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
Link To Document :
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