飞机下滑波束导引系统设计及仿真
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(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. 海军装备部,西安 710089;4. 海军航空兵学院,辽宁 葫芦岛 125001)

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V249.12

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Design and Simulation of Aero Glide Beam Guidance System
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(1. Naval Aeronautical and Astronautical University, Department of Control Engineering, Yantai Shandong 264001, China;2. Naval Aeronautical and Astronautical University,Department of Ordnance Science and Technology, Yantai Shandong 264001, China;3. Naval Equipment Department, Xi’an 710089, China; 4. Naval Aviation Institute, Huludao Liaoning 125001, China)

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    摘要:

    下滑波束导引系统是飞机在自动着陆时所采用的一种重要无线电波束导引系统。首先,简要阐述了下滑波束导引系统的基本工作原理;然后,对导引系统的运动学环节及下滑耦合器进行分析,对飞机下滑波束导引系统结构进行设计;最后,在MATLAB平台下,对所设计的下滑波束导引系统进行大量仿真研究。仿真结果显示,所设计的下滑波束导引系统结构是合理的,其控制系统是稳定的,且其稳态性能也得到改善。

    Abstract:

    The aero glide beam guidance system is an important radio wave guidance system in airplane auto land. Firstly, basic work principle of aero glide beam guidance system was brief discussed. Secondly, kinematic link and glide coupler in the glide beam guidance system were analyzed. The system structure of aero glide beam guidance system was designed. Lastly, a great deal of simulation studies were was done to design aero glide beam guidance system under the Matlab platform. Simulation results showed that the structure of designed aero glide beam guidance system was reasonable, and its control system was stability, and its steady state capability also got an improvement.

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引用本文

曲东才,谢曦鹏,曹栋,冯玉光.飞机下滑波束导引系统设计及仿真[J].海军航空大学学报,2014,29(3):209-212
QU Dong-cai, XIE Xi-peng, CAO Dong, FENG Yu-guang. Design and Simulation of Aero Glide Beam Guidance System[J]. JOURNAL OF NAVAL AVIATION UNIVERSITY,2014,29(3):209-212

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  • 在线发布日期: 2015-04-28
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