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| 综合飞行/推力控制系统的智能设计 | |
| 引用本文： | 郑小洪,侯志强,庞向征,王春城,贾忠湖.综合飞行/推力控制系统的智能设计[J].海军航空工程学院学报,2008,23(6):611-614, 618. |
| 作者姓名： | 郑小洪 侯志强 庞向征 王春城 贾忠湖 |
| 作者单位： | 1. 海军航空工程学院,研究生管理大队,山东,烟台264001 2. 海军航空工程学院,飞行器工程系,山东,烟台264001 3. 91498部队,河北,秦皇岛,066203 |
| 摘 要： | 在介绍正规矩阵参数优化方法和着舰导引控制系统的基础上，为提高舰载飞机的操纵性能，采用智能设计软件IntelDes3．0设计了具有鲁棒性的着舰飞行，推力综合控制系统。基于飞机纵向非线性运动方程的数值仿真结果表明，设计的控制系统对阶跃输入的响应性能良好，鲁棒性较强。 |
| 关 键 词： | 着舰 控制系统 智能设计 |
Intelligent Design of Integrated Flight/Thrust Control System |
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| ZHENG Xiao-hong,HOU Zhi-qiang,Pang Xiang-zheng,WANG Chun-cheng and JIA Zhong-hu.Intelligent Design of Integrated Flight/Thrust Control System[J].Journal of Naval Aeronautical Engineering Institute,2008,23(6):611-614, 618. | |
| Authors: | ZHENG Xiao-hong HOU Zhi-qiang Pang Xiang-zheng WANG Chun-cheng and JIA Zhong-hu |
| Institution: | ZHENG Xiao-hong1a,HOU Zhi-qiang1b,Pang Xiang-zheng2,WANG Chun-cheng2,JIA Zhong-hu1b (1.Naval Aeronautical , Astronautical University a.Graduate Students\' Brigade,b.Department of Airborne Vehicle Engineering,Yantai Sh,ong 264001,China,2.The 91498th Unit of PLA,Qinghuangdao Hebei 066203,China) |
| Abstract: | The Optimization of Parameterized Normal Matrix and the carrier landing guidance control system were introduced.And in order to increase the carrier-based aircraft handling characteristics,the intelligent design software of IntelDes 3.0 was used to design the robust carrier landing flight/thrust control system.The simulation was base on the aircraft longitudinal nonlinear motion equation.And the results showed that the step response was good and the robust was satisfying. |
| Keywords: | carrier landing control system intelligent design |
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