Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative Target
The robust H∞ control for spacecraft rendezvous with a noncooperative target is addressed in this paper. The relative motion of chaser and noncooperative target is firstly modeled as the uncertain system, which contains uncertain orbit parameter and mass. Then the H∞ performance and finite time perf...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
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Wiley
2013-01-01
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| Series: | The Scientific World Journal |
| Online Access: | http://dx.doi.org/10.1155/2013/579703 |
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| _version_ | 1832555863897800704 |
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| author | Shu-Nan Wu Wen-Ya Zhou Shu-Jun Tan Guo-Qiang Wu |
| author_facet | Shu-Nan Wu Wen-Ya Zhou Shu-Jun Tan Guo-Qiang Wu |
| author_sort | Shu-Nan Wu |
| collection | DOAJ |
| description | The robust H∞ control for spacecraft rendezvous with a noncooperative target is addressed in this paper. The relative motion of chaser and noncooperative target is firstly modeled as the uncertain system, which contains uncertain orbit parameter and mass. Then the H∞ performance and finite time performance are proposed, and a robust H∞ controller is developed to drive the chaser to rendezvous with the non-cooperative target in the presence of control input saturation, measurement error, and thrust error. The linear matrix inequality technology is used to derive the sufficient condition of the proposed controller. An illustrative example is finally provided to demonstrate the effectiveness of the controller. |
| format | Article |
| id | doaj-art-6da04b42cd654535a4c102aefbf353c9 |
| institution | Kabale University |
| issn | 1537-744X |
| language | English |
| publishDate | 2013-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | The Scientific World Journal |
| spelling | doaj-art-6da04b42cd654535a4c102aefbf353c92025-02-03T05:46:55ZengWileyThe Scientific World Journal1537-744X2013-01-01201310.1155/2013/579703579703Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative TargetShu-Nan Wu0Wen-Ya Zhou1Shu-Jun Tan2Guo-Qiang Wu3State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian 116024, ChinaSchool of Aeronautics and Astronautics, Dalian University of Technology, Dalian 116024, ChinaSchool of Aeronautics and Astronautics, Dalian University of Technology, Dalian 116024, ChinaSchool of Aeronautics and Astronautics, Dalian University of Technology, Dalian 116024, ChinaThe robust H∞ control for spacecraft rendezvous with a noncooperative target is addressed in this paper. The relative motion of chaser and noncooperative target is firstly modeled as the uncertain system, which contains uncertain orbit parameter and mass. Then the H∞ performance and finite time performance are proposed, and a robust H∞ controller is developed to drive the chaser to rendezvous with the non-cooperative target in the presence of control input saturation, measurement error, and thrust error. The linear matrix inequality technology is used to derive the sufficient condition of the proposed controller. An illustrative example is finally provided to demonstrate the effectiveness of the controller.http://dx.doi.org/10.1155/2013/579703 |
| spellingShingle | Shu-Nan Wu Wen-Ya Zhou Shu-Jun Tan Guo-Qiang Wu Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative Target The Scientific World Journal |
| title | Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative Target |
| title_full | Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative Target |
| title_fullStr | Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative Target |
| title_full_unstemmed | Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative Target |
| title_short | Robust H∞ Control for Spacecraft Rendezvous with a Noncooperative Target |
| title_sort | robust h∞ control for spacecraft rendezvous with a noncooperative target |
| url | http://dx.doi.org/10.1155/2013/579703 |
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