| 带矢量喷管的一体化飞行/推进控制技术研究 |
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| 引用本文： | 王涛,孟庆明.带矢量喷管的一体化飞行/推进控制技术研究[J].航空动力学报,1999,14(4):437-439. |
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| 作者姓名： | 王涛 孟庆明 |
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| 作者单位： | 北京航空航天大学 |
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| 摘 要： | 本文对综合推力矢量飞行／推进控制系统的设计方法进行了研究，在充分考虑了推力矢量飞行、推进子系统之间的相互作用后，建立了带推力矢量综合飞行／推进控制系统的数学模型，结合推力矢量研究的特点，采用鲁棒伺服ＬＱＧ／ＬＴＲ设计法，进行控制系统的设计，通过仿真实验，证明设计达到了要求，方法可行
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| 关 键 词： | 航空发动机 矢量控制 喷管 |
| 收稿时间： | 3/1/1999 12:00:00 AM |
ROBUST INTEGRATED FLIGHT/PROPULSION CONTROL DESIGN FOR A STOL AIRCRAFT |
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| Wang Tao and Meng Qingming.ROBUST INTEGRATED FLIGHT/PROPULSION CONTROL DESIGN FOR A STOL AIRCRAFT[J].Journal of Aerospace Power,1999,14(4):437-439. |
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| Authors: | Wang Tao and Meng Qingming |
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| Institution: | 4th Dept.Beijing University of Aeronautics and Astronautics,Beijing 100083 |
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| Abstract: | An application of robust LQG/LTR control design methodology to a centralized integrated flight/propulsion control (IFPC) system design for STOL/MTD aircraft is presented.The emphasis is put on formulating the Robust Servo LQR (RSLQR)control synthesis problem.A conversion parameter is introduced in controller design to improve the comparability of the system parameters.A detailed evaluation is completed for a controller obtained from RSLQR control design.The results indicate that a RSLQR control design meets the IFPC control system with thrust vectoring. |
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| Keywords: | Aeroengines Vector control Nozzles |
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