An Experimental Study on Attitude Control of Spacecraft using Two-axis Rotational Simulator with a Flexible Arm

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Publisher
ASCC
Issue Date
2002-09-25
Language
ENG
Citation

4th Asian Control Conference, pp.2051 - 2056

URI
http://hdl.handle.net/10203/16526
Appears in Collection
AE-Conference Papers(학술회의논문)

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