| V/STOL飞机建模与仿真分析 |
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| 引用本文： | 范勇,朱纪洪,孟宪宇,刘凯,杨喜立.V/STOL飞机建模与仿真分析[J].中国工程科学,2011,13(3):107-112. |
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| 作者姓名： | 范勇 朱纪洪 孟宪宇 刘凯 杨喜立 |
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| 作者单位： | 1. 清华大学计算机科学与技术系,北京,100084
2. 海军装备研究院,北京,100161 |
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| 基金项目： | 国家863计划项目，国家自然科学基金项目 |
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| 摘 要： | 以原理验证机为背景,建立了无尾布局垂直/短距起降飞行器的数学模型,并通过智能自适应方法对其进行了闭环飞行控制,控制量通过控制分配合理的协调各操纵面,最后在MATLAB7.0/Simulink环境下通过数值仿真进行了验证。结果显示,该平台具备垂直/短距起降能力和较好的飞行性能。
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| 关 键 词： | 无尾布局飞行器 垂直/短距起降飞行器(V/STOL) 动力学建模 飞行控制 |
| 收稿时间： | 2009/12/25 0:00:00 |
| 修稿时间： | 2009/12/25 0:00:00 |
Study on modeling and simulation analysis
for tailless configured V/STOL |
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| Fan Yong,Zhu Jihong,Meng Xianyu,Liu Kai and Yang Xili.Study on modeling and simulation analysis
for tailless configured V/STOL[J].Engineering Science,2011,13(3):107-112. |
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| Authors: | Fan Yong Zhu Jihong Meng Xianyu Liu Kai and Yang Xili |
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| Affiliation: | Fan Yong1,Zhu Jihong1,Meng Xianyu1,Liu Kai1,Yang Xili2(1.Department of Computer Science & Technology,Tsinghua University,Beijing 100084,China,2.Naval Academy of Armament,Beijing 100161,China) |
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| Abstract: | The mathematical model was studied by mechanical analysis and CFD(computing fluid dynamics) computation.Besides,an intelligent adaptive based control law was proposed and the optimization approach is employed to solve the constrained control allocation problem.The results show good closed loop performance and validate the intelligent optimization approach of constrained control allocation for flight control. |
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| Keywords: | tailless configured aerial vehicle V/STOL dynamic modeling flight control |
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