| 某型无人机发动机动力学建模与仿真 |
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| 引用本文： | 何元磊,卢利斌,王翔,邓常兴.某型无人机发动机动力学建模与仿真[J].航空兵器,2007(1):28-31. |
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| 作者姓名： | 何元磊 卢利斌 王翔 邓常兴 |
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| 作者单位： | 第二炮兵工程学院,西安,710025 |
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| 摘 要： | 无人机飞控系统是无人机模拟训练系统的一个重要组成部分。本文基于某型无人机实飞参数,求解出发动机推力,建立了发动机动力学模型。结合无人机六自由度模型建立了无人机飞行仿真模型,并在MATLAB/SIMULINK环境下进行了仿真,结果表明该建模方法是正确的。
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| 关 键 词： | 无人机 发动机推力 六自由度模型 建模 仿真 飞控系统 |
| 文章编号： | 1673-5048(2007)01-0028-03 |
| 修稿时间： | 2006-11-13 |
Engine Dynamics Modeling and Simulation for a Type of UAV |
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| HE Yuan-lei,LU Li-bin,WANG Xiang,DENG Chang-xing.Engine Dynamics Modeling and Simulation for a Type of UAV[J].Aero Weaponry,2007(1):28-31. |
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| Authors: | HE Yuan-lei LU Li-bin WANG Xiang DENG Chang-xing |
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| Abstract: | Flight control system is an important part in UAV simulation training system.Based on several known flight parameters of a UAV,engine thrust force is calculated,a way of building engine dynamics model is put forward and a flight simulation model is established linked with six-degree-of-freedom mathematical model, a simulation is carried out with the environment of MATLAB/SIMULINK.The simulation result proves that the modeling method is benefit for the UAV simulation training system. |
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| Keywords: | UAV engine thrust force six-degree-of-freedom model modeling simulation flight control system |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
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