| 推力矢量控制飞行的仿真研究 |
| |
| 引用本文： | 王立峰,张津,唐海龙.推力矢量控制飞行的仿真研究[J].航空动力学报,2000,15(4):427-430. |
| |
| 作者姓名： | 王立峰 张津 唐海龙 |
| |
| 作者单位： | 北京航空航天大学,404教研室,北京,100083 |
| |
| 摘 要： | 针对推力矢量控制飞行进行了仿真研究.推力矢量参与飞行控制,提高了飞机过失速飞行控制能力.在已建立的飞机和部件级的推进系统模型的基础上,进行了过失速机动飞行仿真,对推进系统常规控制与稳定性控制作了对比,结果验证了推力矢量控制飞行的可行性.
|
| 关 键 词： | 推力矢量控制 飞机模型 发动机模型 综合飞行/推进控制 |
| 收稿时间： | 1999/11/8 0:00:00 |
| 修稿时间： | 1999-11-08 |
Simulation of Vector Thrust Control Flight |
| |
| WANG Li-feng,ZHANG Jin and TANG Hai-long.Simulation of Vector Thrust Control Flight[J].Journal of Aerospace Power,2000,15(4):427-430. |
| |
| Authors: | WANG Li-feng ZHANG Jin and TANG Hai-long |
| |
| Institution: | 4th Dept.,Beijing University of Aeronautics and Astronautics,Beijing100083,China;4th Dept.,Beijing University of Aeronautics and Astronautics,Beijing100083,China;4th Dept.,Beijing University of Aeronautics and Astronautics,Beijing100083,China |
| |
| Abstract: | A simulation about vector thrust control flight was completed.On the basis of aircraft model and propulsion model, post stall flight simulation on routine engine control and engine stability control was accomplished.The results verify feasibilily of the vector thrust control flight. |
| |
| Keywords: | vector thrust contol engine model aircraft model integrated flight and propulsion control |
| 本文献已被 CNKI 万方数据 等数据库收录！ |
| 点击此处可从《航空动力学报》浏览原始摘要信息 |
| 点击此处可从《航空动力学报》下载免费的PDF全文 |
|
