Stability of an elastically connected two-body space station by the perturbation method
| dc.citation.epage | 208 | en_US |
| dc.citation.issue | G3 | en_US |
| dc.citation.spage | 193 | en_US |
| dc.citation.volume | 211 | en_US |
| dc.citation.woscount | 0 | |
| dc.contributor.author | Ge, ZM | en_US |
| dc.contributor.author | Ku, SC | en_US |
| dc.contributor.department | 交大名義發表 | zh_TW |
| dc.contributor.department | 機械工程學系 | zh_TW |
| dc.contributor.department | National Chiao Tung University | en_US |
| dc.contributor.department | Department of Mechanical Engineering | en_US |
| dc.date.accessioned | 2014-12-08T15:02:09Z | |
| dc.date.available | 2014-12-08T15:02:09Z | |
| dc.date.issued | 1997 | en_US |
| dc.description.abstract | This investigation deals with the stability, in a circular orbit, of a flexible space station consisting of two inertially identical rigid end bodies connected together by an elastic structure. The earth-pointing motion and the rotation with arbitrary initial angular velocity perpendicular to the orbital plane are studied by using the multiple-scales technique. The first-order approximate analytical solution and the conditions of stability are obtained. | en_US |
| dc.identifier.doi | 10.1243/0954410971532613 | en_US |
| dc.identifier.issn | 0954-4100 | en_US |
| dc.identifier.journal | PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | en_US |
| dc.identifier.uri | http://dx.doi.org/10.1243/0954410971532613 | en_US |
| dc.identifier.uri | https://ir.lib.nycu.edu.tw/handle/11536/847 | |
| dc.identifier.wosnumber | WOS:A1997XY04500005 | |
| dc.language.iso | en_US | en_US |
| dc.subject | stability | en_US |
| dc.subject | space station | en_US |
| dc.subject | perturbation method | en_US |
| dc.subject | multiple-scales technique | en_US |
| dc.title | Stability of an elastically connected two-body space station by the perturbation method | en_US |
| dc.type | Article | en_US |