| 飞机鲁棒控制器的设计及检验 |
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| 引用本文： | 毛师彬,史忠科.飞机鲁棒控制器的设计及检验[J].飞行力学,2006,24(1):22-25. |
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| 作者姓名： | 毛师彬 史忠科 |
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| 作者单位： | 西北工业大学,自动化学院,陕西,西安,710072 |
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| 摘 要： | 针对飞机鲁棒控制器设计中的检验问题,介绍了系统检验标准,讨论了系统检验的重要性,重点阐述了对系统进行稳定裕度检验、性能指标检验以及控制器脆弱性检验的方法。提出了利用军标要求对鲁棒控制系统进行性能指标检验,并给出了相应控制器脆弱性的检验方法。对某型飞机设计了纵向运动系统的控制器,并对其进行了系统检验。
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| 关 键 词： | 飞控系统 系统检验 稳定裕度 性能检验 脆弱性 |
| 文章编号： | 1002-0853(2006)01-0022-04 |
| 收稿时间： | 2005-01-23 |
| 修稿时间： | 2006-01-13 |
The Design and Examination of Flight Robust Controller |
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| MAO Shi-bin,SHI Zhong-ke.The Design and Examination of Flight Robust Controller[J].Flight Dynamics,2006,24(1):22-25. |
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| Authors: | MAO Shi-bin SHI Zhong-ke |
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| Abstract: | In this paper,the importance of flight control system performance testing is emphasized.And the testing criteria are discussed,for example,stable margins, performance index,and controller fragility.The method of testing the system with military norm and the method of testing the controller with the fragility is presented.A new controller was designed for an aircraft,and the new flight system is examined with the stable margin and the military norm,and the controller is examined with the fragility standard. |
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| Keywords: | flight control system system testing stable margin performance testing fragility |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
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