首页 | 本学科首页   官方微博 | 高级检索  
     

主控格栅反射器基体结构/压电作动器参数集成优化设计
引用本文:宋祥帅,初未萌,谭述君,吴志刚. 主控格栅反射器基体结构/压电作动器参数集成优化设计[J]. 宇航学报, 2021, 42(2): 150-158. DOI: 10.3873/j.issn.1000-1328.2021.02.002
作者姓名:宋祥帅  初未萌  谭述君  吴志刚
作者单位:1. 大连理工大学航空航天学院,大连 116024; 2. 大连理工大学工业装备结构分析国家重点实验室,大连 116024
基金项目:国家自然科学基金(11572069,11872381,11432010)
摘    要:为提高反射器形面控制能力和减小在轨热变形,本文以锆钛酸铅压电陶瓷(PZT)驱动的主控格栅反射器为研究对象,开展反射器基体结构和PZT压电作动器参数的集成优化设计研究。首先,建立主控格栅反射器有限元模型并通过实验验证了有限元模型的正确性。然后,以形面控制能力最大和热变形最小为目标函数,以设计变量上限、下限和结构基频为约束,采用遗传算法(GA)和非支配排序遗传算法(NSGA-II)求解。最后,给出多个仿真算例的优化结果。仿真结果表明,控制能力最大的单目标优化,其热变形远大于控制能力,多目标的帕累托(Pareto)最优前沿可以给出更合理的设计方案。通过优化设计可以显著提高形面控制能力和减小热变形。

关 键 词:集成优化设计  天线反射器  PZT作动器  多目标优化  遗传算法  形面控制
收稿时间:2019-12-20

Integrated Optimization Design of Base Structure/PiezoelectricActuatorParameters for a Grid Reflector with Actuators
SONG Xiang shuai,CHU Wei meng,TAN Shu jun,WU Zhi gang. Integrated Optimization Design of Base Structure/PiezoelectricActuatorParameters for a Grid Reflector with Actuators[J]. Journal of Astronautics, 2021, 42(2): 150-158. DOI: 10.3873/j.issn.1000-1328.2021.02.002
Authors:SONG Xiang shuai  CHU Wei meng  TAN Shu jun  WU Zhi gang
Affiliation:1. School of Aeronautics and Astronautics, DalianUniversity of Technology, Dalian 116024, China;2. StateKey Laboratory of Structural Analysis for Industrial Equipment, DalianUniversity of Technology, Dalian 116024, China
Abstract:To improve the shape control ability of an antennareflector and reduce its thermal deformation in orbit, an integrated optimaldesign of the base structure/PZT actuator parameters for a grid reflectordriven by lead zirconate titanate (PZT) actuators is studied. Firstly, a finiteelement model for the reflector is established, and the accuracy of themodeling method is verified by experiments. Then, the maximum shape controlability and the minimum thermal deformation are considered as the objectivefunctions. The upper and lower limits of the design variables and thefundamental frequency of the structure are considered as the constraints. Thegenetic algorithm (GA) and the non dominated genetic algorithm(NSGA II) are applied to solve the optimizationproblem. Finally, the optimization results of several simulation examples arepresented. The simulation results demonstrate that the single objective optimization with the largest control capability has athermal deformation far greater than the control capability, and the multi objective Pareto optimal front can give morereasonable design solutions. The shape control ability of the reflector can besignificantly improved and its thermal deformation can be reduced by theoptimum design.
Keywords:
本文献已被 CNKI 等数据库收录!
点击此处可从《宇航学报》浏览原始摘要信息
点击此处可从《宇航学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号