Proceedings of the 2015 3rd International Conference on Machinery, Materials and Information Technology Applications

The tracking control of hypersonic aircraft attack angle based on the coupling of elastic form and engines

Authors
Junwei Lei, Yuliang Chen
Corresponding Author
Junwei Lei
Available Online November 2015.
DOI
https://doi.org/10.2991/icmmita-15.2015.117How to use a DOI?
Keywords
hypersonic aircraft; stability; control; free flying; numerical simulation
Abstract

A kind of attack angle tracking controller with a former similar to PID control is proposed based on the pitch channel model of hypersonic aircraft released by America air force research center. Also the speed of the aircraft is controlled to tracking to a constant, which will make the system more stable and more easy to design a controller. At last, detailed numerical simulation is done to testify the rightness of the proposed method and the rightness of the hypersonic aircraft.

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 2015 3rd International Conference on Machinery, Materials and Information Technology Applications
Series
Advances in Computer Science Research
Publication Date
November 2015
ISBN
978-94-6252-120-9
ISSN
2352-538X
DOI
https://doi.org/10.2991/icmmita-15.2015.117How 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

TY  - CONF
AU  - Junwei Lei
AU  - Yuliang Chen
PY  - 2015/11
DA  - 2015/11
TI  - The tracking control of hypersonic aircraft attack angle based on the coupling of elastic form and engines
BT  - Proceedings of the 2015 3rd International Conference on Machinery, Materials and Information Technology Applications
PB  - Atlantis Press
SP  - 605
EP  - 609
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmmita-15.2015.117
DO  - https://doi.org/10.2991/icmmita-15.2015.117
ID  - Lei2015/11
ER  -