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| 飞机自动拉平着陆系统设计及仿真 | |
| 引用本文： | 曲东才,冯玉光,程继红,任建存. 飞机自动拉平着陆系统设计及仿真[J]. 海军航空工程学院学报, 2013, 28(1): 1-5 |
| 作者姓名： | 曲东才 冯玉光 程继红 任建存 |
| 作者单位： | 1. 海军航空工程学院 控制工程系,山东烟台264001 2. 海军航空工程学院 兵器科学与技术系,山东烟台264001 3. 海军航空工程学院 科研部,山东烟台264001 |
| 基金项目： | 国家自然科学基金资助项目(60774016) |
| 摘 要： | 简述了自动拉平系统基本工作原理,对拉平轨迹及指数拉平规律进行分析,之后设计了自动拉平耦合器和拉平着陆系统。在MATLAB平台下,建立了自动拉平着陆系统结构图,并进行了大量仿真研究。仿真结果表明,所设计的自动拉平耦合器和拉平着陆系统参数合适、结构合理,系统工作稳定,并能满足预定的着陆参数要求。 |
| 关 键 词： | 自动拉平系统 拉平轨迹 拉平耦合器 Simulink仿真 |
Design and Simulation on Aerocraft Auto Flatten-Out and Landing System |
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| QU Dong-cai,FENG Yu-guang,CHENG Ji-hong and REN Jian-cun. Design and Simulation on Aerocraft Auto Flatten-Out and Landing System[J]. Journal of Naval Aeronautical Engineering Institute, 2013, 28(1): 1-5 | |
| Authors: | QU Dong-cai FENG Yu-guang CHENG Ji-hong REN Jian-cun |
| Affiliation: | a(Naval Aeronautical and Astronautical University a.Department of Control Engineering;b.Department of Ordnance Science and Technology;c.Department of Scientific Research,Yantai Shandong 264001,China) |
| Abstract: | Firstly, the basic principle of aerocraft auto flatten-out system was simply depictioned, level fly trajectory and exponential rule were analyzed. Secondly, the auto pullout coupler and auto changed level landing system were designed. Lastly,. under the MATLAB platform, the structure diagram of aero auto changed level fly system was established. A great deal of simulation researches was done. Simulation results indicated that the structure of designed auto flatten-out system and it＇s coupler was reasonable, and the control system was stability, and could meet demand for scheduled landing parameters |
| Keywords: | auto flatten-out system level fly trajectory pullout coupler simulation |
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