DETERMINING THE PARAMETERS OF MATHEMATICAL-MODELS OF AIRCRAFT BY THE DISCRETE-CONTINUOUS IDENTIFICATION METHOD

被引:0
|
作者
BANYKIN, IF
机构
来源
关键词
D O I
暂无
中图分类号
TP301 [理论、方法];
学科分类号
081202 ;
摘要
A series of various algorithms for the parameteric identification of the aerodynamic and inertia-mass data of aircraft is considered. Means for solving the basic identification problems when exact information about the aircraft parameters which correspond to their a-priori values is available, as well as when partial indeterminacy is present in the simultaneous knowledge of the aerodynamics and the inertia-mass characteristics, are proposed. The basic premises of the paper are illustrated by the results of numerical simulation.
引用
收藏
页码:46 / 55
页数:10
相关论文
共 50 条