Unmanned Aircraft Preliminary Design and Pneumatic Gauge
- 10.2991/icmcm-16.2016.67How to use a DOI?
- Unmanned aerial vehicle (uav); preliminary design; aerodynamic estimation
The UAV found rapidly, it has the characteristics of manned aircraft do not have, such as cost, no risk of human life, and increasing people's attention. Unmanned aerial vehicle aerodynamic design, it affects the entire airplane aerodynamic characteristics and flight performance, aircraft preliminary design the aerodynamic layout, ensure the success of the program. This article is intended primarily for unmanned aerial vehicle features preliminary selection of a number of programs ,including the wings , fuselage, tail, control parameter selection for main parts such as control surface, and the overall design of the program to be a preliminary discussion, unmanned aerial vehicles and providing a theoretical reference model plane enthusiasts , also design their own little UAV theory laid the foundation of the future.
- © 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/).
Cite this article
TY - CONF AU - Xiujuan Liu AU - Guangxu Ren AU - Chunguang Wang PY - 2016/12 DA - 2016/12 TI - Unmanned Aircraft Preliminary Design and Pneumatic Gauge BT - Proceedings of the 2016 7th International Conference on Mechatronics, Control and Materials (ICMCM 2016) PB - Atlantis Press SP - 331 EP - 336 SN - 2352-5401 UR - https://doi.org/10.2991/icmcm-16.2016.67 DO - 10.2991/icmcm-16.2016.67 ID - Liu2016/12 ER -