Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach
It is well known that single equilibrium orientation point in matrix rotation is represented by two equilibrium points in quaternion. This fact would imply nonefficient control effort as well as problem in guaranteeing stability of the two equilibrium points in quaternion. This paper presents a solu...
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| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
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Wiley
2014-01-01
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| Series: | Modelling and Simulation in Engineering |
| Online Access: | http://dx.doi.org/10.1155/2014/652571 |
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| author | Harry Septanto Riyanto T. Bambang Arief Syaichu-Rohman Ridanto Eko Poetro Adrianto Ravi Ibrahim |
| author_facet | Harry Septanto Riyanto T. Bambang Arief Syaichu-Rohman Ridanto Eko Poetro Adrianto Ravi Ibrahim |
| author_sort | Harry Septanto |
| collection | DOAJ |
| description | It is well known that single equilibrium orientation point in matrix rotation is represented by two equilibrium points in quaternion. This fact would imply nonefficient control effort as well as problem in guaranteeing stability of the two equilibrium points in quaternion. This paper presents a solution to design quaternion-based spacecraft attitude control system whose saturation element is in its control law such that those problems are overcome. The proposed feature of methodology is the consideration on boundedness of solution in the control system design even in the presence of unknown external disturbance. The same methodology is also used to design cooperative spacecrafts attitude control system. Through the proposed method, the most relaxed information-state topology requirement is obtained, that is, the directed graph that contains a directed spanning tree. Some numerical simulations demonstrate effectiveness of the proposed feature of methodology. |
| format | Article |
| id | doaj-art-e732ec12dfb14a43bd7722f1b7b549e6 |
| institution | Kabale University |
| issn | 1687-5591 1687-5605 |
| language | English |
| publishDate | 2014-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | Modelling and Simulation in Engineering |
| spelling | doaj-art-e732ec12dfb14a43bd7722f1b7b549e62025-08-20T03:26:14ZengWileyModelling and Simulation in Engineering1687-55911687-56052014-01-01201410.1155/2014/652571652571Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution ApproachHarry Septanto0Riyanto T. Bambang1Arief Syaichu-Rohman2Ridanto Eko Poetro3Adrianto Ravi Ibrahim4School of Electrical Engineering and Informatics, Institut Teknologi Bandung, Bandung 40123, IndonesiaSchool of Electrical Engineering and Informatics, Institut Teknologi Bandung, Bandung 40123, IndonesiaSchool of Electrical Engineering and Informatics, Institut Teknologi Bandung, Bandung 40123, IndonesiaFaculty of Mechanical and Aerospace Engineering, Institut Teknologi Bandung, Bandung 40123, IndonesiaSchool of Electrical Engineering and Informatics, Institut Teknologi Bandung, Bandung 40123, IndonesiaIt is well known that single equilibrium orientation point in matrix rotation is represented by two equilibrium points in quaternion. This fact would imply nonefficient control effort as well as problem in guaranteeing stability of the two equilibrium points in quaternion. This paper presents a solution to design quaternion-based spacecraft attitude control system whose saturation element is in its control law such that those problems are overcome. The proposed feature of methodology is the consideration on boundedness of solution in the control system design even in the presence of unknown external disturbance. The same methodology is also used to design cooperative spacecrafts attitude control system. Through the proposed method, the most relaxed information-state topology requirement is obtained, that is, the directed graph that contains a directed spanning tree. Some numerical simulations demonstrate effectiveness of the proposed feature of methodology.http://dx.doi.org/10.1155/2014/652571 |
| spellingShingle | Harry Septanto Riyanto T. Bambang Arief Syaichu-Rohman Ridanto Eko Poetro Adrianto Ravi Ibrahim Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach Modelling and Simulation in Engineering |
| title | Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach |
| title_full | Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach |
| title_fullStr | Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach |
| title_full_unstemmed | Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach |
| title_short | Quaternion-Based Attitude Control System Design of Single and Cooperative Spacecrafts: Boundedness of Solution Approach |
| title_sort | quaternion based attitude control system design of single and cooperative spacecrafts boundedness of solution approach |
| url | http://dx.doi.org/10.1155/2014/652571 |
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