Stability analysis of radome error and calibration using neural networks

被引：13

作者：

Lin, CL ^{[1
]}

机构：

[1] Feng Chia Univ, Inst Automat Control Engn, Taichung 40724, Taiwan

来源：

IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | 2001年 / 37卷 / 04期

关键词：

D O I：

10.1109/7.976979

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Theoretical and numerical simulation analyses for the radome refraction effect on stability and Induced miss distance of missiles guided by proportional navigation are presented. Quantitative stability conditions am derived with respect to linear and nonlinear radome error. A novel neural network compensation scheme for radome error is also presented. It is shown that the proposed neural compensator can effectively reduce the influence resulting from radome error. Preliminary results Indicate encouraging improvement in the miss distance and magnitude of the acceleration command.

引用

页码：1442 / 1450

页数：9

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