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非线性非定常气动力的模糊逻辑建模方法
引用本文:刘志涛,孙海生,姜裕标,江峰.非线性非定常气动力的模糊逻辑建模方法[J].实验流体力学,2005,19(1):99-103.
作者姓名:刘志涛  孙海生  姜裕标  江峰
作者单位:中国空气动力研究与发展中心,四川,绵阳,621000
摘    要:建立了非线性非定常气动力的模糊逻辑模型。利用大迎角俯仰及滚转振荡气动力验证了模型的有效性。结果表明:该模糊逻辑模型对非定常气动力有很好的预测能力;利用模糊逻辑方法可建立包括非基本运动状态变量在内的多变量非线性非定常气动力的数学模型。

关 键 词:非定常气动力  模糊逻辑  数学建模  非线性  参数辨识
文章编号:1672-9897(2005)01-0099-05

Fuzzy logic modeling of nonlinear unsteady aerodynamics
LIU Zhi-tao,SUN Hai-sheng,JIANG Yu-biao,JIANG Feng.Fuzzy logic modeling of nonlinear unsteady aerodynamics[J].Experiments and Measur in Fluid Mechanics,2005,19(1):99-103.
Authors:LIU Zhi-tao  SUN Hai-sheng  JIANG Yu-biao  JIANG Feng
Abstract:A fuzzy logic modeling of nonlinear unsteady aerodynamics is developed in this paper. Aerodynamic data for a model obtained in forced pitching and rolling oscillation at high angles of attack has been used to verify the modeling. The results show that it predicts the unsteady aerodynamics very well. This method can be used to develop models with multiple variables including non-basic flight variables.
Keywords:unsteady aerodynamics  fuzzy logic  modeling
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