Aspects Regarding Software Simulation of a Quadcopter Dynamics

Article Preview

Abstract:

The development of unmanned aircraft (UAV) capable of vertical takeoff and landing maneuver (VTOL) and hovering flight is an area of interest for the military and civilian research component. This paper focuses on a quadrotor type miniUAV, and proposes a solution to implement a mathematical model for a quadrotor used in a simulation environment Matlab (Simulink).

You might also be interested in these eBooks

Info:

Periodical:

Pages:

62-67

Citation:

Online since:

July 2013

Keywords:

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2013 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Bouabdallah, S. Design and control of quadrotors with application to autonomous flying. Master's thesis, ÉCOLE POLYTECHNIQUE FÉDÉRALE DE LAUSANNE (2007)

Google Scholar

[2] Turoczi A. Flight Control Systems of an Experimental Unmanned Quad-Rotor Helicopter, 10th International Symposium of Hungarian Researchers on Computational Intelligence and Informatics

Google Scholar

[3] Information on www.mathworks.com.

Google Scholar

[4] Information on www.asl.ethz.ch

Google Scholar

[5] Beard R.W., Quadrotor Dynamics and Control, Brigham Young University, (2008)

Google Scholar

[6] Nise, N. S., Control Systems Engineering 6th edition, John Wiley & Sons,Inc.

Google Scholar