| 引用本文: | 曾庆华,张为华.一种控制学科在设计回路的多学科设计优化方法.[J].国防科技大学学报,2004,26(2):1-4.[点击复制] |
| ZENG Qinghua,ZHANG WeiHua.MDO Research Involving Control Disciplinary in the Design Loop[J].Journal of National University of Defense Technology,2004,26(2):1-4[点击复制] |
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| 一种控制学科在设计回路的多学科设计优化方法 |
| 曾庆华, 张为华 |
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(国防科技大学 航天与材料工程学院，湖南 长沙 410073)
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| 摘要: |
| 提出了一种直接针对设计参数不确定性描述的鲁棒控制器设计方法，并将该方法的研究和多学科设计优化方法的研究结合起来，实现了控制学科在设计回路的多学科设计优化。以某无尾布局微型飞行器为例开展了气动、控制学科的并行设计优化研究，说明了该方法的可行性。 |
| 关键词: 微型飞行器 飞行控制 鲁棒控制 |
| DOI： |
| 投稿日期：2003-09-18 |
| 基金项目:国家自然科学基金资助项目(60175032) |
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| MDO Research Involving Control Disciplinary in the Design Loop |
| ZENG Qinghua, ZHANG WeiHua |
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(College of Aerospace and Materials Engineering, National University of Defense Technology, Changsha 410073, China)
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| Abstract: |
| This paper presents a robust controller design approach based on the design parameters uncertainty, which combines this method with multidisciplinary design optimization, and realizes MDO in the design loop in control disciplinary. The parallel optimization design of aerodynamics and control disciplinary for a given tailess MAV is studied to illustrate that this method is feasible. |
| Keywords: micro air vehicle flight control mdo robust control |
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