Advanced Search
Volume 42 Issue 3
Mar.  2016
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2016  >  42(3): 426-434.
MAO Xiaodong, LIN Guiping, YU Jiaet al. Design of control law for ejection seat under adverse attitudes[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(3): 426-434. doi: 10.13700/j.bh.1001-5965.2015.0188(in Chinese)
Citation: MAO Xiaodong, LIN Guiping, YU Jiaet al. Design of control law for ejection seat under adverse attitudes[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(3): 426-434. doi: 10.13700/j.bh.1001-5965.2015.0188(in Chinese)
shu

Design of control law for ejection seat under adverse attitudes

doi: 10.13700/j.bh.1001-5965.2015.0188
  • 1.

    College of Aerospace Engineering, Shenyang Aerospace University, Shenyang 110136, China

  • 2. School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 31 Mar 2015
  • Publish Date: 20 Mar 2016
    Abstract
  • The escape performance of ejection seat under adverse attitudes is the key technology for the 4th generation ejection seat, and the design of control law algorithm is the core problem for attitude and trajectory adjustment. A new control law design method was presented. Firstly, a simulation model for the entire ejecting process was established and a control parameter optimization model was designed, through which an optimum parameter set was obtained as the discrete control law. Then, by utilizing multi-layer feedback of the error back propagation (BP) algorithm based neural network model, the ultimate continuous control law can be acquired under the whole ejecting conditions. The roll attitude ejecting condition was exampled to design and validate the approached method. The results indicate that the performance of ejection seat by adopting the control law designed by the proposed method is higher than the multi-mode control law and the K36Л-3.5 ejection seat, which also satisfies the performance demand of GJB under most conditions. Consequently, the design method is simple and clear, and the final algorithm is close to the theoretical optimum result. Therefore, it is proved to be a useful method for the design of the 4th generation ejection seat control law.

     

    • FullText(HTML)
  • loading
    • References(24)
  • [1]
    徐世坤. 弹射救生程序控制的发展[J].航空科学技术,1994(4):14-17. XU S K.The development of control law for escape system[J].Aeronautical Science and Technology,1994(4):14-17(in Chinese).
    [2]
    周方. 提高低空不利姿态下救生成功率的措施[J].航空科学技术,1998(6):18-20. ZHOU F.Measures to improve the successfulness of ejection-escaping in the low altitude positions[J].Aeronautical Science and Technology,1998(6):18-20(in Chinese).
    [3]
    ROSS D A, CULHANE D,FERRELL S.Digital recovery sequencer-ACES ejection seats[C]//Proceedings of the 42nd Annual SAFE Symposium.Creswell,OR:SAFE,2004:305-312.
    [4]
    CALKINS R B. ACES II ejection seat improvements[C]//Proceedings of the 34th Annual SAFE Symposium.Creswell,OR:SAFE,1996:86-91.
    [5]
    MILLER B A. NACES-The program and the seat[C]//Proceedings of the 24th Annual SAFE Symposium.Creswell,OR:SAFE,1987:134-139.
    [6]
    D'AULERIO L O U, YOST P.Navy aircrew common ejection seat(NACES)program summary[J].SAFE Journal,1991,21:25-29.
    [7]
    李锐. K36Л-3.5弹射座椅工作模式的探索[J].中航救生,2004,26(3):1-6. LI R.Exploration of K36Л-3.5 ejection seat operation mode[J].China Aeronautical and Astronautical Life-Support,2004,26(3):1-6(in Chinese).
    [8]
    MCCAULEY D, SUMMER M H,WOOD D,et al.Future advanced sequencer technology(FAST)[C]//Proceedings of the 39th Annual SAFE Symposium.Creswell,OR:SAFE,2001:95-110.
    [9]
    李锐. 第四代弹射座椅的关键技术[J].航空科学技术,1995(4):14-17. LI R.The crucial technology of the 4th generation ejection seat[J].Aeronautical Science and Technology,1995(4):14-17(in Chinese).
    [10]
    SWANSON D E, HERNDON G F.CREST system design[C]//Proceedings of the 24th Annual SAFE Symposium.Creswell,OR:SAFE,1987:27-31.
    [11]
    WHEELER C M, NIEDZIELSKI P,BARNETTE B,et al.Fourth generation escape system technology demonstration pintle nozzle controllable propulsion system[C]//Proceedings of the 36th Annual SAFE Symposium.Creswell,OR:SAFE,1998:133-141.
    [12]
    CARLSON R, LUCAS C,TAM B.Multi-axis pintle attitude control(MAXPAC)device for ACES II seat stabilization[C]//Proceedings of the 33rd Annual SAFE Symposium.Creswell,OR:SAFE,1995:225-232.
    [13]
    EVERS S. Russian ejection seat may fly in U.S.JAST[J].Aviation Week and Space Technology,1995,143(8):64-65.
    [14]
    李锐. K36Л-3.5弹射座椅性能分析[J].中航救生,2005,28(1):1-6. LI R.Performance analysis of K36Л-3.5 ejection seats[J].China Aeronautical and Astronautical Life-Support,2005,28(1):1-6(in Chinese).
    [15]
    封文春,林贵平. 弹射座椅多参数多模态控制仿真分析[J].系统仿真学报,2007,19(10):2283-2292. FENG W C,LIN G P.Multi-parameter and multi-mode control simulation analyses of ejection seat[J].Journal of System Simulation,2007,19(10):2283-2292(in Chinese).
    [16]
    封文春. 弹射座椅多参数多模态控制规律设计与仿真[D].北京:北京航空航天大学,2006:90-113. FENG W C.The multi-parameter and multi-mode control law design and simulation of ejection seat[D].Beijing:Beihang University, 2006:90-113(in Chinese).
    [17]
    张汉镔. 飞行器安全救生[M].北京:北京航空航天大学出版社,1990:104-120. ZHANG H B.Aircraft escape system[M].Beijing:Beihang University Press,1990:104-120(in Chinese).
    [18]
    郁嘉,毛晓东, 林贵平,等.风对弹射座椅救生性能的影响[J].航空学报,2013,34(4):727-740. YU J,MAO X D,LIN G P,et al.Impact of wind on ejection seat escape performance[J].Acta Aeronautica et Astronautica Sinica,2013,34(4):727-740(in Chinese).
    [19]
    郁嘉,林贵平, 毛晓东.弹射救生数值仿真及不利姿态下救生性能分析[J].航空学报,2010,31(10):1927-1932. YU J,LIN G P,MAO X D.Numerical simulation of ejection seat and analysis of performance under adverse attitudes[J].Acta Aeronautica et Astronautica Sinica,2010,31(10):1927-1932(in Chinese).
    [20]
    郁嘉,林贵平, 吴铭.弹射座椅减速性能的数值仿真计算[J].航空学报,2006,27(6):1033-1038. YU J,LIN G P,WU M.Numerical simulation of deceleration performance for ejection seat[J].Acta Aeronautica et Astronautica Sinica,2006,27(6):1033-1038(in Chinese).
    [21]
    周开利,康耀红. 神经网络模型及其MATLAB仿真程序设计[M].北京:清华大学出版社,2005:121-148. ZHOU K L,KANG Y H.Neural network model and MATLAB simulating program design[M].Beijing:Tsinghua University Press,2005:121-148(in Chinese).
    [22]
    毛晓东,郁嘉, 林贵平.过载与弹射速度关系研究及神经网络实现[J].航空学报,2010,31(10):1907-1913. MAO X D,YU J,LIN G P.Study of relationship between load factor and ejection velocity and its neural network implementation[J].Acta Aeronautica et Astronautica Sinica,2010,31(10):1907-1913(in Chinese).
    [23]
    MAO X D, YU J,LIN G P.Predicting ejection velocity of ejection seat via back propagation neural network[J].Journal of Aircraft,2011,48(2):668-672.
    [24]
    中华人民共和国国防科学技术工业委员会. 弹射座椅型乘员应急离机救生系统通用规范:GJB-1800A-2007[S].北京:中国航空工业集团公司, 2007. The Commission of Science,Technology and Industry for National Defense of the PRC.General specification for ejection seat type of aircrew emergency escape system:GJB-1800A-2007[S].Beijing:Aviation Industry Corporation of China,2007(in Chinese).
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(931) PDF downloads(6) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return