Proceedings of the 2015 6th International Conference on Manufacturing Science and Engineering

A small UAV deviation control roll research

Authors
Tianxiang Hu
Corresponding Author
Tianxiang Hu
Available Online December 2015.
DOI
10.2991/icmse-15.2015.1How to use a DOI?
Keywords
UAV; Roll; Flying control; Rectify deviation
Abstract

This paper according to the small UAV structure characteristics, the taxiing control structure and control law design are studied and proposed front wheel and rudder deviation control scheme and control structure, analysis, including the front landing gear, pavement condition, brake system, wind and other factors for correcting deviation control effect influence, based on take-off and landing and taxiing deviation control take-off characteristics, design the taxiing test scheme.

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/).

Download article (PDF)

Volume Title
Proceedings of the 2015 6th International Conference on Manufacturing Science and Engineering
Series
Advances in Engineering Research
Publication Date
December 2015
ISBN
10.2991/icmse-15.2015.1
ISSN
2352-5401
DOI
10.2991/icmse-15.2015.1How 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  - Tianxiang Hu
PY  - 2015/12
DA  - 2015/12
TI  - A small UAV deviation control roll research
BT  - Proceedings of the 2015 6th International Conference on Manufacturing Science and Engineering
PB  - Atlantis Press
SP  - 1
EP  - 7
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmse-15.2015.1
DO  - 10.2991/icmse-15.2015.1
ID  - Hu2015/12
ER  -