Suboptimal period design for a maneuvering missile to evade tracking filters

The engagement between an antiship missile and a ship’s defense system is investigated. The missile is equipped with proportional navigation guidance for homing in on its ship target. The ship’s defense system consists of a radar, an estimation system (the extended Kalman filter and the “jump filter...

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Bibliographic Details
Main Author: Lai, Lin-Ying
Other Authors: Aerospace and Ocean Engineering
Format: Others
Language:en_US
Published: Virginia Polytechnic Institute and State University 2015
Subjects:
Online Access:http://hdl.handle.net/10919/53564