Backstepping Controller Design for a Kind of High Speed Vehicle

DOI

10.2991/icmmbe-16.2016.43How to use a DOI?

Keywords

Backstepping, Stability, Lyapunov function, Adaptive, Robustness

Abstract

A kind of backstepping controller is designed for a kind of pitch channel model of hypersonic aircrafts. The main task is to realize attack angle tracking of hypersonic aircrafts. Compared with traditional linear design method, the main difference is that the nonlinear model is directly used in the design process by adopting a Lyapunov function method to guarantee the stability of the whole system. At last, detailed simulations are done to show the rightness of the proposed method.

Copyright

© 2016, 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  - Wenguang Zhang
AU  - Zijian Lin
AU  - Junwei Lei
PY  - 2016/09
DA  - 2016/09
TI  - Backstepping Controller Design for a Kind of High Speed Vehicle
BT  - Proceedings of the6th International Conference on Mechatronics, Materials, Biotechnology and Environment (ICMMBE 2016)
PB  - Atlantis Press
SP  - 221
EP  - 224
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmmbe-16.2016.43
DO  - 10.2991/icmmbe-16.2016.43
ID  - Zhang2016/09
ER  -