基于小扰动动力学模型的舰载机复飞决策系统研究  

Wave-Off Decision System Based on Smmall Disturbance Dynamics Model

作　　者：曲志刚[1,2] 吴文海[1] 秦肖臻[2] 

机构地区：[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

出　　处：《青岛大学学报（自然科学版）》2010年第4期52-56,共5页Journal of Qingdao University(Natural Science Edition)

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。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.

关 键 词：复飞决策系统 复飞准则 复飞区 

分 类 号：V271.492[航空宇航科学与技术—飞行器设计]