Design of 3-Dimensional Discrete Sliding Mode Guidance Law Based on ESO

DOI

10.2991/icectt-15.2015.3How to use a DOI?

Keywords

3-Dimensional space, guidance laws, discrete sliding mode, ESO

Abstract

In the paper ,a new approach to design discrete sliding mode guidance laws is presented based on the target-missile relative motion equation in three-dimensional space. The paper also proposes a new method to estimate the real-time target acceleration through the Extended State Observer. Finally, by mathematical simulation, the design significantly reduces system chattering caused by the variable structure control and has a strong robustness for hitting the maneuvering target.

Copyright

© 2015, 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/).

Download article (PDF)

TY  - CONF
AU  - Nuan Wen
AU  - Zhenghua Liu
AU  - Le Chang
PY  - 2015/11
DA  - 2015/11
TI  - Design of 3-Dimensional Discrete Sliding Mode Guidance Law Based on ESO
BT  - Proceedings of the 2015 International Conference on Electromechanical Control Technology and Transportation
PB  - Atlantis Press
SP  - 14
EP  - 17
SN  - 2352-5401
UR  - https://doi.org/10.2991/icectt-15.2015.3
DO  - 10.2991/icectt-15.2015.3
ID  - Wen2015/11
ER  -