A small UAV deviation control roll research

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/).

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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  -