期刊文献+

自适应伺服惯性力发生器的特性与应用研究 被引量:1

Feature and Application of Adaptive Servo Inertial Force Generators
下载PDF
导出
摘要 研究了伺服惯性力发生器的基本特性及其在直升机振动控制中的应用。首先,建立了由电液伺服控制器、电液伺服阀、液压作动筒、弹性元件和惯性元件组成的伺服惯性力发生器的数学模型;接着,确定了设计电液伺服控制器的准则,分析了伺服惯性力发生器的特性;进而研究了基于自适应前馈控制的振动控制器的设计;最后,将伺服惯性力发生器和振动控制器应用于直升机振动控制。仿真表明,伺服惯性力发生器可提供良好的减振效果。 Deals with the feature and application of a servo inertial force generator (SIFG). The SIFG is an electro hydraulic servo apparatus with two states: passive absorber and active vibration reductor, and includes an inertial mass, a spring, a hydraulic cylinder controlled by a servo valve and a servo controller. Firstly, the mathematical mo del of the SIFG is derived. The criteria for designing the servo controller are determinated. The features of the SIFG with or without the controller are analysed. Then, based on the principle of adaptive filtering, an adaptive controller is built. Lastly, the SIFG is installed in a helicopter fuselage. The vibration reduction of the passive absorber and the SIFG is compared, it can be concluded that the SIFG with adpative controller can provide better vibration reduction.
出处 《南京航空航天大学学报》 EI CAS CSCD 北大核心 1998年第4期366-370,共5页 Journal of Nanjing University of Aeronautics & Astronautics
关键词 直升机 结构振动 伺服系统 自适应控制 SIFG helicopters structural vibration electro hydraulic servo system adaptive control
  • 相关文献

参考文献1

二级参考文献1

共引文献2

同被引文献7

引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部