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Modeling of Carrier-based Aircraft Ski Jump Take-off Based on Tensor 被引量:8

基于张量的舰载机滑跃式起飞动力学建模(英文)
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摘要 A general mathematical model of carrier-based aircraft ski jump take-off is derived based on tensor. The carrier, the aircraft body and the movable parts of the landing gears are treated as independent entities. These entities are assembled into a multi-rigid-body system with flexible links. Dynamical equations of each entity are derived on the basis of the Newton law and the Euler transformation. Using the invariance property of the tensor, the dynamical and kinematical equations are converted to tensor forms which are invariant under time-dependent coordinate transformations. Then the tensor-formed equations are expressed by the matrix operation. Differential equation group of the matrix form is formulated for the programming. The closure of the model is discussed, and the simulation results are given. A general mathematical model of carrier-based aircraft ski jump take-off is derived based on tensor. The carrier, the aircraft body and the movable parts of the landing gears are treated as independent entities. These entities are assembled into a multi-rigid-body system with flexible links. Dynamical equations of each entity are derived on the basis of the Newton law and the Euler transformation. Using the invariance property of the tensor, the dynamical and kinematical equations are converted to tensor forms which are invariant under time-dependent coordinate transformations. Then the tensor-formed equations are expressed by the matrix operation. Differential equation group of the matrix form is formulated for the programming. The closure of the model is discussed, and the simulation results are given.
出处 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2005年第4期326-335,共10页 中国航空学报(英文版)
基金 AeronauticsScienceFoundationofChina(02A51045)
关键词 mathematical model TENSOR carrier-based aircraft ski jump TAKE-OFF mathematical model tensor carrier-based aircraft ski jump take-off
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  • 1Hess R A. Investigating handling qualities using a structure model of human pilot[R]. AIAA 87-2537, 1987
  • 2Mark R A, David K S. Closed-loop pilot vehicle analysis of the approach and landing task[J]. Journal of Guidance , 1987, 10(2):187~194
  • 3Phillips J M, Anderson M R. A variable strategy pilot model[R].AIAA 2000-3983, 2000
  • 4Dang B V, Moing P C. Integration of flight and carrier landing aid systems for shipboard operation[R]. AD-A224. 869, 1991
  • 5Richards R, Chrenka J, Thordsen M. Artificial intelligence technique for pilot approach decision aid logic (PADAL) system [R].ADA388045-2001-3, 2001
  • 6Heffley R. Derivation of human pilot control laws based on literal interpretation of pilot training literature[R]. AIAA 81-18221981,1981
  • 7Anderson M R. Inner and outer loop manual control of carrier aircraft landing[R]. AIAA 96-3877, 1996

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