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直升机神经网络反馈线化飞行控制
引用本文:黄文明,徐锦法,高正.直升机神经网络反馈线化飞行控制[J].南京航空航天大学学报,2001,33(4):351-354.
作者姓名:黄文明  徐锦法  高正
作者单位:南京航空航天大学直升机旋翼动力学重点实验室
基金项目:航空基础科学基金 (编号 :H990 1 -1 0 1 ),国防科技重点实验室基金 (编号 :99JS5 2 .3.2 HK5 2 0 2 )资助项目
摘    要:以SH-2G为控制对象,采用基于神经网络的非线性系统反馈性化控制方法,进行直升机机动飞行仿真,仿真结果表明,所设计的神经网络具有逢适应能力,能够在线补偿反馈线性化所产生的逆变换误差,这种方法无须获得动态逆模型,而只需某一个状态下的动力学模型,就能在全包线提供有效的控制,既避免了传统方法的增益调参,又解决了难以获得动态逆模型及计算量大的问题,是一种很有发展潜力的智能控制方法。

关 键 词:直升机  飞机  控制系统  神经网络  反馈线化飞行控制
文章编号:1005-2615(2001)04-0351-04
修稿时间:2000年11月13

Flight Control of Helicopter by Feedback Linearization Based on Neural Networks
Huang Wenming Xu Jinfa Gao Zheng Key Laboratory of Helicopter Rotor Dynamics,Nanjing University of Aeronautics & Astronautics Nanjing ,P.R.China.Flight Control of Helicopter by Feedback Linearization Based on Neural Networks[J].Journal of Nanjing University of Aeronautics & Astronautics,2001,33(4):351-354.
Authors:Huang Wenming Xu Jinfa Gao Zheng Key Laboratory of Helicopter Rotor Dynamics  Nanjing University of Aeronautics & Astronautics Nanjing  PRChina
Institution:Huang Wenming Xu Jinfa Gao Zheng Key Laboratory of Helicopter Rotor Dynamics,Nanjing University of Aeronautics & Astronautics Nanjing 210016,P.R.China
Abstract:A maneuver simulation of the helicopter, modeling of SH-2G, is performed by using the nonlinear system control technology for feedback linearization based on neural network. Simulational result shows that the neural network is adaptive. It has the online capability of compensating the inverse error caused by feedback linearization. This approach can offer effective control throughout the full flight envelope and only the static inverse model based on a single flight condition is needed, instead of the dynamic inverse model. It solves some problems of gain scheduled, for using conventional approaches, difficulty for constructing the dynamic inverse model and intensive online computation. So it is a kind of intelligent control technology and has great potentialities.
Keywords:helicopters  flight control system  neural networks
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