Dynamics Analysis of Payload On-orbit Catapult Separation Based on ADAMS

Authors
Yi [email protected], Yingmin Jia*, [email protected], Jianheng [email protected]
The Seventh Research Division and the Center for Information and Control School of Automation Science and Electrical Engineering, Beihang University (BUAA), 37 Xueyuan Road, Haidian District Beijing, 100191, China
www.buaa.edu.cn

*
Corresponding author
Corresponding Author
Yingmin [email protected]
Available Online 30 September 2018.
DOI
https://doi.org/10.2991/jrnal.2018.5.2.6
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.

Copyright
Copyright © 2018, the Authors. Published by ALife Robotics Corp. Ltd.
Open Access
This is an open access article under the CC BY-NC license (http://creativecommons.org/licences/by-nc/4.0/).

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