The Design of the Uav Ground Station Controller

DOI

10.2991/icoss-17.2017.7How to use a DOI?

Keywords

UAV;Controller;Independent

Abstract

Take-off and landing UAV need through landing the manual control of the controller on the ground, landing on the ground controller design decides the security and reliability of the aircraft during take-off and landing. Because of the complexity of the tilt rotor machine body structure, the number on the steering gear and its control system is numerous, channel number is less, while the ground controller and a control area small, low accuracy of shortcomings, cannot be used to direct control of high precision, more steering gear rotor machine. Therefore, independent design accord with the characteristics of rotated rotor craft landing on the ground controller is very be necessary.

Copyright

© 2017, 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  - Chong Zhao
AU  - Ning Wang
PY  - 2017/04
DA  - 2017/04
TI  - The Design of the Uav Ground Station Controller
BT  - Proceedings of the 2017 International Conference on Society Science (ICoSS 2017)
PB  - Atlantis Press
SP  - 36
EP  - 39
SN  - 2352-5398
UR  - https://doi.org/10.2991/icoss-17.2017.7
DO  - 10.2991/icoss-17.2017.7
ID  - Zhao2017/04
ER  -