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Techniques for Designing Rotorcraft Control Systems, Final Report

dc.contributor.authorYudilevitch, G.en_US
dc.contributor.authorLevine, William S.en_US
dc.date.accessioned2007-05-23T09:56:52Z
dc.date.available2007-05-23T09:56:52Z
dc.date.issued1994en_US
dc.identifier.urihttp://hdl.handle.net/1903/5528
dc.description.abstractOver the last two and a half years we have been demonstrating a new methodology for the design of rotorcraft flight control systems (FCS) to meet handling qualities requirements. This method is based on multicriterion optimization as implemented in the optimization package CONSOL-OPTCAD (C-O). This package has been developed at the Institute for Systems Research (ISR) at the University of Maryland at College Park. This design methodology has been applied to the design of a FCS for the UH-60A helicopter in hover having the ADOCS control structure. The controller parameters have been optimized to meet the ADS-33C specifications. Furthermore, using this approach, an optimal (minimum control energy) controller has been obtained and trade- off studies have been performed.en_US
dc.format.extent4003484 bytes
dc.format.mimetypeapplication/pdf
dc.language.isoen_USen_US
dc.relation.ispartofseriesISR; TR 1994-54en_US
dc.subjectaircraft computer aided design en_US
dc.subjectnonlinear systemsen_US
dc.subjectoptimizationen_US
dc.subjectrotorcraften_US
dc.subjectIntelligent Servomechanismsen_US
dc.titleTechniques for Designing Rotorcraft Control Systems, Final Reporten_US
dc.typeTechnical Reporten_US
dc.contributor.departmentISRen_US


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