Feedback Control Logic for Spacecraft Eigenaxis Rotations Under Slew Rate and Control Constraints
Guidance, navigation and control conference ; 1994 ; Scottsdale; AZ
1994-01-01
10 pages
In 3 vols
Conference paper
English
AIAA , guidance , navigation , control
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Feedback Control Logic for Spacecraft Eigenaxis Rotations Under Slew Rate and Control Constraints
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