首页 | 本学科首页   官方微博 | 高级检索  
     


Missile Guidance Based on Kalman Filter Estimation of Target Maneuver
Authors:Tang   Y.M. Borrie   J.A.
Affiliation:Luoyang Dynamic Institute Chinese Aeronautical Establishment People's Republic of China;
Abstract:
A fourth-order extended Kalman filter is developed to estimate target maneuvers, and a guidance law using these estimates is implemented.
Keywords:
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号