期刊文献+

振动主动控制系统降级工作模式研究 被引量:2

Study on degradation mode of the active vibration control system
在线阅读 下载PDF
导出
摘要 振动主动控制系统是通过获取振动传感器信号、驱动作动器施加作动力以降低平台振动水平的机电综合系统。对于振动环境恶劣的装备平台,振动主动控制系统工作的稳定性直接影响平台使用体验。当系统内硬件数量较多时,系统对部件可靠度敏感度较高。为了提高系统功能可靠性,保证装备平台安全,在不改变硬件的前提下,本研究从优化控制策略出发,提出了两种系统降级模式,并对其进行可靠性分析;在降级模式的基础上,基于切换系统方法,针对硬件故障数量的不同设计不同等级的降级模式;针对不同降级模式下系统控制参数,对作动器进行最优组合设计,得到在不同降级模式下系统减振控制的最优高维度模型矩阵;最后在实验室内,基于振动主动控制系统实验环境,针对作动单元降级模式进行了实验验证,通过模拟部件故障状态,验证系统降级工作策略与控制模型优选设计的正确性,提高了系统功能可靠性。 The active vibration control system is an electromechanical integrated system which can reduce the vibration level of the platform by obtaining the vibration sensor signal and driving the actuator output force.The stability of the active vibration control system directly affects the experience of using the platform which obtains harsh vibrations.The system is highly sensitive to component reliability when the system contains lots of hardware.In order to improve the functional reliability of the system without changing the hardware,this paper proposes two system degradation modes of system control strategies and analyzes their reliability.Based on the system degradation modes and switch methods,different levels of degradation modes are designed according to the different number of hardware faults.According to the system control parameters under different degradation modes,the optimal combination design of the actuator is proposed.And the optimal high-dimensional matrix of system model under different degradation modes is obtained.Finally,in the laboratory,the degradation mode of the actuator is experimentally verified in the active vibration control system test platform.By disconnecting the power supply of the actuator,the system works correctly for the vibration reduce function.
作者 梁昆 李明强 王国胜 苑博 LIANG Kun;LI Mingqiang;WANG Guosheng;YUAN Bo(China Helicopter Research and Design Institute,333000 Jingdezhen,China)
出处 《应用力学学报》 CAS CSCD 北大核心 2023年第1期81-86,共6页 Chinese Journal of Applied Mechanics
基金 陆军装备预先研究项目(No.LZY20190501001)。
关键词 振动主动控制 降级模式 可靠性分析 实验验证 active vibration control degradation mode reliability analysis experiment verification
  • 相关文献

参考文献7

二级参考文献58

  • 1王芃,刘剑,李博.二乘二取二系统的安全性与可靠性分析[J].铁道通信信号,2013,0(S1):104-105. 被引量:7
  • 2杨铁军,顾仲权,鲁明月,雷凌云,朱明刚.基于误差通道在线辨识的结构振动主动控制系统[J].振动与冲击,2004,23(3):55-59. 被引量:22
  • 3陆轶,顾仲权.直升机结构响应主动控制作动器优化设计研究[J].振动与冲击,2007,26(3):23-26. 被引量:7
  • 4Johnson W. Self-tuning Regulations for Multicyclic Control of Helicopter Vibration [R]//NASA TP 1996. USA: NASA, 1982.
  • 5Stephen A Jacklin. Comparison of Five System Identification Algorithms for Rotorcraft Higher Harmonic Control [R]//NASA TP 1998. USA: NASA, 1998.
  • 6Dan Patt, Li Liu, Jaganath Chandrasekar, et al. Higher Harmonic Control Algorithm for Helicopter Vibration Reduction Revisited [J]. Journal of Guidance, Control, and Dynamics (S0731-5090), 2005, 28(5): 918-930.
  • 7Jonathan K Wong, William A Welsh, Rich Lamb, et aL Risk Reduction Flight Test of a Pre-Production Active Vibration Control System for the MH-60S [R]// Proceedings of the AHS Vertical Lift Aircraft Design Conference, San Francisco, California, USA. USA: American Helicopter Society International, Inc., January 18-19, 2006.
  • 8Teal R S, Mccorvey D L, Mailoy D. Active vibration suppression for the CH47D [ C]. 53rd Annual Forur3 of AHS, 1997:211 -219.
  • 9Welsh W, Fredrickson C, Rauch C. Flight test of an active vibration control system on the UH-60 black hawk helicopter [ C]. 51 81 Annual Forum of AHS, 1995 : 393 -402.
  • 10Goodman R K, Millott T A. Design, development, and flight testing of the active, ibration control system for the 5~ikorsky S- 92 [ C ].56th Annual Forum of AHS, 2000:764- 770.

共引文献32

同被引文献4

引证文献2

二级引证文献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