Sliding Mode Control Of Pitch Channel Nonlinear Model Of A Kind Of High Speed Vehicles Without Sign Function

DOI

10.2991/icence-16.2016.100How to use a DOI?

Keywords

Backstepping, Stability, Lyapunov function, Adaptive, Robustness

Abstract

A kind of Sliding mode 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 sliding mode design method, the main difference is that the sign function is not used and a kind of proportional control item is directly used to reduce the chattering phenomenon. 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  - Guangbin Wu
AU  - Guoqiang Liang
AU  - Zijian Lin
AU  - Junwei Lei
PY  - 2016/09
DA  - 2016/09
TI  - Sliding Mode Control Of Pitch Channel Nonlinear Model Of A Kind Of High Speed Vehicles Without Sign Function
BT  - Proceedings of the 2nd International Conference on Electronics, Network and Computer Engineering (ICENCE 2016)
PB  - Atlantis Press
SP  - 524
EP  - 527
SN  - 2352-538X
UR  - https://doi.org/10.2991/icence-16.2016.100
DO  - 10.2991/icence-16.2016.100
ID  - Wu2016/09
ER  -