The Cruise Missile Guidance and Control System Design and Simulation Based on the Integral Sliding Mode Control

DOI

10.2991/iceep-18.2018.320How to use a DOI?

Keywords

Integral Sliding Mode Control, Cruise Missile, Guidance and Control System, MATLAB

Abstract

As a long-range precision guided high-tech weaponry, the cruise missiles have the advantages of strong penetration prevention capability, diversification of tactical use, and economical efficiency etc. After the Gulf War, many countries competed for research and develop the cruise missile. In this paper, the cruise missile’s guidance system and control system are designed separately. The proportional guidance method is used as the guidance system guidance method. The PID control and integral sliding mode control are used to design the controller. The simulation results show that the integral sliding mode control can effectively improve the guidance accuracy and rapid strike ability of cruise missiles, and provide a new method for missile control.

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  - Xipeng Liu
PY  - 2018/09
DA  - 2018/09
TI  - The Cruise Missile Guidance and Control System Design and Simulation Based on the Integral Sliding Mode Control
BT  - Proceedings of the 2018 7th International Conference on Energy and Environmental Protection (ICEEP 2018)
PB  - Atlantis Press
SP  - 1760
EP  - 1764
SN  - 2352-5401
UR  - https://doi.org/10.2991/iceep-18.2018.320
DO  - 10.2991/iceep-18.2018.320
ID  - Liu2018/09
ER  -