Air-to-Air Missile Tracking and Guidance Law Identification Based on CKF

被引：0

作者：

Wu Xiao-tian ^{[1
]}

Yang Jin-heng ^{[1
]}

Wang Xing ^{[1
]}

Zhang Xiang ^{[1
]}

机构：

[1] Air Force Engn Univ, Aeronaut & Astronaut Engn Coll, Xian, Shaanxi, Peoples R China

来源：

PROCEEDINGS OF THE 2017 4TH INTERNATIONAL CONFERENCE ON MACHINERY, MATERIALS AND COMPUTER (MACMC 2017) | 2017年 / 150卷

关键词：

guidane law identification; cubature Kalman filter; augmented proportional navigation; missile tracking;

D O I：

暂无

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

An air-to-air missile tracking and guidance law identification method based on CKF is proposed. A precise air-to-air missile model is constructed with drag force taken into consideration. With CKF method and preprocessing, guidance law filter is designed for missile tracking and estimation of guidance law, gravity compensation and drag constant. Simulation results indicate the rapidness and accuracy of this method.

引用

页码：320 / 327

页数：8