| 无人机飞行控制系统非线性设计技术研究 |
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| 引用本文： | 杨遵,雷虎民,刘玉浩.无人机飞行控制系统非线性设计技术研究[J].战术导弹控制技术,2008(2). |
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| 作者姓名： | 杨遵 雷虎民 刘玉浩 |
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| 作者单位： | 桂林空军学院;空军工程大学导弹学院;空军第三飞行学院; |
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| 基金项目： | 总装武器装备预研基金资助项目(9140A04050407JB3201);;航天科技创新基金资助项目(CASC0209) |
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| 摘 要： | 基于现代控制理论的非线性设计是现代无人机飞行控制系统的重要设计方法。在分析总结国内外文献资料的基础上,论述了当前无人机飞行控制系统设计领域中几种重要的非线性设计技术,包括非线性反馈线性化方法、滑模变结构控制方法、多模型自适应控制方法和基于控制Lya- punov函数的Backstepping方法。
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| 关 键 词： | 无人机 飞行控制 反馈线性化 滑模变结构控制 多模型自适应控制 Backstepping |
Study of nonlinear design technique for unmanned aerial vehicle flight control system |
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| YANG Zun LEI Hu-min LIU Yu-hao.Study of nonlinear design technique for unmanned aerial vehicle flight control system[J].Control Technology of Tactical Missile,2008(2). |
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| Authors: | YANG Zun LEI Hu-min LIU Yu-hao |
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| Affiliation: | 1.Guilin Air Force Academy;Guilin 541003;China;2.The Missile Institute;Airforce Engineering University;Sanyuan 713800;3.No.3 Flight Academy of Air Force;Jinzhou 121000;China |
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| Abstract: | The nonlinear design based on the modem control theory is an important design approach of the unmanned aerial vehicle flight control system.After analyzing and summarizing the home and abroad references,several nonlinear techniques were presented in the field of the current unmanned aerial vehi- cle flight control system.They are nonlinear feedback linearization,sliding mode variable structure con- trol,multiple model adaptive control and Backstepping approach based the control Lyapunov function. |
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| Keywords: | unmanned aerial vehicle flight control feedback linearization sliding mode variable structure control multiple model adaptive control Backstepping |
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