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基于虚拟惯性台的刹车系统仿真研究

Study on Brake Control System Test Method Based on Virtual Simulation Experiments
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摘要 针对传统的惯性台试验不具备带起落架刹车能力,无法开展多轮起落架系统刹车试验的不足,提出了一种能与试验室惯性台试验原理、方法相结合,又能克服传统的物理试验不足的虚拟惯性台试验方法。利用仿真软件建立了虚拟惯性台仿真试验模型,对模型进行了仿真分析,并与外场实测结果进行了对比。结果表明:仿真分析结果与实测结果较为接近,所建立的模型简易可行,可以方便开展带起落架的多轮起落架刹车系统虚拟试验。 With the lack of traditional virtual simulation experiments test don't have the capability with landing gear, which also can't be carried out several rounds of the landing gear brake system test, this paper proposes one test method which is combined with laboratory simulation experiments test principle and can overcome the traditional test method by the lack of physical test. Based on software MATLAB, the model of virtual simulation experiments are established and analyzed in the simulation. With the contrast of outfield test result, it shows that simulation analysis result is proximity to outfield test result. The model is simple and convenient to carry out brake system virtual test with multi-wheel landing gear.
出处 《航空制造技术》 2015年第S2期97-98,共2页 Aeronautical Manufacturing Technology
关键词 虚拟惯性台 刹车 虚拟试验 Virtual simulation experiments Brake Virtual test
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  • 1牟让科,胡孟权.飞机非对称着陆和滑跑载荷分析[J].机械科学与技术,2000,19(z1):72-74. 被引量:16
  • 2何恒,吴瑞祥,黄伟明.基于ANN与FNN的飞机防滑刹车系统设计[J].航空学报,2005,26(1):116-120. 被引量:8
  • 3田广来,谢利理,岳开宪,常顺宏.飞机防滑刹车系统的最佳滑移率式控制方法研究[J].航空学报,2005,26(4):461-464. 被引量:27
  • 4E Bakker, L Nyborg , H B Pacejka. Tyre Modelling for Use in Vehicle Dynamics Studies[R]. Society of Automotive Engineers Paper No. 870421, 1988.
  • 5Barnes A G, Yager T J. Simulation of aircraft behaviors and close to the ground[R]. AGARD-AG-285, 1985.
  • 6Barnes A G, Yager T J. Enhancement of aircraft ground handling simulation capability[R]. AGARD AG 333, 1998.
  • 7Kapseong R. A description modeling and simulation of aircraft runway dynamics[R]. AIAA 2003-1895, 2003.
  • 8Pi W S, Yamane J R, Smith M J C. Generic aircraft ground operation simulation[R]. AIAA 86-0989, 1986.
  • 9Goldthorpe S H,Kernik A C,Mcbee L S, et al. Ground and control requirement for high-speed rollout and turnoff (ROTO)[R]. NASACR 195026,1995.
  • 10Tanner J A, Stubbs S M. Behavior of aircraft antiskid braking systems on dry and wet runway surfaces: a slip-ratio-controlled system with ground speed reference from unbraked nose wheel[R]. NASA TN D-8455, 1977.

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