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

DOI

10.2991/macmc-17.2018.64How to use a DOI?

Keywords

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

Abstract

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.

Copyright

© 2018, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Xiao-tian Wu
AU  - Xing Wang
AU  - Jin-heng Yang
AU  - Xiang Zhang
PY  - 2018/01
DA  - 2018/01
TI  - Air-to-Air Missile Tracking and Guidance Law Identification Based on CKF
BT  - Proceedings of the 2017 4th International Conference on Machinery, Materials and Computer (MACMC 2017)
PB  - Atlantis Press
SP  - 320
EP  - 327
SN  - 2352-5401
UR  - https://doi.org/10.2991/macmc-17.2018.64
DO  - 10.2991/macmc-17.2018.64
ID  - Wu2018/01
ER  -