Volume 29 Issue 11
Nov.  2003
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Jia Yuhong, Liu Ying. Improvement of taxing performance for civil airliner by active control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(11): 1017-1021. (in Chinese)
Citation: Jia Yuhong, Liu Ying. Improvement of taxing performance for civil airliner by active control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(11): 1017-1021. (in Chinese)

Improvement of taxing performance for civil airliner by active control

  • Received Date: 01 Jul 2003
  • Publish Date: 30 Nov 2003
  • Based on two performance indexes of vertical acceleration and vertical displacement of body, by the non-linear model of self-tuning of landing gear and the ARAMX model of system, using the design of controller of the multi-step recursive predictor and the identification of the model parameters and system structure, the self-tuning control of landing gear was implemented. The simulation results show that the control scheme can effectively improve the performance of taxing for civil airliner.

     

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  • [1] 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 Jia Yuhong,He Qingzhi,Yang Guozhu.Taxing performance analysis of active control of landing gear[J].Acta Aeronautica et Astronautica Sinica,1999,20 (6):545~548(in Chinese) [2] 李清泉.自适应控制系统理论、设计与应用[M].北京:科学出版社,1990. 249~310 Li Qingquan.Theory,design and applications of adaptive control[M].Beijing:Science Press,1990.249~310(in Chinese) [3] John R M, Huey D C. A mathematical model of an active control landing gear for load control during impact and roll-out .NASA TND8080,1976 [4] 吴士昌,藏瀛芝. 自适应控制[M]. 北京:机械工业出版社,1989.135~173 Wu Shichang,Zang Yingzhi. Adaptive control[M]. Beijing:China Machine Press,1989.135~173(in Chinese) [5] 吴广玉.系统辨识与自适应控制[M].哈尔滨:哈尔滨工业大学出版社,1987.48~242 Wu Guangyu. System identification and adaptive control[M]. Harbin:The Press in Harbin Institute of Technology,1987.48~242(in Chinese)
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