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
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;
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
DOI :
10.1109/ISISE.2009.56