DocumentCode
2072945
Title
Flight Simulation Testbed of Unmanned Helicopter
Author
Wu, Jiande ; Feng, Ting ; Fan, Yugang
Author_Institution
Fac. of Inf. Eng. & Autom., Kunming Univ. of Sci. & Technol., Kunming, China
fYear
2009
fDate
26-28 Dec. 2009
Firstpage
497
Lastpage
499
Abstract
This paper designed a flight simulation testbed of unmanned helicopter. This testbed has the advantage of simple structure, easy implement, low cost, convenient movement and so on. It is suitable for various flight test of mini-unmanned helicopter. It provides attitude needed by unmanned helicopter, such as pitch, yaw, roll and so on, to ensure that unmanned helicopter can be free flight within a certain range. Making use of the testbed can reproduce the actual flight of unmanned helicopter under laboratory conditions, and can be very convenient for attitude control, flight control, navigation and other scientific researches; accordingly, it ensures the security of flight test for unmanned helicopter.
Keywords
aerospace simulation; attitude control; helicopters; mobile robots; remotely operated vehicles; attitude control; flight control; flight simulation testbed; mini unmanned helicopter; Aerospace engineering; Aerospace simulation; Computational modeling; Costs; Design engineering; Helicopters; Paper technology; Vehicle crash testing; Winches; Wire; flight simulation; testbed; unmanned helicopter;
fLanguage
English
Publisher
ieee
Conference_Titel
Information Science and Engineering (ISISE), 2009 Second International Symposium on
Conference_Location
Shanghai
Print_ISBN
978-1-4244-6325-1
Electronic_ISBN
978-1-4244-6326-8
Type
conf
DOI
10.1109/ISISE.2009.56
Filename
5447291
Link To Document