Linear estimation and control studies of vibration suppression of SCOLE flexible mastA Kalman filter and a controller are presented for vibration suppression of the Spacecraft Control Laboratory Experiment flexible mast mounted in the cantilevered configuration. Mode shapes and frequencies of the structure obtained from a finite element analysis are used to compute the controller and filter gains. The paper presents results and discussion from simulation and experimental studies. Comparison of experimental results with those obtained by simulation show close agreement.
Document ID
19910039111
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ghosh, D. (Planning Research Corp. Hampton, VA, United States)
Montgomery, R. C. (NASA Langley Research Center Hampton, VA, United States)
Norris, M. A. (Planning Research Corp. Hampton, VA, United States)
Meirovitch, L. (Virginia Polytechnic Institute and State University Blacksburg, United States)