垂尾抖振主动控制的压电作动器布局优化

doi:10.7527/S1000-6893.2016.0005

固体力学与飞行器总体设计

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

垂尾抖振主动控制的压电作动器布局优化

梁力, 杨智春, 欧阳炎, 王巍

西北工业大学航空学院结构动力学与控制研究所, 西安 710072

收稿日期:2015-09-18 修回日期:2015-11-22 出版日期:2016-10-15 发布日期:2016-01-22
通讯作者: 杨智春,Tel.:029-88460461 E-mail:yangzc@nwpu.edu.cn E-mail:yangzc@nwpu.edu.cn
作者简介:梁力男,硕士研究生。主要研究方向:结构振动主动控制。Tel.:029-88460461 E-mail:lil1991.0@163.com;杨智春男,博士,教授,博士生导师。主要研究方向:气动弹性力学、结构动力学及结构健康监测。Tel.:029-88460461 E-mail:yangzc@nwpu.edu.cn
基金资助:
国家自然科学基金（11502208）

Optimization of piezoelectric actuator configuration on a vertical tail for buffeting control

LIANG Li, YANG Zhichun, OUYANG Yan, WANG Wei

Institute of Structural Dynamics and Control, School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China

Received:2015-09-18 Revised:2015-11-22 Online:2016-10-15 Published:2016-01-22
Supported by:
National Natural Science Foundation of China (11502208)

摘要/Abstract

摘要：

为了提高压电作动器垂尾抖振主动控制系统的控制性能，提出一种基于输出可控性的压电作动器优化准则。使用压电驱动载荷等效方法建立压电纤维复合材料（MFC）压电作动器力学模型，并建立了带MFC压电作动器垂尾结构模型的动力学方程。在模态可控性和模态价值理论的基础上，提出考虑剩余模态影响的压电作动器优化目标函数。针对垂尾结构的前5阶模态使用遗传算法优化得到压电作动器的布局方案，使用线性二次高斯（LQG）最优控制方法控制垂尾的抖振响应。仿真结果表明，本文优化得到的布局方案比用其他方法能更好地均衡系统的模态可控性，减小剩余模态的影响，获得更好的垂尾抖振响应控制。

关键词: 压电作动器, 智能结构, 布局优化, 抖振, 可控性

Abstract:

In order to improve the control performance of the tail buffet control system using piezoelectric actuators, a new optimization criterion is used to optimize the configuration of piezoelectric actuators based on output controllability. Macro-fiber composite (MFC) piezoelectric actuator is modeled by a load simulation method of piezoelectric actuator. Dynamic equations of the vertical tail incorporating MFC actuators are obtained by finite element method. An objective function, using modal controllability and modal cost theory, is suggested with the consideration of residual modes to limit the spillover effect. In order to control the first five modes of the vertical tail, genetic algorithm is used to find the optimal configuration and linear-quadratic Gaussian (LQG) controller is adopted to control the response of the vertical tail. Simulation results show that the optimal configuration of MFC actuators not only improves the control performance but also balances system controllability and reduces the influence of residual modes.

Key words: piezoelectric actuators, smart structures, optimization of configuration, buffeting, controllability

中图分类号:

梁力, 杨智春, 欧阳炎, 王巍. 垂尾抖振主动控制的压电作动器布局优化[J]. 航空学报, 2016, 37(10): 3035-3043.

LIANG Li, YANG Zhichun, OUYANG Yan, WANG Wei. Optimization of piezoelectric actuator configuration on a vertical tail for buffeting control[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(10): 3035-3043.

参考文献

[1] LEE B H K. Vertical tail buffeting of fighter aircraft[J]. Progress in Aerospace Sciences, 2000, 36(3):193-279.
[2] MOSES R W, WIESEMAN C D, BENT A A, et al. Evaluation of new actuators in a buffet loads environment[C]//Proceedings of SPIE. Bellingham,WA:The International Society for Optics and Photonics, SPIE, 2001, 4332:10-21.
[3] CHEN Y, ULKER F D, WICKRAMASINGHE V, et al. Development of robust control law for active buffeting load alleviation of smart fin structures[J]. Journal of Intelligent Material Systems and Structures, 2014, 25(7):818-831.
[4] CHEN Y, VIRESH W, ZIMCIK D. Development and verification of real-time controllers for F/A-18 vertical fin buffet load alleviation[C]//Proceedings of SPIE. Bellingham,WA:The International Society for Optical Engineering, SPIE, 2006:617310.1-617310.12.
[5] GUPTA V, SHARMA M, THAKUR N. Optimization criteria for optimal placement of piezoelectric sensors and actuators on a smart structure:A technical review[J]. Journal of Intelligent Material Systems and Structures, 2010, 21(12):1227-1243.
[6] ARBEL A. Controllability measures and actuator placement in oscillatory systems[J]. International Journal of Control, 1981, 33(3):565-574.
[7] HAC A, LIU L. Sensor and actuator location in motion control of flexible structures[J]. Journal of Sound and Vibration, 1993, 167(2):239-261.
[8] COLLET M. Shape optimization of piezoelectric sensors dealing with spill-over instability[J]. IEEE Transactions on Control Systems Technology, 2001, 9(4):654-662.
[9] BRUANT I, PROSLIER L. Optimal location of actuators and sensors in active vibration control[J]. Journal of Intelligent Material Systems and Structures, 2005, 16(3):197-206
[10] BRUANT I, GALLIMARD L, NIKOUKAR S. Optimal piezoelectric actuator and sensor location for active vibration control, using genetic algorithm[J]. Journal of Sound and Vibration, 2010, 329(10):1615-1635.
[11] 王军, 杨亚东, 张家应, 等. 面向结构振动控制的压电作动器优化配置研究[J]. 航空学报, 2012, 33(3):494-500. WANG J, YANG Y D, ZHANG J Y, et al. Investigation of piezoelectric actuator optimal configuration for structural vibration control[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(3):494-500(in Chinese).
[12] SADRI A M, WYNNE R J, WRIGHT J R. Robust strategies for active vibration control of strain actuated plate like structures[C]//UKACC International Conference on (Conf. Publ. No. 455) Control '98. Herts, London:IET, 1998:213-218.
[13] SADRI A M, WRIGHT J R, WYNNE R J. Modelling and optimal placement of piezoelectric actuators in isotropic plates using genetic algorithms[J]. Smart Materials and Structures, 1999, 8(4):490-498.
[14] HAMDAN A M A, NAYFEH A H. Measures of modal controllability and observability for first-and second-order linear systems[J]. Journal of Guidance, Control, and Dynamics, 1989, 12(3):421-428.
[15] JUNKINS J L, KIM Y. Measure of controllability for actuator placement[J]. Journal of Guidance, Control, and Dynamics, 1991, 14(5):895-902.
[16] MEHRABIAN A R, YOUSEFI-KOMA A. A novel technique for optimal placement of piezoelectric actuators on smart structures[J]. Journal of the Franklin Institute, 2011, 348(1):12-23.
[17] SOHN J W, CHOI S B, KIM H S. Vibration control of smart hull structure with optimally placed piezoelectric composite actuators[J]. International Journal of Mechanical Sciences, 2011, 53(8):647-659.
[18] 李敏, 陈伟民, 王明春, 等. 压电驱动的载荷比拟方法[J]. 中国科学E辑:科学技术, 2009, 39(11):2576-2584. LI M, CHEN W M, WANG M C, et al. A load simulation method of piezoelectric actuator in FEM for smart structure[J]. Science in China Series E:Technological Science, 2009, 39(11):2576-2584(in Chinese).
[19] POPOV V M. Hyperstability of control systems[M]. Berlin:Springer-Verlag, 1974:52-55.
[20] SKELTON R E, SINGH R, RAMAKRISHNAN J. Component model reduction by component cost analysis[C]//AIAA Guidance, Navigation, and Control Conference. Reston:AIAA, 1988.
[21] JUNKINS J L, KIM Y. Introduction to dynamics and control of flexible structures[M]. Reston:AIAA, 1993:316-327.
[22] ALDRAIHEM O J, SINGH T, WETHERHOLD R C. Optimal size and location of piezoelectric actuator/sensors:Practical considerations[J]. Journal of Guidance, Control, and Dynamics, 2000, 23(3):509-515.
[23] PREUMONT A. Vibration control of active structures:An introduction[M]. 3rd ed. Berlin:Springer, 2011:261-264.

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

垂尾抖振主动控制的压电作动器布局优化

Optimization of piezoelectric actuator configuration on a vertical tail for buffeting control

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	张瑞桐, 汪雷, 刘佳佳, 朱继宏. 考虑接头参数化的空间桁架轻量化设计[J]. 航空学报, 2024, 45(5): 529715-529715.
[2]	郑志阳, 张阳, 张钊, 吴宝海, 张莹. 基于GA⁃SVR的薄壁叶片辅助支撑布局优化方法[J]. 航空学报, 2023, 44(4): 426805-426805.
[3]	何佳琦, 吴伟达, 罗阳军. 基于P-CS模型与数字孪生的星载天线反射器形面鲁棒性控制方法[J]. 航空学报, 2023, 44(19): 328343-328343.
[4]	李西宁, 叶园园, 李卫平, 王守川. 面向形状控制的传感器和作动器布局综合优化[J]. 航空学报, 2023, 44(13): 227880-227880.
[5]	胡嘉欣, 芮姝, 高瑞朝, 苟建军, 龚春林. 飞行器结构布局与尺寸混合优化方法[J]. 航空学报, 2022, 43(5): 225363-225363.
[6]	郭文杰, 朱继宏, 罗利龙, 常亮. 考虑组件保形约束的多组件结构系统布局优化[J]. 航空学报, 2022, 43(5): 225225-225225.
[7]	曾开春, 寇西平, 杨兴华, 余立, 查俊. 跨声速风洞试验模型主动减振结构优化设计[J]. 航空学报, 2022, 43(2): 224944-224944.
[8]	章胜华, 邓枫, 覃宁, 刘学强. 激波控制鼓包对跨声速抖振影响的数值研究[J]. 航空学报, 2022, 43(11): 526806-526806.
[9]	刘深深, 陈江涛, 桂业伟, 唐伟, 王安龄, 韩青华. 基于数据挖掘的飞行器气动布局设计知识提取[J]. 航空学报, 2021, 42(4): 524708-524708.
[10]	刘昊, 王巍, 金伟, 牛文超, 杨智春. 垂尾抖振响应的鲁棒-FxLMS主动控制试验[J]. 航空学报, 2021, 42(2): 224090-224090.
[11]	张科, 袁慎芳, 任元强, 徐跃胜. 基于逆向有限元法的变形机翼鱼骨的变形重构[J]. 航空学报, 2020, 41(8): 223617-223617.
[12]	何萌, 杨体浩, 白俊强, 杨一雄. 基于后缘襟翼偏转的大型客机变弯度技术减阻收益[J]. 航空学报, 2020, 41(7): 123462-123462.
[13]	金伟, 杨智春, 孟德虹, 陈炎, 黄虎, 王勇军, 何石, 陈园方. 先进战斗机全动V尾抖振动强度设计与验证[J]. 航空学报, 2020, 41(6): 523473-523473.
[14]	陈晓明, 孙绍山, 陶呈纲, 唐勇. 放宽静稳定度飞机时间延迟稳定边界[J]. 航空学报, 2020, 41(6): 523487-523487.
[15]	高传强, 张伟伟. 机翼跨声速抖振数值模拟及模态分析[J]. 航空学报, 2019, 40(7): 122597-122597.