The open loop response analysis of duck wing with trust resistance balance and constant elasticity
- 10.2991/icmmita-15.2015.116How to use a DOI?
- open loop; stability; resistance; balance; duck wing
A kind of virtual flying condition is assumed that the trust and resistance is the same that can keep the force balance during the flying process of high speed aircraft. The main function of this virtual assumption is that it can the unstable open loop aircraft fly a longer time so more date can be gotten and the duck wing response or effect can be analyzed more clearly. So it is a new method and it is effective and meaningful for the open loop dynamic analysis especially for high speed unstable control objects.
- © 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 - Haibo Wang AU - Aijun Zhou AU - Junbo Chu AU - Tianwei Li AU - Guoqiang Liang PY - 2015/11 DA - 2015/11 TI - The open loop response analysis of duck wing with trust resistance balance and constant elasticity BT - Proceedings of the 2015 3rd International Conference on Machinery, Materials and Information Technology Applications PB - Atlantis Press SP - 600 EP - 604 SN - 2352-538X UR - https://doi.org/10.2991/icmmita-15.2015.116 DO - 10.2991/icmmita-15.2015.116 ID - Wang2015/11 ER -