Two adaptive controllers designed for the Spacecraft Control Laboratory Experiment (SCOLE) at NASA Langley Research Center are discussed. The first controller is an adaptive model following variable structure controller and the second is an indirect LQ adaptive controller. For each technique, the design of the controller is outlined and simulation results are presented. Plans for future studies are also discussed.
Adaptive control techniques for the SCOLE configuration
VPI&SU/AIAA Symposium ; 1987 ; Blacksburg, VA, United States
1988-01-01
Conference paper
No indication
English
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