期刊文献+

起落架摆振控制及试验研究综述 被引量:11

Review of Landing Gear Shimmy Control and Tests
在线阅读 下载PDF
导出
摘要 从摆振控制和摆振试验两个方面回顾起落架摆振研究中的问题。列举起落架摆振控制研究中采用的控制算法,给出各种控制算法的效果和局限性。分析了各种起落架摆振试验,介绍了摆振试验所获得的有益结果。指出摆振控制相关试验研究不足和摆振试验耗费高的特点,提出了今后起落架摆振现象研究的方向。 Landing gear shimmy problem is divided into two aspects: shimmy control and shimmy test.The shimmy control algorithms are listed and corresponding effects and limitations are discussed.Various shimmy tests are investigated and valuable results through shimmy test are given.It is pointed out that there is a lack of test about shimmy control and the shimmy test is costly.The development trend about landing gear shimmy is provided.
出处 《飞机设计》 2011年第2期38-41,共4页 Aircraft Design
基金 航空科学基金资助项目(04B52012)
关键词 摆振 起落架 控制 试验 shimmy landing gear control test
  • 相关文献

参考文献18

  • 1Crede C E. Feasibility study of an active vibration isolator for a helicopter rotor[R]. Virginia: DTIC, WADC. 1958.
  • 2Dewispelare A R, Stager R P. Investigation of landing gear alternatives for high performance aircraft [J]. Journal of Aircraft. 1983, 20(4):319-326.
  • 3贾玉红,何庆芝,杨国柱.主动控制起落架滑行性能分析[J].航空学报,1999,20(6):545-548. 被引量:18
  • 4刘晖,顾宏斌,吴东苏.半主动控制起落架缓冲性能初步研究[J].航空学报,2006,27(5):864-868. 被引量:22
  • 5Bandaru S, Maiti D K. Lateral stability of a typical nose landing gear using torsional magneto-rheological (MR) damper[C]. Proceedings of Annual IEEE India Conference, India: INDICON, 2008:553-558.
  • 6Li G X. Modelling and analysis of a dual-wheel nosegear:shimmy instability and impact motions[C]. Proceedings of Aerospace Atlantic Conference, Ohio: SAE, 1993:129-143.
  • 7Pouly G, Huynh T H , Lauffenbruger J P, et al. Indirect fuzzy adaptive control for active shimmy damping [C]. Proceedings of the International Federation of Automatic Control, Seoul: IFAC, 2008: 15052-15057.
  • 8Huynh T H, Pouly G, Lauffenbruger J P, et al. Active shimmy damping using direct adaptive fuzzy control [C]. Proceedings of the International Federation of Automatic Control, Seoul: IFAC, 2008: 15058-15063.
  • 9Fallah M S, Long S H, Xie W F, et al. Robust model predictive control of shimmy vibration in aircraft landing gears [J]. Journal of Aircraft, 2008, 45 (6) : 1872-1880.
  • 10Gerhard S. Shimmy analysis of a simple aircraft nose landing gear model using different mathematical methods[J]. Aerospace Science and Technology, 1997, 8 (1) : 545-555.

二级参考文献11

  • 1高泽迥.半准备机场及双气室减震器设计[J].航空学报,1987,8(12):585-593.
  • 2张淑兰,飞机设计,1989年,3期,41页
  • 3高泽迥,航空学报,1987年,8卷,12期,585页
  • 4刘锐琛 苏开鑫 邰永起.飞机起落架强度设计指南[M].成都:四川科学技术出版社,1989..
  • 5Krüger W.Integrated design process for the development of semi-active landing gears for transport aircraft[D].University Stuttgart,2000.
  • 6Ghiringhelli G L.Testing of semi-active landing gear control for a general aviation aircraft[J].Journal of Aircraft,2000,37(4):606-615.
  • 7Lichtarowizc A,Duggins R K,Markland E.Discharge coefficients for incompressible non-cavitating flow through long orifices[J].Journal of Mechanical Engineering Scien-ce,1965,7(2):210-219.
  • 8Currey N S.起落架设计手册[M].北京:航空工业部,1982.
  • 9高泽迥.飞机设计手册,起飞着陆系统设计(14分册)[M].北京:航空工业出版社,2002.
  • 10顾宏斌,丁运亮,吴云生,万吉生,周可斌,哈晓春.油液压缩性对减摆器工作特性的影响[J].南京航空航天大学学报,1999,31(6):628-633. 被引量:17

共引文献35

同被引文献73

引证文献11

二级引证文献27

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部