电子与通信

临近空间飞行器信息系统一体化载荷平台

  • 阎啸 ,
  • 唐博 ,
  • 张天虹 ,
  • 秦开宇
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  • 电子科技大学 航空航天学院, 成都 611731
阎啸,男,博士,副教授,主要研究方向:电子测试与仪器。Tel.:028-61831506,E-mail:yanxiao@uestc.edu.cn;唐博,男,博士,工程师,主要研究方向:航空航天测控通信。Tel.:028-61831506,E-mail:tangbocd@126.com;张天虹,女,博士,主要研究方向:临近空间信号处理与建模。E-mail:tianhongzhang_uestc@outlook.com;秦开宇,男,博士,主要研究方向:飞行器测控通信与有效载荷技术。Tel.:028-61831870,E-mail:kyqin@uestc.edu.cn

收稿日期: 2016-04-20

  修回日期: 2016-05-27

  网络出版日期: 2016-06-20

基金资助

中央高校基本科研基金(ZYGX2015J121)

Payload platform of near space vehicle information system

  • YAN Xiao ,
  • TANG Bo ,
  • ZHANG Tianhong ,
  • QIN Kaiyu
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  • School of Aeronautics and Astronautics, University of Electronic and Technology of China, Chengdu 611731, China

Received date: 2016-04-20

  Revised date: 2016-05-27

  Online published: 2016-06-20

Supported by

the Foundamental Research Founds for the Central Universities (ZYGX2015J121)

摘要

介绍了临近空间日趋受到各国的关注和研究、临近空间的概念以及临近空间飞行器的概况。从高超声速临近空间飞行器设计层面分析了临近空间飞行器信息系统多任务需求和现有设计的矛盾,指出研究临近空间飞行器一体化综合电子系统信号交链和多任务一体化协同技术是解决此矛盾的有效途径。通过对临近空间飞行器信息系统一体化载荷平台的研究,构建了采用冗余备份技术的包括信号处理模块、控制模块的统一开放的柔性系统平台架构。

本文引用格式

阎啸 , 唐博 , 张天虹 , 秦开宇 . 临近空间飞行器信息系统一体化载荷平台[J]. 航空学报, 2016 , 37(S1) : 127 -133 . DOI: 10.7527/S1000-6893.2016.0181

Abstract

The paper indicates that the near space has attracted increasing attention from the governments and researchers. The second part briefly introduces the concept of near space and gives a concise overview of the near space vehicle. Contradiction between multitasking requirements and now available design of the near space vehicle information system is analyzed, pointing out that the integration of near space vehicle integrated electronic system signal chain and multitasking integration synergy technology is an effective way to solve this contradiction. The near space vehicle information system integration research using redundancy backup technology is presented, building a unified system platform architecture including signal processing module and control module.

参考文献

[1] 崔尔杰. 近空间飞行器研究发展现状及关键技术问题[J]. 力学进展, 2009, 39(6):658-673. CUI E J. Research statutes, development trends and key technical problems of near space flying vehicles[J]. Advances in Mechanics, 2009, 39(6):658-673(in Chinese).
[2] CROW R P. Combined ground and satellite system for global aircraft surveillance guidance and navigation:U.S. patent 5627546[P]. 1997-5-6.
[3] KIM D, PARK B, LEE S, et al. Design of efficient navigation message format for UAV pseudolite navigation system[J]. IEEE Transactions on Aerospace and Electronic Systems, 2008, 44(4):1342-1355.
[4] 王艳奎. 临近空间飞行器应用前景及发展分析[J]. 国防科技, 2009, 30(2):20-24. WANG Y K. An analysis on application prospects and development of near-space vehiclos[J]. National Defense Sciense & Technology, 2009,30(2):20-24.
[5] HANK J M, MURPHY J S, MUTZMAN R C. The X-51A scramjet engine flight demonstration program[C]//AIAA International Space Planes and Hypersonic Systms and Technolgies Conference. Reston:AIAA, 2008.
[6] LANE J. Design processes and criteria for the X-51A flight vehicle airframe[R]. Chicago:BOeing Co Huntington Beach Ca Integrated Defense Systems, 2007.
[7] BROCH J, MALTZ D A, JOHNSON D B, et al. A performance comparison of multi-hop wireless ad hoc network routing protocols[C]//Proceedings of the 4th Annual ACM/IEEE International Conference on Mobile Computing and Networking Piscataway, NJ:IEEE Press, 1998:85-97.
[8] BORG M P, SCHNEIDER S P. Effect of freestream noise on roughness-induced transition for the X-51A forebody[J]. Journal of Spacecraft and Rockets, 2008, 45(6):1106-1116.
[9] ZHANG K, ZHANG W, ZENG J Z. Preliminary study of routing and date integrity in mobile Ad hoc UAV network[C]//2008 International Conference on Apperceiving Computing and Intelligence Analysis. Piscataway, NJ:IEEE Press, 2008:347-350.
[10] XIAO Z X, ZHANG M H, XIAO L H. Studies of roughness-induced transition using three-equation k-ω-γ transition/turbulence model[C]//AIAA International Space Planes and Hypersonic Systms and Technolgies Conference. Reston:AIAA, 2013.
[11] Office of the Secretary of Defense. Unmanned aircraft systems road-map2005- 2030[M]. Washington, D.C.:Office of the Secretary of Defense, 2005:32-36.
[12] 沈振, 张庆振, 高勇, 等. 高动态无人飞行器再入段GNC系统关键技术研究[J]. 系统仿真学报, 2008(S1):518-521. SHEN Z, ZHANG Q Z, GAO Y, et al. Research on key techniques for guidance navigation and control sytems of high-dyanamic unmanned vehicle during reentry phase[J]. Journal of System Simulation, 2008(S1):518-521 (in Chinese).
[13] 尹志忠, 李强. 近空间飞行器及其军事应用分析[J]. 装备指挥技术学院学报, 2006, 17(5):64-68. YIN Z Z, LI Q. Analysis of near space vehicle and its military application[J]. Journal of the Academy of Equipment Command & T echnology, 2006,17(5):64-68 (in Chinese).
[14] DUBOIS-MATRA O, BISHOP R H. Tracking and identification of a maneuvering reentry vehicle[J]. Journal of Guidance, Control, and Dynamics, 2003, 17(5):1124-1130.
[15] BOWCUTT K, SMITH T, KOTHARI A, et al. The Hypersonic Space and Global Transportation System:A Concept for Routine and Affordable Access to Space[C]//17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Reston:AIAA, 2011, 6:68.
[16] WHITMORE S A, DUNBAR B J. Orbital space plane, past, present, and future[C]//AIAA International Air and Space Symposium and Exposition:The Next. Reston:AIAA, 2003:14-17.
[17] 黄伟, 罗世彬, 王振国. 临近空间高超声速飞行器关键技术及展望[J]. 宇航学报, 2010, 31(5):1259-1265. HUANG W, LUO S B, WANG Z G. Key techniques and prospect of near-space hypersonic vehicle[J]. Journal of Astronautics, 2010, 31(5):1259-1265(in Chinese).
[18] ANILKUMAR A K, ANANTHASAYANAM M R, SUBBA RAO P V. Prediction of Re-entry of Space Debris Objects:Constant Gain Kalman Filter Approach[C]//Proceedings of AIAA AFM Conference. Reston:AIAA, 2003.
[19] GUPTA K K, CHOI S B, IBRAHIM A. Development of aerothermoelastic acoustics simulation capability of flight vehicles[C]//48th AIAA Aerospace Sciences Meeting. Reston:AIAA, 2010:4-7.

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