| 基于能量的大型飞机纵向着陆控制研究 |
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| 引用本文： | 李爱军,徐小野,柯吉,袁刚.基于能量的大型飞机纵向着陆控制研究[J].西北工业大学学报,2011,29(1). |
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| 作者姓名： | 李爱军 徐小野 柯吉 袁刚 |
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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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| 基金项目： | 航空科学基金(20080553018、20090753007)资助 |
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| 摘 要： | 文章分析并建立了基于能量的大型飞机纵向自动着陆控制系统。利用特征结构配置方法(Eigen structure Assignment,EA)设计了飞机俯仰姿态保持内回路和控制增稳系统,针对发动机推力回路复杂模型不确定性,用定量反馈法(Quantitative Feedback Theory,QFT)对推力回路进行了补偿设计,以总能量控制为核心控制结构,协调控制飞机升降舵和油门杆,实现飞行速度和飞行航迹的解耦,进而完成定坡度下滑和拉平过程。仿真表明所设计的自动着陆控制系统满足飞机精确进场和着陆要求。
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| 关 键 词： | 自动着陆 总能量控制 大型飞机 解耦 |
Applying Total Energy Control to Designing Feasible Large Aircraft Longitudinal Landing Control System |
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| Li Aijun,Xu Xiaoye,Ke Ji,Yuan Gang.Applying Total Energy Control to Designing Feasible Large Aircraft Longitudinal Landing Control System[J].Journal of Northwestern Polytechnical University,2011,29(1). |
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| Authors: | Li Aijun Xu Xiaoye Ke Ji Yuan Gang |
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| Abstract: | Aim.The introduction of the full paper reviews some papers in the open literature,mostly in Chinese,and then applies total energy control to achieving its feasibility.Sections 1,2 and 3 explain our design and give simulation results to verify its feasibility.The core of section 2 consists of:(1) we utilize the Eigen-structure assignment(EA) method to design the pitch inner-loop of aircraft and its control augmentation system;(2) taking both the uncertainty and complexity of aircraft engine control loop into... |
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| Keywords: | aircraft landing control control system analysis automatic landing control system total energy control |
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