai Guoyu,et al.Study on damand of space rapid launch[J].Modern Electronics Technique,2014,37(19):125-127.(in Chinese)
[4]Pendleton R.Rapidly deployable space capabilities based assessment-approach and status[C].7th Responsive Space Conference,Los Angeles:2009.
[5]陈杰.美国快速空间响应运载器发展研究[J].中国航天,2007(8):33-37.Chen Jie.Research on operationally responsiveness space of America[J].Aerospace China,2007(8):33-37.(in Chinese)
[6]宋征宇.新一代运载火箭电气系统体系架构的研究[J].载人航天,2016,22(3):317-322.Song Zhengyu.Research on avionics system configuration of next generation launch vehicle[J].Manned Spaceflight,2016,22(3):317-322.(in Chinese)
[7]范崇盛,李桂芳,马晓风.基于智能BIT的运载火箭电气系统设计[C].航天科技集团公司运载器总体技术学术研讨会.北京:2016,6:523-530.
[8]刘少伟,郑文荣.BIT技术发展与应用研究[J].国外电子测量技术,2011,30(5):23-25.Liu Shaowei,Zheng Wenrong.Study on the development and application of BIT technology[J].Foreign Electronic Measurement Technology,2011,30(5):23-25.(in Chinese)
[9]权赫,张鹏,屈晨.运载火箭电气系统BIT设计流程及方法研究[J].电子测量技术,2016,39(1):61-64.Quan He,Zhang Peng,Qu Chen.Design process and method research of BIT for Launch vehicle electrical system[J].Electronic Measurement Technology,2016,39(1):61-64.(in Chinese)
[10]田心宇,张小林,吴海涛,等.机载计算机BIT虚警及解决策略研究[J].西北工业大学学报.2011,29(3):400-404.Tian Xinyu,Zhang Xiaolin,Wu Haitao,et al.A study of built-in test false alarm in an airborne computer[J].Journal of Northwestern Polytechnical University,2011,29(3):400-404.(in Chinese)
[11]宋征宇.新一代航天运输系统测发控技术发展的方向[J].航天控制,2013,31(4):3-9.Song Zhengyu.The development trend of test and launch control technology on future space transportation system[J].Aerospace Control,2013,31(4):3-9.(in Chinese)
[12]张磊.载人航天运载火箭地面测试发射控制系统[J].导弹与航天运载技术,2004(1):34-37.Zhang Lei.Ground test launch control system of LM-2Flaunch vehicle[J].Missiles and Space Vehicles,2004(1):34-37.(in Chinese)
[13]辛朝军,蔡远文,王韬,等.日本Epsilon火箭发射成功的分析及启示[J].装备学院学报,2014,25(3):67-71.Xin Chaojun,Cai Yuanwen,Wang Tao,et al.Analysis and enlightenments of the success on Japan’s epsilon rocket[J].Journal of Equipment Academy,2014,25(3):67-71.(in Chinese)
[14]张晨光,杨华,杨军.运载火箭新型地面测试发控系统构想[J].宇航学报,2005,26(3):249-252.Zhang Chenguang,Yang Hua,Yang Jun.Conception of a new model of launch vehicle ground test launch control system[J].Journal of Astronautics,2005,26(3):249-252.(in Chinese)
[15]尹茂君.运载火箭故障诊断系统研究与实现[D].成都:电子科技大学,2011.
[16]张素明,安雪岩,颜廷贵,等.大型运载火箭的健康管理技术应用分析与探讨[J].导弹与航天运载技术,2013(6):33-38.Zhang Suming,An Xueyan,Yan Tinggui,et al.Analysis and discussion of health management technology for large launch vehicle[J].Missiles and Space Vehicles,2013(6):33-38.(in Chinese)
[17]Johnson S B,Gormley T J,Kessler S S.System health management:with aerospace applications[M].Chichester,West Sussex:John Wiley&Sons Ltd,2011.
[18]宋征宇.运载火箭远程故障诊断技术综述[J].宇航学报,2016,37(2):135-144.Song Zhengyu.The survey of launch vehicle long distance fault diagnosis technique[J].Journal of Astronautics,2016,37(2):135-144.(in Chinese)
[19]肖明清,朱小平,夏锐.并行测试技术综述[J].空军工程大学学报(自然科学版),2005,6(3):22-25.Xiao Mingqing,Zhu Xiaoping,Xia Rui.Summary of parrallel test technology[J].Journal of Air Force Engineering University(Natural Science Edition),2005,6(3):22-25.(in Chinese)
[20]刘琪,孟庆虎,张从霞.并行测试技术及在空空导弹检测中的应用浅析[J].计测技术,2010,30(1):8-10.Liu Qi,Meng Qinghu,Zhang Congxia.Analysis and application of parallel test in airborne missile test equipments[J].Metrology&Measurement Technology,2010,30(1):8-10.(in Chinese)