飞行器合理传递参数的解法

本文基于矢量矩阵分析法,建立了含气动、结构和飞行参数及其偏量的数学模型,它可用来分析飞行器的合理传递参数。按此方法不仅可以同时调整若干设计参数,而且还可简化计算机辅助设计的程序。为选择合理传递参数,列出了设计参数的调整准则。 取用动态因子和转换因子,使所得方法对于正常式、鸭式、旋转弹翼式和弹道式导弹都是适用的。

SOLUTION TO RATIONAL TRANSFER PARAMETERS OF FLIGHT VEHICLE

A mathematic model involving the aerodynamic, structure and flight parameters and their deviations based on vectormatrix analysis is established in this paper, it can be used to analyse rational transfer parameters of vehicles. Not only several design parameters can be modified at the same time, but also computer aided design programming can be simplified by using the above calculation method. In order to choose rational transfer parameters, the adjusting criterions of design parameter are given here.By taking the dynamic factors and transform factors, the method presented here is suitable to normal, canard, controlwing and ballistic vehicles.