| 折叠翼飞行器鲁棒飞行控制系统设计方法 |
| |
| 引用本文： | 姜智超,吴森堂,金宪哲. 折叠翼飞行器鲁棒飞行控制系统设计方法[J]. 控制与决策, 2008, 23(7) |
| |
| 作者姓名： | 姜智超 吴森堂 金宪哲 |
| |
| 作者单位： | 北京航空航天大学,自动控制系,北京,100083;北京航空航天大学,自动控制系,北京,100083;北京航空航天大学,自动控制系,北京,100083 |
| |
| 摘 要： | 为解决折叠翼飞行器在机载发射段主升力翼面/立尾展开前后气动特性变化较大,以及对飞行控制律鲁棒性要求较高的问题,基于飞行器六自由度非线性动态模型,应用随机鲁棒分析与设计方法(SRAD),对机载发射段折叠翼飞行器的翼面/立尾展开过程,设计了鲁棒飞行控制律,并通过对风干扰环境下的六自由度非线性弹道仿真,验证了翼面/立尾展开段鲁棒飞行控制律的有效性.
|
| 关 键 词： | 折叠翼飞行器 鲁棒飞行控制律 随机鲁棒设计 |
Design of robust flight control systems for a flex-wing vehicle |
| |
| JIANG Zhi-chao,WU Sen-tang,JIN Xian-zhe. Design of robust flight control systems for a flex-wing vehicle[J]. Control and Decision, 2008, 23(7) |
| |
| Authors: | JIANG Zhi-chao WU Sen-tang JIN Xian-zhe |
| |
| Affiliation: | JIANG Zhi-chao,WU Sen-tang,JIN Xian-zhe (Department of Automatic,Beijing University of Aeronautics , Astronautics,Beijing 100083,China.) |
| |
| Abstract: | In order to resolve the big change of aerodynamic performance and high robustness desire of flight control systems before-and-after main lift fin/vertical tail of flex-wing vehicle unfold during airborne launch time,based on 6-DOF nonlinear dynamic flight model,robust flight control systems during main lift fin/vertical tail unfolded process in airborne launch time are designed by applying stochastic robustness analysis and design.The 6-DOF nonlinear trajectory in the interference of wind environment is sim... |
| |
| Keywords: | Flex-wing vehicle Robust flight control systems Stochastic robustness analysis and design |
| 本文献已被 CNKI 维普 万方数据 等数据库收录！ |
|
