The Design of Mini Quad-Rotor Unmanned Aerial Vehicle Control System

Abstract:

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In this paper we describe a small four-rotor UAV's autonomous flight control system. A comprehensive plan of flight control system was designed base on the remote control model aircraft for flight platform, and Completed with AVR microcontroller core flight control system software and hardware design. It including device type, hardware circuit design and software design. Preliminary study of the four rotor while the helicopter flight control program design, For the future to perform more complex tasks such as fixed-point flight, obstacle avoidance and coordination of multiple aircraft flying and so lay a foundation.

Info:

Periodical:

Advanced Materials Research (Volumes 383-390)

Edited by:

Wu Fan

Pages:

569-573

DOI:

10.4028/www.scientific.net/AMR.383-390.569

Citation:

Y. Zhao and J. X. Yang, "The Design of Mini Quad-Rotor Unmanned Aerial Vehicle Control System", Advanced Materials Research, Vols. 383-390, pp. 569-573, 2012

Online since:

November 2011

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Price:

$35.00

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