Calculation and simulation of the space manipulator experiment

Ji Ping Lu*, Shui Yuan Tang, Yan Yan, Ke Fei Miao

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

A self-servicing system of satellite is one coupling system. The attitude of satellite is affected by the movements of a manipulator. According to the structure of the arm, a dynamic model of the self-servicing system is put forward. The operations of the self-servicing system are simulated in ADAMS, which result shows that different movement paths of the arm make different influence on the attitude of the satellite. In order to test the functions of the system, an experiment is done on the air-bearing platform. This paper calculates and simulates the movement path of the experiment system. The result is valuable to guide the experiment on the air-bearing platform.

Original languageEnglish
Title of host publicationProceedings - 2010 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2010
Pages74-78
Number of pages5
DOIs
Publication statusPublished - 2010
Event2010 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2010 - Xiamen, China
Duration: 29 Oct 201031 Oct 2010

Publication series

NameProceedings - 2010 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2010
Volume1

Conference

Conference2010 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2010
Country/TerritoryChina
CityXiamen
Period29/10/1031/10/10

Keywords

  • Component
  • Dynamic model
  • Simulation
  • The air bearing
  • The self-servicing system

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