Vibroimpact Dynamics of a Tethered Satellite System
This paper presents the vibroimpact dynamics of an in-plane tethered subsatellite caused by sudden braking during deployment or retrieval. The full dynamics of the subsatellite are composed of its free-flight and the instantaneous impacts. At the moment of impact, the reflective angle of the subsate...
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| Format: | Article |
| Language: | English |
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Wiley
2017-01-01
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| Series: | Shock and Vibration |
| Online Access: | http://dx.doi.org/10.1155/2017/8748094 |
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| _version_ | 1832554252698910720 |
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| author | B. S. Yu H. Wen |
| author_facet | B. S. Yu H. Wen |
| author_sort | B. S. Yu |
| collection | DOAJ |
| description | This paper presents the vibroimpact dynamics of an in-plane tethered subsatellite caused by sudden braking during deployment or retrieval. The full dynamics of the subsatellite are composed of its free-flight and the instantaneous impacts. At the moment of impact, the reflective angle of the subsatellite is envisioned to be equal to its incident angle such that the impact law is obtained. Then, the stability of the periodic vibroimpacts is analyzed using the composite Poincaré map. Further, the vibroimpact responses that do not exceed a specified region are numerically determined via the cell mapping method. |
| format | Article |
| id | doaj-art-d61c5511732a4ccf9bcfa9d718958157 |
| institution | Kabale University |
| issn | 1070-9622 1875-9203 |
| language | English |
| publishDate | 2017-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | Shock and Vibration |
| spelling | doaj-art-d61c5511732a4ccf9bcfa9d7189581572025-02-03T05:52:05ZengWileyShock and Vibration1070-96221875-92032017-01-01201710.1155/2017/87480948748094Vibroimpact Dynamics of a Tethered Satellite SystemB. S. Yu0H. Wen1State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaState Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, ChinaThis paper presents the vibroimpact dynamics of an in-plane tethered subsatellite caused by sudden braking during deployment or retrieval. The full dynamics of the subsatellite are composed of its free-flight and the instantaneous impacts. At the moment of impact, the reflective angle of the subsatellite is envisioned to be equal to its incident angle such that the impact law is obtained. Then, the stability of the periodic vibroimpacts is analyzed using the composite Poincaré map. Further, the vibroimpact responses that do not exceed a specified region are numerically determined via the cell mapping method.http://dx.doi.org/10.1155/2017/8748094 |
| spellingShingle | B. S. Yu H. Wen Vibroimpact Dynamics of a Tethered Satellite System Shock and Vibration |
| title | Vibroimpact Dynamics of a Tethered Satellite System |
| title_full | Vibroimpact Dynamics of a Tethered Satellite System |
| title_fullStr | Vibroimpact Dynamics of a Tethered Satellite System |
| title_full_unstemmed | Vibroimpact Dynamics of a Tethered Satellite System |
| title_short | Vibroimpact Dynamics of a Tethered Satellite System |
| title_sort | vibroimpact dynamics of a tethered satellite system |
| url | http://dx.doi.org/10.1155/2017/8748094 |
| work_keys_str_mv | AT bsyu vibroimpactdynamicsofatetheredsatellitesystem AT hwen vibroimpactdynamicsofatetheredsatellitesystem |