Design of optoelectronic pod system for Z-3 unmanned helicopter

DOI

10.2991/aest-16.2016.138How to use a DOI?

Keywords

optoelectronic pod; Z-3 unmanned helicopterimage; stabilization; demonstration flight.

Abstract

Aerial survey of geological disasters have higher demand to the stability of the payload, especially with a payload of optoelectronic pod can absorb the unmanned helicopter attitude and vibration and compensates the attitude angle change. Keeping the payload optical axis perpendicular is to the horizontal plane. Based on the analysis of posture change and vibration frequency, optoelectronic pod system that is based on TMS320f2812 as the main controller, adopting the closed-loop control system. The results of field demonstration flight indicate that the optoelectronic pod compensates the attitude angle change due to the unmanned helicopter attitude and vibration. The high quality images which were obtained by demonstration flight satisfy low-altitude digital aerophotogrammetry.

Copyright

© 2016, 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)

TY  - CONF
AU  - Yingping Guo
AU  - Jinsheng Yang
AU  - Xuqing Wang
PY  - 2016/11
DA  - 2016/11
TI  - Design of optoelectronic pod system for Z-3 unmanned helicopter
BT  - Proceedings of the 2016 International Conference on Advanced Electronic Science and Technology (AEST 2016)
PB  - Atlantis Press
SP  - 1028
EP  - 1035
SN  - 1951-6851
UR  - https://doi.org/10.2991/aest-16.2016.138
DO  - 10.2991/aest-16.2016.138
ID  - Guo2016/11
ER  -