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快速机动测发控技术在智慧火箭中的应用
引用本文:徐昕,徐玮,于大海,潘东梅,张新伟.快速机动测发控技术在智慧火箭中的应用[J].南京航空航天大学学报,2018,50(S1):6-11.
作者姓名:徐昕  徐玮  于大海  潘东梅  张新伟
作者单位:上海航天电子技术研究所, 上海, 201109
摘    要:智能测试发射技术是智慧火箭概念的关键环节,快速机动是实现智能测试发射的重要发展方向。针对我国运载火箭测发周期较长、地面测试设备复杂、缺乏机动发射能力的情况,CZ-6运载火箭测发控系统以可靠、简易、快速、集成为主要特征。通过采用"总线为主、无线为辅、有线配合"的综合测试模式,结合军用方舱结构形式、高集成度测发设备、大流量数据传输与实时判读等关键技术,配合火箭总体实现了CZ-6运载火箭7 d快速简易测发的目标,为未来智慧火箭的智能测试发射打下了技术基础。

关 键 词:快速机动  测发控系统  BIT  方舱
收稿时间:2018/3/23 0:00:00
修稿时间:2018/5/30 0:00:00

Application of Fast Maneuver Test Launch Control Technology in Intelligent Launch Vehicle
XU Xin,XU Wei,YU Dahai,PAN Dongmei,ZHANG Xinwei.Application of Fast Maneuver Test Launch Control Technology in Intelligent Launch Vehicle[J].Journal of Nanjing University of Aeronautics & Astronautics,2018,50(S1):6-11.
Authors:XU Xin  XU Wei  YU Dahai  PAN Dongmei  ZHANG Xinwei
Institution:Shanghai Aerospace Electronic Technology Institute, Shanghai, 201109, China
Abstract:Intelligent test and launch technology is the key link of the concept of intelligent launch vehicle. Fast maneuver is an important development direction for intelligent test and launch technology. Aiming at situations of the long test and launch period, the complex ground test equipment, and the lack of maneuverability for the launch vehicle in China, the test launch control system of CZ-6 launch vehicle should have the main features of the reliability, simplicity, fast and integration. By using the method of "gave priority of the digital bus, assisted by the telemetry, cooperated with wired test", combined with the key technologies of shelter structure, high integration equipment, large flow data transmission and real time interpretation, the goal of the 7 d rapid launch is achieved, which provide a technical foundation for the intelligent test and launch technology of intelligent launch vehicle in future.
Keywords:fast maneuver  test launch control system  build-in test(BIT)  shelters
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