Proceedings of the 3rd International Conference on Mechanical Engineering and Intelligent Systems (ICMEIS 2015)

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Modeling and PID Control of Height Loop of a Kind of Airship Vehicle

Authors
Yidong Wang, Junwei Lei, Lingling Wang
Corresponding Author
Yidong Wang
Available Online August 2015.
DOI
10.2991/icmeis-15.2015.35How to use a DOI?
Keywords
airship; pitch channel; adaptive; PID; stability
Abstract

The airship modeling is the basic of the airship control problem. Based on airship modeling of pitching channel of airship and its nonlinear model, an traditional PID altitude controller of airship is designed. Finally, this control method is proved to be effective by numerical simulation.

Copyright
© 2015, 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 3rd International Conference on Mechanical Engineering and Intelligent Systems (ICMEIS 2015)
Series
Advances in Engineering Research
Publication Date
August 2015
ISBN
978-94-62520-98-1
ISSN
2352-5401
DOI
10.2991/icmeis-15.2015.35How to use a DOI?
Copyright
© 2015, 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

risenwbib
TY  - CONF
AU  - Yidong Wang
AU  - Junwei Lei
AU  - Lingling Wang
PY  - 2015/08
DA  - 2015/08
TI  - Modeling and PID Control of Height Loop of a Kind of Airship Vehicle
BT  - Proceedings of the 3rd International Conference on Mechanical Engineering and Intelligent Systems (ICMEIS 2015)
PB  - Atlantis Press
SP  - 180
EP  - 184
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmeis-15.2015.35
DO  - 10.2991/icmeis-15.2015.35
ID  - Wang2015/08
ER  -