| Title: | OS19-5 Dynamics Analysis of Payload On-orbit Catapult Separation Based on ADAMS |
|---|---|
| Publication: | ICAROB2018 |
| Volume: | 23 |
| Pages: | 728-731 |
| ISSN: | 2188-7829 |
| DOI: | 10.5954/ICAROB.2018.OS19-5 |
| Author(s): | Yi Li, Yingmin Jia, Jianheng Ling |
| Publication Date: | February 2, 2018 |
| Keywords: | Guide mechanism, catapult separation, virtual prototype, angular velocity |
| Abstract: | In this paper, a catapult separation device equipped with guide mechanism is considered, and the corresponding dynamic model is descripted firstly. Then, employing the dynamic simulation software ADAMS, the virtual prototype model of the separation device is established, and the whole process of on-orbit separation is simulated. Finally, the structure parameters of the guide mechanism such as the number of roller group or distance between groups are studied. The simulation results could provide references for the optimization of the separation device. |
| PDF File: | https://alife-robotics.co.jp/members2018/icarob/data/html/data/OS_pdf/OS19/OS19-5.pdf |
| Copyright: | © The authors. This article is distributed under the terms of the Creative Commons Attribution License 4.0, which permits non-commercial use, distribution and reproduction in any medium, provided the original work is properly cited. See for details: https://creativecommons.org/licenses/by-nc/4.0/ |
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