DocumentCode
2809814
Title
Flight control system design for miniature unmmaned helicopter based on PowerPC
Author
Wang, Qiang
Author_Institution
Seventh Res. Div., Beihang Univ., Beijing, China
fYear
2011
fDate
15-17 July 2011
Firstpage
4088
Lastpage
4091
Abstract
This paper presents a novel design of flight control system for miniature unmanned helicopter based on PowerPC. The structure is compact, multi-serial communication is credible, and the interface is flexible. An important design about security which makes change between telecontrol device and flight control system is offered. At the end of the paper, the result of Hardware in the loop simulation experimentation is given, and the result shows the flight control system is multifunctional and reliable.
Keywords
aerospace computing; aircraft control; control engineering computing; helicopters; microrobots; mobile robots; remotely operated vehicles; PowerPC; flight control system design; hardware in the loop simulation experimentation; miniature unmanned helicopter; multiserial communication; telecontrol device; Aerospace control; Control systems; Hardware; Helicopters; Manufacturing; Navigation; Pulse width modulation; PowverPC; RTLinux; fight control system; unmanned helicopter;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechanic Automation and Control Engineering (MACE), 2011 Second International Conference on
Conference_Location
Hohhot
Print_ISBN
978-1-4244-9436-1
Type
conf
DOI
10.1109/MACE.2011.5987901
Filename
5987901
Link To Document