A Simple Backstepping Control Method for Saucer-shaped Aircraft

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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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  -