| contributor author | Yao | |
| contributor author | Zhang | |
| contributor author | Shijie | |
| contributor author | Xu | |
| date accessioned | 2017-05-08T21:33:53Z | |
| date available | 2017-05-08T21:33:53Z | |
| date copyright | October 2012 | |
| date issued | 2012 | |
| identifier other | %28asce%29as%2E1943-5525%2E0000156.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56303 | |
| description abstract | The vibration isolation platform of control moment gyroscopes (CMGs) on satellites is discussed. First, the theory of single-axis vibration isolation is presented and an isolation scheme for CMGs is put forward and applied to a satellite, which can provide an ultraquiet environment for optical payloads. Second, an integrated satellite dynamic model including the vibration isolation platform and pyramid configuration of the CMGs is built. The validity of this dynamic model is then verified by | |
| publisher | American Society of Civil Engineers | |
| title | Vibration Isolation Platform for Control Moment Gyroscopes on Satellites | |
| type | Journal Paper | |
| journal volume | 25 | |
| journal issue | 4 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000156 | |
| tree | Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 004 | |
| contenttype | Fulltext | |
