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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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 |
_version_ |
1724186661601935360 |