| 双层气囊隔振装置多目标协同姿态控制方法 |
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| 引用本文： | 卜文俊,施亮,何琳,徐伟.双层气囊隔振装置多目标协同姿态控制方法[J].国防科技大学学报,2019,41(6):70-74. |
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| 作者姓名： | 卜文俊 施亮 何琳 徐伟 |
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| 作者单位： | 海军工程大学振动与噪声研究所,湖北武汉430033;海军工程大学船舶振动噪声重点实验室,湖北武汉430033 |
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| 基金项目： | 国防科技重点实验室基金资助项目(61422040601-162204004) |
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| 摘 要： | 针对双层气囊隔振装置高精度姿态平衡控制需求,提出多目标协同姿态控制方法。通过建立双层隔振装置动力学模型、充放气控制等效作用力模型,建立了控制响应特性分析模型。并基于多目标满意优化方法建立了多目标协同姿态控制方法,使得双层气囊隔振装置能够较好地适应上下层气囊隔振装置姿态耦合,实现姿态平衡控制,并可有效抑制结构弹性变形对姿态平衡控制的影响。在双层气囊隔振装置上验证了该控制方法的可行性。该方法将用于某型船舶大型发电机组双层气囊隔振系统,实现双层气囊隔振装置柔性支撑状态下的姿态平衡控制。
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| 关 键 词： | 双层气囊隔振装置 多目标协同 姿态控制 |
| 收稿时间： | 2018/8/20 0:00:00 |
| 修稿时间： | 2018/12/24 0:00:00 |
Multi-objective coordinated attitude control method for dual layer air spring vibration isolation mounting |
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| BU Wenjun,SHI Liang,HE Lin and XU Wei.Multi-objective coordinated attitude control method for dual layer air spring vibration isolation mounting[J].Journal of National University of Defense Technology,2019,41(6):70-74. |
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| Authors: | BU Wenjun SHI Liang HE Lin and XU Wei |
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| Institution: | Institute of Vibration & Noise, Naval University of Engineering, Wuhan 430033, China;National Key Laboratory on Ship Vibration & Noise, Naval University of Engineering, Wuhan 430033, China,Institute of Vibration & Noise, Naval University of Engineering, Wuhan 430033, China;National Key Laboratory on Ship Vibration & Noise, Naval University of Engineering, Wuhan 430033, China,Institute of Vibration & Noise, Naval University of Engineering, Wuhan 430033, China;National Key Laboratory on Ship Vibration & Noise, Naval University of Engineering, Wuhan 430033, China and Institute of Vibration & Noise, Naval University of Engineering, Wuhan 430033, China;National Key Laboratory on Ship Vibration & Noise, Naval University of Engineering, Wuhan 430033, China |
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| Abstract: | A multi-objective coordinated attitude control method was studied in this paper, which aimed at the high precision attitude control of the dual layer air spring vibration isolation mounting. After establishing the dynamics model of dual layer air spring vibration isolation mounting and the equivalent model of charge and discharge control, the control response characteristic model was established. Then the multi-objective coordinated attitude control model was brought out based on the multi-objective satisfactory optimization method. This control method can adapt to the attitude control coupling of the superstratum and the substratum air spring vibration isolation mounting. And it can also restrain the elasticity distortion influence on the attitude equilibrium control. This control method was verified on a dual layer air spring vibration isolation mounting experimental system. It will be used in a dual air spring vibration isolation mounting for some large ship generator set and realize the high vibration isolation efficiency. |
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| Keywords: | dual air spring vibration isolation mounting multi-objective coordinated attitude control |
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