Kinematics Analysis and Simulation of Small Satellite Docking Mechanism End Executor

Yuan Zhang; Ying Ying Wang; Yan Song; Li Li Zhou

doi:10.4028/www.scientific.net/AMM.487.460

Paper Titles

A Design of Miniaturized High Performance Charge Amplifier
p.435

Image Analysis of a Moving Bubble Train in a Tube
p.440

Finite Element Simulation of Partical Discharge Acoustic Pressure Levels Distribution in Gas Insulated Switchgear
p.447

Simulation and Analysis of Water Pump Bearing Assembly Based on ANSYS
p.455

Kinematics Analysis and Simulation of Small Satellite Docking Mechanism End Executor
p.460

Analysis of RC Member’s Reliability Subjected to Eccentric Compression Based on Monte Carlo Simulation
p.465

A Study on the Flow Field Simulation of Insertion Flow Sensor in Large Diameter Pipeline
p.470

Collective Smart Вehaviour of Magnetic Nanoparticles at Simulation of Hysteresis Phenomena in Artificial Ordered Array
p.475

Modeling and Analysis of Surface Topography in Elliptical Vibration Cutting
p.479

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 487Kinematics Analysis and Simulation of Small...

Kinematics Analysis and Simulation of Small Satellite Docking Mechanism End Executor

Abstract:

In order to save space mission cost, prolonging the working life of the spacecraft and improving the flexibility and capable of performing various tasks should get more attention on orbit servicing technology. For the docking process of a new type of two independent service in-orbit spacecraft, this paper finished the kinematics analysis, for the whole docking capture process, two groups of different initial conditions and control function of the simulation analysis were finished by the ADAMS software. The results prove that the docking mechanism performance is very good, and reliable connection can be realized in the general initial conditions.

You might also be interested in these eBooks

Mechanical Structures and Smart Materials

View Preview

Info:

Periodical:

Applied Mechanics and Materials (Volume 487)

Pages:

460-464

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.487.460

Citation:

Cite this paper

Online since:

January 2014

Authors:

Yuan Zhang*, Ying Ying Wang, Yan Song, Li Li Zhou

Keywords:

Docking Mechanism, End Executor, Kinematics Analysis

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

* - Corresponding Author

References

[1] LIN Laixing, Development of Space Rendezvous and Docking Technology in Past 40 Years, SPACECRAFT ENGINEERING , 16 (2008)70-77.

Google Scholar

[2] CUI Nai gang, WANG Ping, GUO Ji feng, CHENG Xing, A Review of On-Orbit Servicing, Journal of Astronautics, 28(2007)805-811.

Google Scholar

[3] LIN Qi , LAI Jiazhe, Study on Simulation Technology of Rendezvous and Docking in Space, Journal of the Academy of Equipment Command & Technology, 19(2008)53-57.

Google Scholar

[4] Wang Hua, Tang Guojin, Wang Feng, Application of Prototype Method to Rendezvous and Docking Simulation System, MISSILES AND SPACE VEHICLES, 5(2004) 18-22.

Google Scholar

[5] Zhou Lini, Attitude Dynamics And Control Simulation For RVD Target -Spacecraft, National University of Defense technology , (2004).

Google Scholar

[6] LU Wei, GENG Yunhai, CHEN Xueqin, WANG Feng, Coupled Control of Relative Position and Attitude for On –orbit Servicing Spacecraft with Respect to Target, Acta Aeronautica et Astronautica Sinic, 32(2011)857-865.

Google Scholar

[7] GuanYingzi YangDaming, Dynamic Modeling of Spacecraft Docking Process, Journal of Nanjing University of Science and Technology, 28(2001)6-9.

Google Scholar

[8] LI Qiang，HUANG Yi－yong，CHEN Xiao－qian，ZHAO Yong, Modeling and Simulating of Independent On－orbit Servicing Spacecrafts' Docking Process, Computer Simulation, 10(2011)57-61.

Google Scholar