| 阵风减缓直接升力控制方案的仿真研究 |
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| 引用本文： | 费玉华.阵风减缓直接升力控制方案的仿真研究[J].飞行力学,2000,18(1):69-72. |
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| 作者姓名： | 费玉华 |
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| 作者单位： | 北京航空航天大学自动控制系,北京,100083 |
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| 摘 要： | 阵内减缓技术可有效地抑制飞机飞行过程中受到阵风和湍充影响所产生的附加过载。研究阵风载荷减缓的基本原理及各种控制方案，结合我国的实际情况，提出了以副翼作为直接升力操纵面的阵风减缓控制方案，建立了直接升力控制的阵风减缓系统的数学模型，并就阵风减缓系统进行了计算机辅助设计与仿真，验证了方案的可行性。
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| 关 键 词： | 阵风减缓系统 直接力控制 飞机副翼 |
| 修稿时间： | : |
Direct Lift Force Control Plan about Gust Load Alleviation Modeling and Simulation |
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| Fei Yuhua.Direct Lift Force Control Plan about Gust Load Alleviation Modeling and Simulation[J].Flight Dynamics,2000,18(1):69-72. |
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| Authors: | Fei Yuhua |
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| Abstract: | During aircraft is flying and when gust and turbulence is encountered ,the load acting on the aircraft wing may be reduced with gust load alleviation system. Researching the principle of gust load alleviation and control plan, the gust load alleviation system with additional aileron that is used to surface of direct lift force is given. The direct lift force control plan about gust load alleviation modeling, computing design and simulation about gust load alleviation are given. Simulation proves that the gust load alleviation control plan is feasible. |
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| Keywords: | gust alleviation active control technology direct force control modeling and simulation |
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