| 侧向稳定系统参数平面设计法 |
| |
| 引用本文： | 费玉华,王宗学.侧向稳定系统参数平面设计法[J].飞行力学,1995,13(4):16-22. |
| |
| 作者姓名： | 费玉华 王宗学 |
| |
| 作者单位： | 北京航空航天大学 |
| |
| 摘 要： | 首先介绍了鲁棒系统设计的参数平面法，然后采用该方法对某支线客机的侧向稳定系统进行了鲁棒设计，最生以几种不同的飞行状态为例，通过计算机仿真，对所设计的控制律参数进行了验证，结果表明：飞机侧向稳定系统的参数平面法设计是可行的。
|
| 关 键 词： | 鲁棒性 部分状态反馈 旅客机 侧向稳定系统 |
THE PARAMETER SPACE DESIGN OF THE LATERAL-DIRECTIONAL STABILITY SYSTEMS |
| |
| Fei Yuhua,Wang Zongxue.THE PARAMETER SPACE DESIGN OF THE LATERAL-DIRECTIONAL STABILITY SYSTEMS[J].Flight Dynamics,1995,13(4):16-22. |
| |
| Authors: | Fei Yuhua Wang Zongxue |
| |
| Institution: | Beijing University of Aeronautics and Astronautics |
| |
| Abstract: | At first,this paper introduces the parameter space design of robust control systems.A robust design of lateral-directional stability system for a aircraft is then finished in the method.After that,with some flying-state as an example,the control law designed is verified by a computer simulation. Finally,the conclusion that the parameter space design of the aircraft lateral-directional stability system is good and can be applied to practical en-gineering was drawn up. |
| |
| Keywords: | Robust Part state variable feedback Parameter space design |
| 本文献已被 CNKI 维普 等数据库收录！ |
