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Attitude Control Considering Variable Input Saturation Limit for a Spacecraft Equipped with Flywheels
TIAN, Lin, XU, ShijieVolume:
25
Language:
english
Journal:
Chinese Journal of Aeronautics
DOI:
10.1016/S1000-9361(11)60400-7
Date:
June, 2012
File:
PDF, 274 KB
english, 2012