Proceedings of the 2017 5th International Conference on Machinery, Materials and Computing Technology (ICMMCT 2017)

A Simple Backstepping Control Method for Saucer-shaped Aircraft

Authors
YuLiang Chen, HuaLi Wu, LiLi Yang, Junwei Lei
Corresponding Author
YuLiang Chen
Available Online April 2017.
DOI
10.2991/icmmct-17.2017.169How to use a DOI?
Keywords
Backstepping Control; Saucer-shaped Aircraft, Stability, Lyapunov function
Abstract

In this paper, a simple backstepping control method is designed for a class of simplified linear model of saucer-shaped aircraft. This method can solve the non-minimum phase problem for the control of the aircraft by means of matching the two gains. The advantage of this method is that there is no need to use integral control to obtain better control precision, thus reducing the complexity of the control algorithm. The effectiveness of the proposed method is verified by detailed simulation analysis.

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 the 2017 5th International Conference on Machinery, Materials and Computing Technology (ICMMCT 2017)
Series
Advances in Engineering Research
Publication Date
April 2017
ISBN
978-94-6252-318-0
ISSN
2352-5401
DOI
10.2991/icmmct-17.2017.169How 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  - YuLiang Chen
AU  - HuaLi Wu
AU  - LiLi Yang
AU  - Junwei Lei
PY  - 2017/04
DA  - 2017/04
TI  - A Simple Backstepping Control Method for Saucer-shaped Aircraft
BT  - Proceedings of the 2017 5th International Conference on Machinery, Materials and Computing Technology (ICMMCT 2017)
PB  - Atlantis Press
SP  - 841
EP  - 844
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmmct-17.2017.169
DO  - 10.2991/icmmct-17.2017.169
ID  - Chen2017/04
ER  -