| 基于小扰动动力学模型的舰载机复飞决策系统研究 |
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| 引用本文： | 曲志刚,吴文海,秦肖臻.基于小扰动动力学模型的舰载机复飞决策系统研究[J].青岛大学学报(自然科学版),2010,23(4):52-56. |
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| 作者姓名： | 曲志刚 吴文海 秦肖臻 |
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| 作者单位： | [1]海军航空工程学院青岛分院,山东青岛266041 [2]华中科技大学,武汉430074 |
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| 摘 要： | 从提高舰载机着舰安全性出发,提出了满足着舰安全要求的复飞准则,对基于飞机小扰动动力学模型复飞决策系统的实现技术以及复飞边界计算方法进行了研究,并以国外某型飞机为例,利用matlab软件对复飞边界进行了计算,并对复飞过程进行了仿真验证,结果表明基于小扰动动力学模型的复飞决策方法切实可行。
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| 关 键 词： | 复飞决策系统 复飞准则 复飞区 |
Wave-Off Decision System Based on Smmall Disturbance Dynamics Model |
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| QU Zhi-gang,WU Wen-hai,QIN Xiao-zhen.Wave-Off Decision System Based on Smmall Disturbance Dynamics Model[J].Journal of Qingdao University(Natural Science Edition),2010,23(4):52-56. |
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| Authors: | QU Zhi-gang WU Wen-hai QIN Xiao-zhen |
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| Institution: | 1.Qingdao Branch,Naval Aeronautical and Astronautical University,Qingdao 266041,China;2.Huazhong University of Science and Technology,Wuhan 430074,China) |
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| Abstract: | The wave-off system is studied to improve the landing safety of the aircraft.In this paper the wave-off decision system is proposed based on the small disturbance dynamics model,To verify the effectiveness of the wave-off decision methods,the border of the wave-off area is calculated in a foreign aircraft with the method of matlab.Simulation results show the wave-off decision principle developed in this paper is feasible. |
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| Keywords: | wave-off decision system wave-off rule wave-off area |
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