Aircraft 6-DOF Modular Modeling Based on MATLAB Simulink

DOI

10.2991/iccia-17.2017.176How to use a DOI?

Keywords

aircraft, 6-DOF modeling, Matlab Simulink, modular principle.

Abstract

Aircraft is playing an increasing important role in aerospace field. To analysis the property of an aircraft, a model and simulation which is accurate and succinate is necessary. In this paper, 6DOF aircraft full motion equations are derived on the basis of newton's second law in the condition of plane earth hypothesis and rigid body hypothesis. Matlab Simulink was adopted to modeling simulation in which modular principle was employed. And the simulation results were reliable though the qualitative analysis.

Copyright

© 2017, 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  - Huixian Wang
AU  - Dongli Ma
PY  - 2016/07
DA  - 2016/07
TI  - Aircraft 6-DOF Modular Modeling Based on MATLAB Simulink
BT  - Proceedings of the 2nd International Conference on Computer Engineering, Information Science & Application Technology (ICCIA 2017)
PB  - Atlantis Press
SP  - 1002
EP  - 1005
SN  - 2352-538X
UR  - https://doi.org/10.2991/iccia-17.2017.176
DO  - 10.2991/iccia-17.2017.176
ID  - Wang2016/07
ER  -