Show simple item record

dc.contributor.authorSunkara, Vishwamithra Reddy
dc.contributor.authorNobleheart, Wilfred
dc.contributor.authorChakravarthy, Animesh
dc.date.accessioned2014-12-12T14:39:38Z
dc.date.available2014-12-12T14:39:38Z
dc.date.issued2014-11
dc.identifier.citationVishwamithra Sunkara, Wilfred Nobleheart, and Animesh Chakravarthy. "Performance Metrics for Tiltrotor Flight Dynamics During the Transition Regime", Journal of Guidance, Control, and Dynamics, Vol. 37, No. 6 (2014), pp. 2039-2044en_US
dc.identifier.issn0731-5090
dc.identifier.otherWOS:000343924400026
dc.identifier.urihttp://dx.doi.org/10.2514/1.G000310
dc.identifier.urihttp://hdl.handle.net/10057/11007
dc.descriptionClick on the DOI link to access the article (may not be free).en_US
dc.description.abstractFor control system design purposes, desirable locations of short period and phugoid poles with their respective damping factors and natural frequencies are specified for fixed-wing aircraft in U.S. Department of Defense military specifications (MIL-SPEC) documents [1,2] and for heliocopters in aeronautical design standard (ADS)/MIL-SPEC documents [3-5]. In both cases, the control system designers can verify and demonstrate the validity of their design, in part by analytically verifying that the closed-loop system, when linearized about different trim conditions, possesses damping factors and natural frequencies that satisfy these requirements.en_US
dc.description.sponsorshipFAA funded project on Fly-by-Wire and Fly-by-Light Control Systems for Rotorcraft (FAA Award Number 07-C-GA-WISU), in the course of this work.en_US
dc.language.isoen_USen_US
dc.publisherAmerican Institute of Aeronautics and Astronauticsen_US
dc.relation.ispartofseriesJournal of Guidance, Control, and Dynamics;v.37:no.6
dc.subjectSystemsen_US
dc.subjectPolesen_US
dc.subjectZerosen_US
dc.titlePerformance metrics for tiltrotor flight dynamics during the transition regimeen_US
dc.typeArticleen_US
dc.rights.holder©2012 AIAA


Files in this item

FilesSizeFormatView

There are no files associated with this item.

This item appears in the following Collection(s)

Show simple item record