| 飞机直接力模态控制律设计 |
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| 引用本文： | 冯刚.飞机直接力模态控制律设计[J].航空学报,1988,9(2):51-57. |
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| 作者姓名： | 冯刚 |
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| 作者单位： | 南京航空学院 |
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| 摘 要： | 本文应用特征结构配置理论提出了一种飞机直接力模态控制系统设计方法,即适当选取闭环特征向量使得飞机相应状态动态解耦,从而实现飞机直接力模态控制要求。本文为某型飞机设计了直接力两种模态——机身俯仰和垂直平移的控制器。
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| 关 键 词： | |
| 收稿时间： | 1987-05-11; |
CONTROL LAW DESIGN OF A CCV AIRPLANE |
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| Feng Gang.CONTROL LAW DESIGN OF A CCV AIRPLANE[J].Acta Aeronautica et Astronautica Sinica,1988,9(2):51-57. |
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| Authors: | Feng Gang |
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| Institution: | Nanjing Aeronautical Institute |
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| Abstract: | In this paper, a method is presented for the design of control laws of a CCV airplane via eigenstructure assignment, i.e.,the eigenvectors of closed-loop system are selected properly to decouple the correspondant states of the aircraft,and to realize CCV control laws of the airplane. In the end of the paper, the controllers of pitch pointing and vertical translation modes are designed for an airplane.And the simulation results of two modes are excellent. |
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| Keywords: | eigenstructure assignment state feedback direct force control vertical translation pitch pointing |
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