一种天线馈源结构在扰动力影响下的振动控制方法

Vibration control method for feed source structure under external excitation

  • 摘要: 高功率微波系统上使用的固面天线一般为悬臂结构,在有外界扰动力情况下,很难保持馈源结构较低加速度响应的要求。传统的动力吸振方法可以较好地控制悬臂结构的振动响应,但是这种方法仅能在一个有限的频率范围内抑制悬臂结构的响应加速度。为了解决上述问题,提出了一种主动控制与被动吸振相结合的最优振动控制方法。通过分析和仿真固面天线的结构模型得到主动吸振器最佳的安装位置,然后根据简化被动吸振器数学模型计算出最优的参数,在此基础上,将滑模控制方法与主动吸振方法相结合设计了相应的控制律,同时,证明了控制律的稳定性。仿真分析了存在主动控制吸振器情况下的两自由度振动系统,得出天线馈源结构随时间的振动响应情况。结果表明:该方法可以有效降低在外界扰动下馈源结构顶部的加速度响应,顶部最大振幅相比无控制情况可降低95%以上,馈源结构在该控制器作用下处于较稳定的状态。

     

    Abstract:
    Background
    The structure of cantilever has existed in solid surface antenna for high power microwave system. It is difficult to maintain the low acceleration for feed source structure of solid surface antenna during external vibration excitation. The traditional dynamic vibration absorber has a good control effect on the structure of cantilever. However, the application of traditional dynamic vibration absorber is limited to a narrow range of frequency.
    Purpose
    This study aims to solve the problems of large acceleration and narrow range of frequency in traditional vibration absorber of solid surface antenna. A kind of active vibration control method combined with optimal passive absorber is proposed in this paper.
    Methods
    Firstly, the best installed position of dynamic absorber is obtained by analyzing and simulating the model of solid surface antenna. Secondly, the optimal parameters are calculated according to the mathematical model of simplified passive dynamic absorber system. Thirdly, the sliding mode control parameters were obtained by considering the external excitation using an active absorber method. Finally, the stability of sliding mode control method was demonstrated.
    Results
    This control method combined sliding mode control with an active control absorber, which can reduce the vibration response of antenna effectively. This paper simulated the two-degree-of-freedom vibration system with active control absorber, which gave time-domain vibration response of antenna. The top point displacement of antenna under the predetermined excitation was reduced more than 95% by comparing the condition of no control strategy.
    Conclusions
    This vibration control method can effectively reduce acceleration for feed source structure, enabling it to maintain a more stable state. Furthermore, this controller can be extended to control the acceleration of various cantilever structures in pulse power equipment.

     

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