The research of open loop characteristics of lifting wing based on constant speed constant elastic cases
- https://doi.org/10.2991/icmmita-15.2015.118How to use a DOI?
- lift wing; open loop; stability; aircraft; actuator effect;
The open loop response of lift wing is researched based on a kind of high speed vehicle model which is released by America air force research center. Since the speed of aircraft is too high, so its open loop response is unstable, which is difficult to do open loop actuator analysis with traditional method. In this paper, a kind of virtual flying conditions is assumed to make the simulation can last longer which can get more data to analysis the actuator effect, so the speed and elastic shape are considered to be constant. With the numerical simulation technology, the unstable open loop characteristics are recorded and analyzed.
- © 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 - Guoqiang Liang AU - Di Liu PY - 2015/11 DA - 2015/11 TI - The research of open loop characteristics of lifting wing based on constant speed constant elastic cases BT - Proceedings of the 2015 3rd International Conference on Machinery, Materials and Information Technology Applications PB - Atlantis Press SP - 610 EP - 613 SN - 2352-538X UR - https://doi.org/10.2991/icmmita-15.2015.118 DO - https://doi.org/10.2991/icmmita-15.2015.118 ID - Liang2015/11 ER -