Robust compensator design for attitude control of the Spacecraft Control Laboratory Experiment (SCOLE) configuration is considered. A loop-shaping procedure similar to that used in the LQG/LTR method is used to iteratively design the compensator. A satisfactory compensator is obtained by including the rigid modes and three elastic modes in the design model.
Design of robust line-of-sight pointing control system for the SCOLE configuration
1987 American Control Conference ; 1987 ; Minneapolis, MN, United States
1987-01-01
Conference paper
No indication
English