Energy Based Control of a Swash Mass Helicopter Through Decoupling Change of Coordinates

We consider a small helicopter structure that is maneuvered through the control of moving masses. It is referred to as a swash mass helicopter (SMH). This paper addresses the trajectory tracking control problem for the SMH, with a specific focus on the decoupling change of coordinates of both rotati...

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Main Authors: Babak Salamat, Andrea M. Tonello
Format: Article
Language:English
Published: IEEE 2020-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/9076666/
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spelling doaj-5bc261a18f464e3c8d025c1818efb1e12021-03-30T01:39:32ZengIEEEIEEE Access2169-35362020-01-018774497745810.1109/ACCESS.2020.29901139076666Energy Based Control of a Swash Mass Helicopter Through Decoupling Change of CoordinatesBabak Salamat0https://orcid.org/0000-0001-7262-3264Andrea M. Tonello1https://orcid.org/0000-0002-9873-2407Institute of Networked and Embedded Systems, Chair of Embedded Communication Systems, University of Klagenfurt, Klagenfurt, AustriaInstitute of Networked and Embedded Systems, Chair of Embedded Communication Systems, University of Klagenfurt, Klagenfurt, AustriaWe consider a small helicopter structure that is maneuvered through the control of moving masses. It is referred to as a swash mass helicopter (SMH). This paper addresses the trajectory tracking control problem for the SMH, with a specific focus on the decoupling change of coordinates of both rotational and translational dynamics. We propose a control scheme in which position tracking is the primary objective, while the attitude tracking task is considered as a secondary objective. The intermediate control signals related to the attitude dynamics exploit the structural properties of the SMH and are enhanced with terms that grant a more accurate tracking of the target trajectory. The closed-loop system stability under the trajectory tracking objective is obtained following the Interconnection and Damping Assignment Passivity-Based Control (IDA-PBC) approach. In addition, the presence of external disturbances can diminish the trajectory tracking performance. For this reason, a nonlinear outer loop controller is added to the IDA-PBC to compensate the disturbances. Finally, the results of several simulations are reported to evaluate the performance of the control strategy.https://ieeexplore.ieee.org/document/9076666/Unmanned aerial vehiclesswash mass helicopterdecoupling change of coordinatespassivity-based controltrajectory tracking
collection DOAJ
language English
format Article
sources DOAJ
author Babak Salamat
Andrea M. Tonello
spellingShingle Babak Salamat
Andrea M. Tonello
Energy Based Control of a Swash Mass Helicopter Through Decoupling Change of Coordinates
IEEE Access
Unmanned aerial vehicles
swash mass helicopter
decoupling change of coordinates
passivity-based control
trajectory tracking
author_facet Babak Salamat
Andrea M. Tonello
author_sort Babak Salamat
title Energy Based Control of a Swash Mass Helicopter Through Decoupling Change of Coordinates
title_short Energy Based Control of a Swash Mass Helicopter Through Decoupling Change of Coordinates
title_full Energy Based Control of a Swash Mass Helicopter Through Decoupling Change of Coordinates
title_fullStr Energy Based Control of a Swash Mass Helicopter Through Decoupling Change of Coordinates
title_full_unstemmed Energy Based Control of a Swash Mass Helicopter Through Decoupling Change of Coordinates
title_sort energy based control of a swash mass helicopter through decoupling change of coordinates
publisher IEEE
series IEEE Access
issn 2169-3536
publishDate 2020-01-01
description We consider a small helicopter structure that is maneuvered through the control of moving masses. It is referred to as a swash mass helicopter (SMH). This paper addresses the trajectory tracking control problem for the SMH, with a specific focus on the decoupling change of coordinates of both rotational and translational dynamics. We propose a control scheme in which position tracking is the primary objective, while the attitude tracking task is considered as a secondary objective. The intermediate control signals related to the attitude dynamics exploit the structural properties of the SMH and are enhanced with terms that grant a more accurate tracking of the target trajectory. The closed-loop system stability under the trajectory tracking objective is obtained following the Interconnection and Damping Assignment Passivity-Based Control (IDA-PBC) approach. In addition, the presence of external disturbances can diminish the trajectory tracking performance. For this reason, a nonlinear outer loop controller is added to the IDA-PBC to compensate the disturbances. Finally, the results of several simulations are reported to evaluate the performance of the control strategy.
topic Unmanned aerial vehicles
swash mass helicopter
decoupling change of coordinates
passivity-based control
trajectory tracking
url https://ieeexplore.ieee.org/document/9076666/
work_keys_str_mv AT babaksalamat energybasedcontrolofaswashmasshelicopterthroughdecouplingchangeofcoordinates
AT andreamtonello energybasedcontrolofaswashmasshelicopterthroughdecouplingchangeofcoordinates
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