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飞机侧向波束导引控制系统结构方案及仿真
引用本文:曲东才,程继红,解传军.飞机侧向波束导引控制系统结构方案及仿真[J].海军航空工程学院学报,2016,31(3):332-336.
作者姓名:曲东才  程继红  解传军
作者单位:海军航空工程学院控制工程系,山东烟台 264001,海军航空工程学院科研部,山东烟台 264001,海军航空兵学院四系,辽宁葫芦岛 125001
摘    要:侧向波束导引控制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。分析了侧向波束导引控制系统原理,基于飞机协调控制,构建一种侧向波束导引控制系统结构方案,在 MATLAB平台下,对所设计的侧向波束导引控制系统进行大量仿真研究。仿真结果显示,所设计的侧向波束导引控制系统结构是合理的,当其侧向耦合器结构参数设置准确时,可很好地改善导引控制系统的稳定性及动态品质。

关 键 词:侧向波束  偏差角  侧向耦合器  导引控制规律  仿真研究

Scheme Design and Simulation of Aero Lateral Beam Guidance Control System
QU Dongcai,CHENG Jihong and XIE Chuanjun.Scheme Design and Simulation of Aero Lateral Beam Guidance Control System[J].Journal of Naval Aeronautical Engineering Institute,2016,31(3):332-336.
Authors:QU Dongcai  CHENG Jihong and XIE Chuanjun
Institution:Naval Aeronautical and Astronautical University Department of Control EngineeringYantai Shandong 264001, China,Naval Aeronautical and Astronautical University Department of Scientific Research, Yantai Shandong 264001, China and The 4th Department of Naval Avation Institute, Huludao Liaoning 250011, China
Abstract:The aero lateral beam guidance system is an important radio wave guidance control system in airplane auto land.The basis work principle of the aero lateral beam guidance control system was briefly analyzed, and basis on assumptionaero lateral harmonious control foundation, the compendious structure scheme of aero lateral beam guidance system wasdesigned. Lastly, a great deal of simulation researches was done to designed aero lateral beam guidance system under theMATLAB platform. Simulation results showed that the designed structure scheme of aero lateral beam guidance systemwas reasonable, and when parameters of the lateral coupler was reasonable set on, stability nd dynamic qualities of the de.signed control system were greatly improved.
Keywords:lateral beame  deviation angle  lateral coupler  guidance control law  simulation research
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