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智能桨叶振动自适应控制研究
引用本文:马扣根 Melch.,J.智能桨叶振动自适应控制研究[J].南京航空航天大学学报,1997,29(6):633-637.
作者姓名:马扣根 Melch.  J
作者单位:[1]南京航空航天大学直升机技术研究所 [2]德国宇航研究院结构力学研究所
基金项目:国家自然科学基金,航空科学基金
摘    要:以德国宇航研究院的智能桨叶为原型,研究了智能桨叶振动控制的实时仿真。以两台高速信号处理器(DSP)为核心,辅以其他器件,构造智能桨叶振动控制实时仿真系统。其中一台DSP用于智能桨叶动态特性的实时在线模拟,另一台用于实时控制。所提出的采用MX滤波器模拟智能桨叶的动态特性和反馈与自适应前馈组合控制方法均由专用汇编程序实现。在此系统上实现了对智能桨叶在4Ω、8Ω(Ω为旋翼转速)谐和激励下桨叶振动的控制,

关 键 词:振动主动控制  自适应控制  直升机  智能桨叶

Research on Adaptive Vibration Control of Smart Rotor Blade
Ma Kougen.Research on Adaptive Vibration Control of Smart Rotor Blade[J].Journal of Nanjing University of Aeronautics & Astronautics,1997,29(6):633-637.
Authors:Ma Kougen
Abstract:Deals with the real time simulation of smart rotor blade vibration control. A real time simulation system is constructed. The key units of the system are two Motorola DSP56002EVM boards. One of them is used as a rotor blade dynamics simulator, the other controller. In the simulator, two recursive MX filters are responsible for the responses caused by disturbances and controllers, respectively. In the control strategies, adaptive feedforward control and a presented hybrid control are studied. The hybrid control combines an adaptive feedforward controller with a conventional feedback controller, and can control the modal damping and the responses of smart blades simultaneously. The simulator and the controllers are realized by the special assembly language. The dramatical vibration reductions are obtained for harmonic excitations.
Keywords:active vibration control  adaptive control  helicopters  digital signal processing  real time simulation
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