Tracking air-to-air missile using proportional navigation model with genetic algorithm particle filter

DOI10.1155/2016/3921608zbMath1400.93301OpenAlexW2298317882WikidataQ59131210 ScholiaQ59131210MaRDI QIDQ1793088

Chenwei Ruan, Zhongliang Zhou, Hongqiang Liu, Lei Yu

Publication date: 12 October 2018

Published in: Mathematical Problems in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1155/2016/3921608

Mathematics Subject Classification ID

Filtering in stochastic control theory (93E11) Kinematics of a particle (70B05)

Cites Work

• Optimal planar evasive aircraft maneuvers against proportional navigation missiles
• Optimal estimation and Cramér-Rao bounds for partial non-Gaussian state space models

This page was built for publication: Tracking air-to-air missile using proportional navigation model with genetic algorithm particle filter