Closed loop lab tests of NASA's Mini-MastA design strategy which integrates model reduction by modal cost analysis and a multiobjective controller synthesis algorithm is used to design controllers for NASA's Mini-Mast system. The necessary modeling and control algorithms are easily programmed in Matlab standard software. Hence, this method is very practical for controller design for large space structures. The design algorithm also presents a solution for the important problem of tuning multiple-loop controllers.
Document ID
19910045503
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hsieh, C. (Purdue Univ. West Lafayette, IN, United States)
Kim, J. H. (Purdue Univ. West Lafayette, IN, United States)
Skelton, Robert E. (Purdue University West Lafayette, IN, United States)