| 无垂尾推力矢量飞机的自适应控制仿真研究 |
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| 引用本文： | 王衍洋,刘军虎.无垂尾推力矢量飞机的自适应控制仿真研究[J].飞行力学,2004,22(4):9-12. |
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| 作者姓名： | 王衍洋 刘军虎 |
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| 作者单位： | 1. 北京航空航天大学,航空科学与工程学院,北京,100083
2. 中国航天科工集团,二院研发部,北京,100854 |
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| 基金项目： | 航空基金资助项目(00A51049) |
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| 摘 要： | 研究了采用自适应控制系统的无垂尾构型推力矢量飞机的飞行控制性能.论述了在有参数未知的情况,使用状态变量反馈可线性化的非线性系统的输出轨迹的控制问题,推导出了自适应控制律的设计方法.最后,针对算例飞机给出了仿真计算的结果,证实了在无垂尾构型推力矢量飞机上应用自适应控制系统的可行性.
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| 关 键 词： | 推力矢量 自适应控制 无垂尾构型 |
| 文章编号： | 1002-0853(2004)04-0009-04 |
| 修稿时间： | 2003年10月29 |
Adaptive Control for the Vertical Tailless Aircraft with Thrust Vectoring Control |
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| WANG Yan-yang,LIU Jun-hu.Adaptive Control for the Vertical Tailless Aircraft with Thrust Vectoring Control[J].Flight Dynamics,2004,22(4):9-12. |
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| Authors: | WANG Yan-yang LIU Jun-hu |
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| Institution: | WANG Yan-yang~1,LIU Jun-hu~2 |
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| Abstract: | In this paper, the design of an adaptive control system of the vertical tailless aircraft with thrust vectoring control was presented, and the problem of output trajectory control of the typical input-output feedback linearizable nonlinear dynamic system by state variable's feedback is considered. An adaptive control system is designed for a specific aircraft by the design method of the adaptive control system introduced in the paper. Some results are given, and the feasibility and correctness of the design of the adaptive control system then is confirmed. |
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| Keywords: | thrusting vector adaptive control vertical tailless aircraft |
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