| 基于动态逆的直升机飞行品质设计研究 |
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| 引用本文： | 曹嘉旻. 基于动态逆的直升机飞行品质设计研究[J]. 科学技术与工程, 2011, 11(16): 3725-3728,3749 |
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| 作者姓名： | 曹嘉旻 |
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| 作者单位： | 中航工业飞行试验研究院,西安,710089 |
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| 摘 要： | 直升机的固有特点使其飞行品质较差,而直升机的使用任务却要求它具有良好的飞行品质。本文采用动态逆和极点配置相结合的方法设计直升机飞行控制律,并通过仿真手段进行检验,证实了样例直升机飞行品质提高以及所用飞行控制率的鲁棒性,从而表明本文控制律的有效性。
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| 关 键 词： | 直升机 飞行品质 飞行控制 动态逆 鲁棒性 |
| 收稿时间： | 2011-02-17 |
| 修稿时间： | 2011-03-07 |
The Research of Helicopter Flight Quality Based On The Dynamic Inversion |
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| caojiamin. The Research of Helicopter Flight Quality Based On The Dynamic Inversion[J]. Science Technology and Engineering, 2011, 11(16): 3725-3728,3749 |
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| Authors: | caojiamin |
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| Affiliation: | CAO Jia-min,GAO Hua(Chinese Flight Test Establishment,Xian 710089,P.R.China) |
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| Abstract: | Helicopter inherent characteristics make its flight poorer quality, and helicopters use task is asking that it has good flying qualities. This paper adopts dynamic inversion and poles configuration design method of combining the helicopter flying control law, and through the simulation method for inspection, confirmed the sample helicopter flight quality improvement and used the robustness of flight control, which shows that the control law is effective. |
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| Keywords: | Helicopter Flight Quality Flight Control Dynamic Inversion |
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