Dynamic Modeling of the Capture Process of Snare Space Grapple Device

Article Preview

Abstract:

Snare space grapple device is designed for grappling large in-orbit payloads. Based on describing the grappling process, dynamic modeling of capturing a free-floating vehicle with large solar sails is performed by using Newton-Euler and hybrid coordinate methods in this paper. The models considering target vehicle as a rigid central body with flexible appendages which are discrete by using finite element method.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 217-218)

Pages:

1093-1097

Citation:

Online since:

March 2011

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2011 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] G. Hirzinger, K. Landzettel, B. Brunner, et al. DLR's robotics technologies for on-orbit servicing. Advanced Robotics, 2004, 18(2), pp.139-174, (2004).

DOI: 10.1163/156855304322758006

Google Scholar

[2] M. Oda, N. Inaba, M. Nishida, et al. Development of an EVA end-effector, grapple fixtures and tools for the satellite mounted robot system. Pro. of IEEE/RSJ Int. Conf. on Intelligent Robots and Systems. Osaka, Japan, Nov. 4-8, 1996, Volume3, pp.1536-1543, (1996).

DOI: 10.1109/iros.1996.569017

Google Scholar

[3] E. C. Wu, J. C. Hwang and J. T. Chladek. Fault tolerant joint development for the space shuttle remote manipulator system: analysis and development. IEEE Transaction on Robotics and Automation, 1993, 9(5), pp.675-684, (1993).

DOI: 10.1109/70.258058

Google Scholar

[4] R. Daniell, S. Sachdev. The design and development of an end effector for the shuttle remote manipulator system. The 16th Aerospace Mechanisms Symposium, Orlando, USA, May 13-14, 1982. pp.45-59, (1982).

Google Scholar

[5] S. Burns, S. Razvi. Evolution of the space station robotic manipulator. 58th International Astronautical Congress 2007, Hyderabad, India, Sep. 24- 28, 2007, Volume 10, pp.6933-6945, (2007).

Google Scholar

[6] S. Abiko, K. Yoshida, Y. Sato, et al. Performance Improvement of JEMRMS in Light of Vibration Dynamics. 8th International Symposium on Artificial Intelligence, Robotics and Automation in Space, Munich, Germany, Sep. 5-8, 2005, pp.543-548, (2005).

Google Scholar

[7] W. Feshe. Automated rendezvous and dockong of spacecraft. Cambridge Univercity Press, UK, 2003, pp.283-335, (2003).

Google Scholar