DocumentCode :
700484
Title :
Outer flatness: Trajectory generation for a model helicopter
Author :
van Nieuwstadt, Michiel ; Murray, Richard M.
Author_Institution :
Ford Res. Centre Aachen, Aachen, Germany
fYear :
1997
fDate :
1-7 July 1997
Firstpage :
325
Lastpage :
330
Abstract :
This paper introduces the concept of outer flatness, a derivative of differential flatness. Outer flatness describes a system that can be split in 2 subsytems, a non-flat inner system and a flat outer system. The outputs of the outer system are the tracking outputs of interest. The inputs of the outer system are the outputs of the inner system, and not subject to our direct control. The inputs of the inner system are the real actuator inputs. This system structure is also present in backstepping and dynamic inversion. We present two theorems on exponential and bounded tracking for outer flat systems, based on Lyapunoff arguments. We validate the approach with simulations and experiments on a model helicopter.
Keywords :
aircraft control; control nonlinearities; differential equations; helicopters; trajectory control; backstepping; differential flatness; dynamic inversion; exponential tracking; flat outer system; model helicopter; nonflat inner system; outer flatness; trajectory generation; Actuators; Dynamics; Helicopters; Jacobian matrices; Mathematical model; Rotors; Trajectory;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (ECC), 1997 European
Conference_Location :
Brussels
Print_ISBN :
978-3-9524269-0-6
Type :
conf
Filename :
7082114
Link To Document :
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