DocumentCode
3028200
Title
Compare Tabletop style platform with umbrella style platform of air bearings spacecraft simulator
Author
Li, Yanbin ; Gao, Youhua
Author_Institution
Sch. of Mech. Eng., Shenyang Univ. of Technol., Shenyang, China
fYear
2010
fDate
8-10 June 2010
Firstpage
252
Lastpage
255
Abstract
The “Tabletop” and “umbrella” style platforms of 3DOF air-bearing spacecraft simulator were compared. According to the theory on kineto-elastodynamic analysis and on the spacecraft attitude kinetics, the formulary for the platform structure mass-center displacement is deduced. It is calculated that the unbalance torque resulted from deforming of the platform of air-bearing simulator acted on gravity. Both of the styles can be compared by analyzing unbalance torque influence by changing of distance between the plate and the center of rotation of the simulator.The result shows that tabletop style platform has such advantages as lower equilibrium sensitivity, higher adaptability for payload than umbrella style platform. However, because the rotation center of air bearing of tabletop style platform locates the plate of the platform, the maximal deflection angle of the simulator was restricted.
Keywords
aerospace components; aerospace simulation; elastodynamics; machine bearings; space vehicles; air bearing spacecraft simulator; kinetoelastodynamic analysis; mass-center displacement; spacecraft attitude kinetics; tabletop style platform; torque unbalance; umbrella style platform; Adaptation model; Atmospheric modeling; Finite element methods; Payloads; Sensitivity; Space vehicles; Torque;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location
Harbin
Print_ISBN
978-1-4244-6043-4
Electronic_ISBN
978-1-4244-7505-6
Type
conf
DOI
10.1109/ISSCAA.2010.5632323
Filename
5632323
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