空战模拟器导弹火控工作式推导研究  

Study on missile fire control formula for air combat simulator

作　　者：胡朝晖[1] 汪凯[1] 车奇 李东文 

机构地区：[1]空军工程大学工程学院,陕西西安710038 [2]空军驻深圳蛇口地区军事代表室,广东深圳518000

出　　处：《电光与控制》2005年第6期63-65,共3页Electronics Optics & Control

摘　　要：为了求解空战模拟器上导弹火控工作式,建立了空空导弹发射区的计算模型,根据拟合导弹火控工作式的要求,计算了空空导弹发射区离散边界点,并采用多元非线性回归方法进行数学拟合,进而求得空战模拟器上导弹火控工作式。In order to obtain the missile fire control formula of Air Combat Simulator, models of air to air missile launching area are built in this paper. The discrete points of the missile launching area border are calculated out according to the requirement fire control formula fitting. Polynomial nonlinear regression, i.e., the Gauss ＇ Newton nonlinear least - squares method is used for data fitting, thus the missile fire control formula of air combat simulator is obtained.

关 键 词：空战模拟器 导弹火控工作式 非线性回归分析 

分 类 号：V211.78[航空宇航科学与技术—航空宇航推进理论与工程]