Research on free flying of high speed aircraft without control

DOI

10.2991/icmmita-15.2015.109How to use a DOI?

Keywords

aircraft; stability; control; free flying; numerical simulation

Abstract

The research is based on a kind of pitch channel hypersonic aircraft model built is released by USA air force, adopting the digital simulation to verify the basic free flight state preliminarily. The difference of the stability and divergent could get observation through the simulation result between hypersonic aircraft’s attitude and attack angle and the traditional low supersonic aircraft. The research is aimed at evaluate the rationality of models, and do the preliminary analysis of the dynamic characteristics of hypersonic aircraft.

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  - Aijun Zhou
AU  - Haibo Wang
AU  - Junbo Chu
AU  - Tianwei Li
AU  - Guoqiang Liang
PY  - 2015/11
DA  - 2015/11
TI  - Research on free flying of high speed aircraft without control
BT  - Proceedings of the 2015 3rd International Conference on Machinery, Materials and Information Technology Applications
PB  - Atlantis Press
SP  - 568
EP  - 571
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmmita-15.2015.109
DO  - 10.2991/icmmita-15.2015.109
ID  - Zhou2015/11
ER  -