The establishment and Simulation of the dynamic model of the Four rotor aircraft

DOI

10.2991/ameii-16.2016.72How to use a DOI?

Keywords

Four rotor aircraft, Dynamic model, matlab Simulink, Simulation analysis.

Abstract

With the development of space technology and mature, four rotor aircraft with its low cost, high performance, unique structure and flight mode and other characteristics, are widely used in military and civil fields. According to the basic characteristics of four rotor aircraft prototype and flight characteristics, build up the dynamic and power system dynamics model. First the assumptions of the model, and analysis of the stress, dynamic model of the four rotor aircraft by the laws of physics. The simulation model was established in the MATLAB Simulink environment. The analysis of the simulation results, the model is verified the feasibility and validity of the model can be obtained, through the design of the control method, for the future spacecraft attitude solution to lay a good foundation work. This paper proposes a method of establishing a four rotor aircraft model, provides the reference for the further study of the four rotor flight system.

Copyright

© 2016, 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  - Wei Wu
AU  - Kai Fan Zhao
AU  - Qiang Wang
PY  - 2016/04
DA  - 2016/04
TI  - The establishment and Simulation of the dynamic model of the Four rotor aircraft
BT  - Proceedings of the 2nd International Conference on Advances in Mechanical Engineering and Industrial Informatics (AMEII 2016)
PB  - Atlantis Press
SP  - 352
EP  - 357
SN  - 2352-5401
UR  - https://doi.org/10.2991/ameii-16.2016.72
DO  - 10.2991/ameii-16.2016.72
ID  - Wu2016/04
ER  -