Simulation of open loop response of a kind of high speed aircraft with virtual flying conditions

DOI

10.2991/icmmita-15.2015.113How to use a DOI?

Keywords

aircraft; simulation; open loop; virtual flying; stability

Abstract

A kind of numerical simulation method is used to testify the open loop response of a kind high speed aircraft. Since the final aim is to the testify the rightness of the system model and its corresponding air coefficients, so virtual flying condition is set to make the system more simple and more easy to be stable so that the simulation can be last for a longer time, which is very important and difficult for high speed aircraft. The attack angle and elastic shape of the aircraft is set to be constant so the virtual flying is constructed and it is reasonable for the aircraft, so it is effective and valid to testify the system model.

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  - Junbo Chu
AU  - Aijun Zhou
AU  - Yuqiang Jin
PY  - 2015/11
DA  - 2015/11
TI  - Simulation of open loop response of a kind of high speed aircraft with virtual flying conditions
BT  - Proceedings of the 2015 3rd International Conference on Machinery, Materials and Information Technology Applications
PB  - Atlantis Press
SP  - 586
EP  - 589
SN  - 2352-538X
UR  - https://doi.org/10.2991/icmmita-15.2015.113
DO  - 10.2991/icmmita-15.2015.113
ID  - Chu2015/11
ER  -