The Research on Virtual Prototype of Rod-Cone Docking Mechanism

Xin Hua Xie; Jun Jie Zhou; Gang Zhao; Wan Qing Li

doi:10.4028/www.scientific.net/AMM.684.354

Paper Titles

Based on 3D Virtual Prototype Technology and Finite Element Analysis of the Optimization of the Automobile Front Axle
p.330

Research on the Protection of Forward-Facing Cavity on the Flow Field of Low Total Pressure Opposing Jet
p.335

Based on Analysis of Finite Element Analysis of Automobile Transmission Shaft Comprehensive Optimization
p.341

Three-Dimensional Finite Element Coupled Analysis of a Diesel Engine Piston
p.347

The Research on Virtual Prototype of Rod-Cone Docking Mechanism
p.354

Axial Deformation of the Planetary Differential Micro-Displacement Mechanism with Finite Element Analysis
p.358

Based on the Finite Element Analysis of Rescue Vehicles Modular Virtual Prototype Research
p.364

Research on Ballast System of 1000t Crane Vessel
p.369

Stability and Control of Tooling System for High-Speed Machining
p.375

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 684The Research on Virtual Prototype of Rod-Cone...

The Research on Virtual Prototype of Rod-Cone Docking Mechanism

Abstract:

The achievement of space orbit service space autonomous docking technology. At present, many kinds of autonomous docking mechanism are appeared according to different service object. In order to widen the application range from lives of docking mechanism, design a space rod - cone docking mechanism in this paper. The mechanism can be in the context of a larger space, achieve self-occupied docking. And based on the ADAMS-View to complete the mechanism dynamics virtual prototype. According to the space orbit autonomous docking technology, set up virtual prototype mainly docking detection parameters, Analysis of dynamic characteristics in the whole of the docking process and complete the mechanism.

You might also be interested in these eBooks

Proceedings of 2014 International Conference on Mechanics and Mechanical Engineering

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volume 684)

Pages:

354-357

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.684.354

Citation:

Cite this paper

Online since:

October 2014

Authors:

Xin Hua Xie, Jun Jie Zhou, Gang Zhao, Wan Qing Li

Keywords:

Docking Mechanism, Dynamic Characteristic, On-Orbit Service, Space Docking Technology, Virtual Prototype

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] Reynerson, c. m. Spacecraft modular architecture design for on-orbit servicing. IEEE aerospace conference proceedings, 2000, v 4: 227-237.

DOI: 10.1109/aero.2000.878426

Google Scholar

[2] Inga-lena, hannukka. An Alternative Concept of Docking for The Conexpress Satellite. Master thesis, Lulea University of Technology, Jan, (2006).

Google Scholar

[3] Davis, Thomas M; Melanson, David. Xss-10 micro-satellite flight demonstration program results. Proceedings of SPIE - the international society for optical engineering, 2004, v 5419: 16-25.

Google Scholar

[4] Caswell, Doug; Visentin, Gianfranco; etc. Conexpress orbital life extension vehicle European space agency bulletin. 2006, n 127: 54-61.

Google Scholar