Proceedings of 2016 International Conference on Modeling, Simulation and Optimization Technologies and Applications (MSOTA2016)

Overview of Missile Control Method

Authors
Chen Li, Jingyu Yang, Qing Wang, Zhijie Zhang, Hailong Wang, Jiahe Sun, Tianfen Mo, Shiwei Sun
Corresponding Author
Chen Li
Available Online December 2016.
DOI
10.2991/msota-16.2016.75How to use a DOI?
Keywords
classical guidance law; missile control method; modern guidance law
Abstract

The classical guidance law and the modern guidance law in the missile control system are introduced comparatively comprehensive. Firstly, the classical guidance law is introduced; Then the guidance law based on modern control theory is introduced emphatically, and the advantages and disadvantages of these guidance laws and development trend are analyzed. Finally, several kinds of composite control methods are expounded briefly.

Copyright
© 2017, 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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Volume Title
Proceedings of 2016 International Conference on Modeling, Simulation and Optimization Technologies and Applications (MSOTA2016)
Series
Advances in Computer Science Research
Publication Date
December 2016
ISBN
10.2991/msota-16.2016.75
ISSN
2352-538X
DOI
10.2991/msota-16.2016.75How to use a DOI?
Copyright
© 2017, 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/).

Cite this article

TY  - CONF
AU  - Chen Li
AU  - Jingyu Yang
AU  - Qing Wang
AU  - Zhijie Zhang
AU  - Hailong Wang
AU  - Jiahe Sun
AU  - Tianfen Mo
AU  - Shiwei Sun
PY  - 2016/12
DA  - 2016/12
TI  - Overview of Missile Control Method
BT  - Proceedings of 2016 International Conference on Modeling, Simulation and Optimization Technologies and Applications (MSOTA2016)
PB  - Atlantis Press
SP  - 348
EP  - 350
SN  - 2352-538X
UR  - https://doi.org/10.2991/msota-16.2016.75
DO  - 10.2991/msota-16.2016.75
ID  - Li2016/12
ER  -