DocumentCode :
2650479
Title :
Design and Development of a 5-DOF Air-Bearing Spacecraft Simulator
Author :
Jian, Xu ; Gang, Bao ; QinJun, Yang ; Jun, Li
Author_Institution :
Res. Center of Pneumatics, Harbin Inst. of Technol., Harbin
fYear :
2009
fDate :
1-2 Feb. 2009
Firstpage :
126
Lastpage :
130
Abstract :
The Five Degrees of Freedom Air-bearing Spacecraft Simulator (5DOFASS) is designed at Harbin Institute of Technology for the purpose of simulating spacecraft autonomous formation flying and orbital maneuver. The 5DOFASS contains an attitude platform supported on a hemispherical air-bearing and a translation platform floated on three linear air-bearing feet, which provides a very low friction and 0-g environment in an Earth-bound laboratory. In this paper, the design and development of the 5DOFASS is described in detail, including working principle, structure, and control system. Some ongoing research problems and future plans are reported at the end of the article.
Keywords :
aerospace control; aerospace simulation; product design; zero gravity experiments; 0-g environment; 5-DOF air-bearing spacecraft simulator; 5DOFASS; Earth-bound laboratory; attitude platform; five degrees of freedom; hemispherical air-bearing; linear air-bearing feet; orbital maneuver; spacecraft autonomous formation flying; very low friction; Aerospace electronics; Computational modeling; Control systems; Foot; Friction; Propulsion; Robotics and automation; Space technology; Space vehicles; Testing; air-bearing; cold gas propulsion system; image process; spacecraft simulator;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Informatics in Control, Automation and Robotics, 2009. CAR '09. International Asia Conference on
Conference_Location :
Bangkok
Print_ISBN :
978-1-4244-3331-5
Type :
conf
DOI :
10.1109/CAR.2009.7
Filename :
4777209
Link To Document :
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