| 面向飞推一体化的飞行器建模方法 |
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| 引用本文： | 孔雪,宁国栋,杨明,王松艳,晁涛.面向飞推一体化的飞行器建模方法[J].系统工程与电子技术,2019,41(1):141-147. |
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| 作者姓名： | 孔雪 宁国栋 杨明 王松艳 晁涛 |
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| 作者单位： | 1.哈尔滨工业大学航天学院控制与仿真中心, 黑龙江 哈尔滨 150001;
2.北京机电工程研究所, 北京 100074 |
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| 摘 要： | The airbreathing hypersonic vehicle (ABHV) is a typical vehicle which has multidimensional nonlinear restrictions and intricate coupling. Due to the strong coupling interactions and multidimensional nonlinear restrictionists,the flight powered by scramjet is a critical phase of reference trajectory, guidance and control designing. Therefore, the development of a reasonable ABHV model is inevitable. The existing models of integrated aircraft scramjet are difficult for control design directly，and also can not be used with a numeric model together. To achieve the goal of exhuming the potential applications and expanding flight feasibility of ABHV,and improving the efficiency and robustness of ABHV from the overall level, based on the working mechanism and numerical model of scramjet, the performance and protected model of scramjet is researched, and the control oriented model of ABHV is developed.
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Modeling method oriented to vehicle of integrated flight/propulsion |
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| KONG Xue,NING Guodong,YANG Ming,WANG Songyan,CHAO Tao.Modeling method oriented to vehicle of integrated flight/propulsion[J].System Engineering and Electronics,2019,41(1):141-147. |
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| Authors: | KONG Xue NING Guodong YANG Ming WANG Songyan CHAO Tao |
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| Institution: | 1. Control and Simulation Center, School of Aeronautics, Harbin Institute of Technology, Harbin 150001, China;;
2. Beijing Institute of Mechanical and Electrical Engineering, Beijing 100074, China; |
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