DocumentCode
2112410
Title
Modeing of a helicopter with an under-slung load system
Author
Thanapalan, Kary ; Wong, Toh Ming
Author_Institution
Fac. of Eng. Sci., Univ. Coll. London, London, UK
fYear
2010
fDate
29-31 July 2010
Firstpage
1451
Lastpage
1456
Abstract
This paper considers modeling and simulation study of a helicopter with an under-slung external load system. Mathematical models of a single main rotor helicopter and an under-slung load are presented in this paper. Considering the two models, a mathematical model for a helicopter carrying an under-slung load is obtained. The combined system model can be used for stability analysis and controller development to improve system performance.
Keywords
helicopters; loading; mathematical analysis; stability; controller development; helicopter modeing; mathematical models; single main rotor helicopter; stability analysis; under slung load system; Aerodynamics; Equations; Helicopters; Load modeling; Mathematical model; Rotors; Stability analysis; Dynamic System; Mathematical Model; Modeling; Stability;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (CCC), 2010 29th Chinese
Conference_Location
Beijing
Print_ISBN
978-1-4244-6263-6
Type
conf
Filename
5573621
Link To Document