| ASTOVL升力风扇飞机的组合飞行/推进控制系统的研究 |
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| 引用本文： | 金爱娟,郭锁凤,徐松源. ASTOVL升力风扇飞机的组合飞行/推进控制系统的研究[J]. 哈尔滨理工大学学报, 2000, 5(5): 50-53 |
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| 作者姓名： | 金爱娟 郭锁凤 徐松源 |
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| 作者单位： | 上海交通大学,船舶与海洋工程学院,上海,200030;南京航空航天大学,自动控制系,南京,210016;哈尔滨理工大学,计算机与控制学院,黑龙江,哈尔滨,150080 |
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| 摘 要： | 介绍了推力矢量技术,动态逆原理,研究了推力矢量喷管,升风风扇以及气动舵面组合作用下ASTOVL升力风扇飞机的飞行／推进控制系统,采用非线性动态逆理论并针对ASTOVL升力风扇飞机的俯仰控制,设计了动态逆控制律,并将所设计的控制规律进行了仿真。结果证明,该方法能够满足控制系统性能的要求,具有工程应用前景。
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| 关 键 词： | 推力矢量 组合飞行/推进控制系统 非线性动态逆控制律 广义逆 ASTOVL升力风扇飞机 |
| 文章编号： | 1007-2683(2000)05-0050-04 |
| 修稿时间： | 2000-03-22 |
Study of the Integrated Flight/Propulsion Control System for ASTOVL Lift-fan Aircraft |
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| JIN Ai-juan,GUO Suo-feng,XU Song-yuan. Study of the Integrated Flight/Propulsion Control System for ASTOVL Lift-fan Aircraft[J]. Journal of Harbin University of Science and Technology, 2000, 5(5): 50-53 |
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| Authors: | JIN Ai-juan GUO Suo-feng XU Song-yuan |
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| Abstract: | Thrust vector technology and dynamic inverse principle are presented. A flight/propulsion control system about ASTOVL lift-fan aircraft is developed where lift-fan, thrust vector nozzles and aerodynamic control surfaces are integrated together. For the pitch control, the control law is designed with dynamic inverse theory, then it is applied to the simulation. The results indicate that this method is efficient to control the system, which will provide an extensive prospect of application in engineering. |
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| Keywords: | thrust vecotr integrated flight/propulsion control system nonlinear dynamic inverse control law pseudoinverse ASTOVL lift-fan aircraft |
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