Fuzzy bang-bang relay controller for satellite attitude control system
Two level bang-bang controllers are generally used in conjunction with the thrust reaction actuator for spacecraft/satellite attitude control. These controllers are fast acting and dispense time dependent; full or no thrust-power to control the satellite attitude in minimum time. A minimum time-fuel...
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2017
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| Online Access: | Fuzzy Sets and Systems Volume 161, Issue 15, 1 August 2010, Pages 2104-2125 |
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uniten-123456789-50252017-11-14T07:15:39Z Fuzzy bang-bang relay controller for satellite attitude control system Nagi, F. Ahmed, S.K. Zainul Abidin, A.A. Nordin, F.H. Two level bang-bang controllers are generally used in conjunction with the thrust reaction actuator for spacecraft/satellite attitude control. These controllers are fast acting and dispense time dependent; full or no thrust-power to control the satellite attitude in minimum time. A minimum time-fuel attitude control system extends the life of a satellite and is the main focus of this paper. Fuzzy controllers are favored for satellite control due to their simplicity and good performance in terms of fuel saving, absorbing non-linearities and uncertainties of the plant. A fuzzy controller requires a soft fuzzy engine, and a hardware relay to accomplish bang-bang control action. The work in this paper describes a new type of fuzzy controller in which the hardware relay action is configured in the soft fuzzy engine. The new configuration provides fuzzy decision-making flexibility at the inputs with relay like two-level bang-bang output. The new fuzzy controller is simulated on a three-axis satellite attitude control platform and compared with conventional a fuzzy controller, sliding mode controller and linear quadratic regulator. The result shows that the proposed controller has minimum-time response compared to other controllers. Inherent chattering associated with a two-level bang-bang controller produces undesirable low amplitude frequency limit cycles. The chattering can be easily stopped in the proposed fuzzy bang-bang relay controller, hence adding multi-functionality to its simple design. © 2010 Elsevier B.V. All rights reserved. 2017-11-14T03:21:27Z 2017-11-14T03:21:27Z 2010 Article 10.1016/j.fss.2009.12.004 en Fuzzy Sets and Systems Volume 161, Issue 15, 1 August 2010, Pages 2104-2125 |
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Digital Repository |
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Local University |
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Universiti Tenaga Nasional |
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UNITEN Institutional Repository |
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Online Access |
| language |
English |
| description |
Two level bang-bang controllers are generally used in conjunction with the thrust reaction actuator for spacecraft/satellite attitude control. These controllers are fast acting and dispense time dependent; full or no thrust-power to control the satellite attitude in minimum time. A minimum time-fuel attitude control system extends the life of a satellite and is the main focus of this paper. Fuzzy controllers are favored for satellite control due to their simplicity and good performance in terms of fuel saving, absorbing non-linearities and uncertainties of the plant. A fuzzy controller requires a soft fuzzy engine, and a hardware relay to accomplish bang-bang control action. The work in this paper describes a new type of fuzzy controller in which the hardware relay action is configured in the soft fuzzy engine. The new configuration provides fuzzy decision-making flexibility at the inputs with relay like two-level bang-bang output. The new fuzzy controller is simulated on a three-axis satellite attitude control platform and compared with conventional a fuzzy controller, sliding mode controller and linear quadratic regulator. The result shows that the proposed controller has minimum-time response compared to other controllers. Inherent chattering associated with a two-level bang-bang controller produces undesirable low amplitude frequency limit cycles. The chattering can be easily stopped in the proposed fuzzy bang-bang relay controller, hence adding multi-functionality to its simple design. © 2010 Elsevier B.V. All rights reserved. |
| format |
Article |
| author |
Nagi, F. Ahmed, S.K. Zainul Abidin, A.A. Nordin, F.H. |
| spellingShingle |
Nagi, F. Ahmed, S.K. Zainul Abidin, A.A. Nordin, F.H. Fuzzy bang-bang relay controller for satellite attitude control system |
| author_facet |
Nagi, F. Ahmed, S.K. Zainul Abidin, A.A. Nordin, F.H. |
| author_sort |
Nagi, F. |
| title |
Fuzzy bang-bang relay controller for satellite attitude control system |
| title_short |
Fuzzy bang-bang relay controller for satellite attitude control system |
| title_full |
Fuzzy bang-bang relay controller for satellite attitude control system |
| title_fullStr |
Fuzzy bang-bang relay controller for satellite attitude control system |
| title_full_unstemmed |
Fuzzy bang-bang relay controller for satellite attitude control system |
| title_sort |
fuzzy bang-bang relay controller for satellite attitude control system |
| publishDate |
2017 |
| url |
Fuzzy Sets and Systems Volume 161, Issue 15, 1 August 2010, Pages 2104-2125 |
| first_indexed |
2018-09-05T07:32:08Z |
| last_indexed |
2018-09-05T07:32:08Z |
| _version_ |
1610751912249917440 |