DocumentCode
700710
Title
A toy more difficult to control than the real thing
Author
Mullhaupt, P. ; Srinivasan, B. ; Levine, J. ; Bonvin, D.
Author_Institution
Inst. d´Autom., Ecole Polytech. Fed. de Lausanne, Lausanne, Switzerland
fYear
1997
fDate
1-7 July 1997
Firstpage
1652
Lastpage
1657
Abstract
Standard helicopters use the propeller angle to alter the aerodynamic force and have been shown to be feedback linearizable with the pitch, yaw and roll angles being the flat outputs. In this work, a-two-degree-of-freedom, laboratory-scale helicopter-like system (termed the toycopter), where the aerodynamic force is manipulated using the propeller speed, is considered. For such a system the yaw and pitch angles are not flat outputs contrarily of the real helicopters. Moreover, the system does not seem to be flat and is shown to admit at most a one dimensional defect. Various properties of this system are investigated to illustrate the difficulties that arise in the control of the toycopter.
Keywords
aerodynamics; helicopters; propellers; aerodynamic force; feedback linearization; pitch angles; propeller speed; toycopter control; two-degree-of-freedom laboratory-scale helicopter-like system; yaw angles; Aerodynamics; Blades; Couplings; Force; Helicopters; Propellers; Torque; Differential Flatness; Helicopters; Modeling; Underactuated systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Control Conference (ECC), 1997 European
Conference_Location
Brussels
Print_ISBN
978-3-9524269-0-6
Type
conf
Filename
7082340
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