DocumentCode
1804774
Title
Design and implementation of flight control system software for unmanned helicopter
Author
Wu, Yukang ; Hu, Fei ; An, Jie
Author_Institution
Sch. of Software, Shanghai Jiao Tong Univ., Shanghai, China
Volume
4
fYear
2011
fDate
24-26 Dec. 2011
Firstpage
2196
Lastpage
2200
Abstract
In this paper, we address the design of software that achieves stable, reliable feather for an unmanned helicopter´s flight control system. According to the logical view and data view are given to the flight control system, the method of software architecture is researched. At last, the results of this work are illustrated by experiment, showing that the software base on this architecture has well stability and reliability.
Keywords
aircraft control; autonomous aerial vehicles; control engineering computing; helicopters; software architecture; software reliability; data view; flight control system software design; flight control system software implementation; logical view; software architecture; software reliability; software stability; unmanned helicopter; Control systems; Educational institutions; Global Positioning System; Hardware; Power capacitors; Reliability;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer Science and Network Technology (ICCSNT), 2011 International Conference on
Conference_Location
Harbin
Print_ISBN
978-1-4577-1586-0
Type
conf
DOI
10.1109/ICCSNT.2011.6182412
Filename
6182412
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