Volume 30 Issue 06
Jun.  2004
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He Heng, Wu Ruixiang. Improved BP neural network in design of aircraft antiskid braking system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(06): 561-564. (in Chinese)
Citation: He Heng, Wu Ruixiang. Improved BP neural network in design of aircraft antiskid braking system[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(06): 561-564. (in Chinese)

Improved BP neural network in design of aircraft antiskid braking system

  • Received Date: 22 Jan 2003
  • Publish Date: 30 Jun 2004
  • The construction of Sp (perfect slip ratio) identifier with back-propagation neural network was proposed to prevent skidding and have the best braking effect in the aircraft braking process. In order to improve the learning ability of the network, a type of self-adaptive learning rate method, second-order learning rate method, was introduced. Some problems in the practice of this method were discussed and the solutions were presented. A third-order learning rate method was deduced based on the method. The method of reasonable configuration of active functions was proposed. The combination of these methods renders better learning precision and speed.

     

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  • [1] 焦志强. 系缆气球气动力、动稳定性及大气扰动响应 . 北京:北京航空航天大学航空科学与工程学院,2003 Jiao Zhiqiang. Aerodynamic estimation stability and dynamics repouse for a tethered balloon .BeiJing:School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics,2003 [2] Jones S P,DeLaurier J D. Aerodynamic estimation techniques for aerostats and airships . AIAA-81-1339,1981 [3]Jones S P. Aerodynamics of a new aerostat design with inverted-y fins . AIAA 85-0867-CP, 1985
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