Proceedings of the 2016 4th International Conference on Machinery, Materials and Computing Technology

A kind of differential sliding mode controller design for pitch channel simplified model of hypersonic aircraft

Authors
Guoqiang Liang, Guangbin Wu
Corresponding Author
Guoqiang Liang
Available Online March 2016.
DOI
https://doi.org/10.2991/icmmct-16.2016.11How to use a DOI?
Keywords
hypersonic aircraft; stability; control; free flying; numerical simulation
Abstract
A kind of differential type sliding mode control law was proposed to improve the robustness of a kind of simplified pitch channel model of hypersonic aircraft which is widely discussed recently. The advantage of sliding mode control is that it has differential item which can provide a special damping for flying system. With the increasing of damping ratio, the stable margin of the who flying system can be greatly increased. Also, to prove the stability of the whole system, two Lyapunov functions were constructed and all signals of close system are proved to be stable. At last, detailed simulation was done to testify the effectiveness of the proposed method.
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This is an open access article distributed under the CC BY-NC license.

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Volume Title
Proceedings of the 2016 4th International Conference on Machinery, Materials and Computing Technology
Series
Advances in Engineering Research
Publication Date
March 2016
ISBN
978-94-6252-165-0
ISSN
2352-5401
DOI
https://doi.org/10.2991/icmmct-16.2016.11How to use a DOI?
Open Access
This is an open access article distributed under the CC BY-NC license.

Cite this article

TY  - CONF
AU  - Guoqiang Liang
AU  - Guangbin Wu
PY  - 2016/03
DA  - 2016/03
TI  - A kind of differential sliding mode controller design for pitch channel simplified model of hypersonic aircraft
BT  - Proceedings of the 2016 4th International Conference on Machinery, Materials and Computing Technology
PB  - Atlantis Press
SP  - 53
EP  - 58
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmmct-16.2016.11
DO  - https://doi.org/10.2991/icmmct-16.2016.11
ID  - Liang2016/03
ER  -