The open loop response analysis of duck wing with trust resistance balance and constant elasticity

DOI

10.2991/icmmita-15.2015.116How to use a DOI?

Keywords

open loop; stability; resistance; balance; duck wing

Abstract

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.

Copyright

© 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/).

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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  -