Proceedings of the 2017 4th International Conference on Machinery, Materials and Computer (MACMC 2017)

A Tracking Differentiator Based Backstepping Control of Missile System

Authors
Wenguang Zhang, Lili Yang, Junwei Lei
Corresponding Author
Wenguang Zhang
Available Online January 2018.
DOI
10.2991/macmc-17.2018.132How to use a DOI?
Keywords
Tracking differentiator; stability; Backstepping; Missile; Control system
Abstract

To avoid the complex calculation of derivative in the backstepping design procedure, a novel kind of tracking differentiator was adopt to solve the derivative of ideal angle speed of the pitch channel missile system. Also, the ideal angle speed should be bounded or the stability of the system can not be guaranteed. And a Lyapunov function was chosen to prove the stability of the whole system. At last, the detailed numerical simulation was done to show the rightness and effectiveness of the proposed 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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Volume Title
Proceedings of the 2017 4th International Conference on Machinery, Materials and Computer (MACMC 2017)
Series
Advances in Engineering Research
Publication Date
January 2018
ISBN
978-94-6252-439-2
ISSN
2352-5401
DOI
10.2991/macmc-17.2018.132How to use a DOI?
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/).

Cite this article

TY  - CONF
AU  - Wenguang Zhang
AU  - Lili Yang
AU  - Junwei Lei
PY  - 2018/01
DA  - 2018/01
TI  - A Tracking Differentiator Based Backstepping Control of Missile System
BT  - Proceedings of the 2017 4th International Conference on Machinery, Materials and Computer (MACMC 2017)
PB  - Atlantis Press
SP  - 700
EP  - 703
SN  - 2352-5401
UR  - https://doi.org/10.2991/macmc-17.2018.132
DO  - 10.2991/macmc-17.2018.132
ID  - Zhang2018/01
ER  -