Publication:
Development of Closed-Loop Tail-Sizing Criteria for a High Speed Civil Transport

dc.contributor.authorKaminer, Isaac
dc.contributor.authorHoward, R.M.
dc.contributor.authorButtrill, C.
dc.dateSeptember­ October 1997
dc.date.accessioned2017-04-25T19:07:05Z
dc.date.available2017-04-25T19:07:05Z
dc.date.issued1997-09
dc.descriptionJournal of Aircraft, Vol. 34, No. 5, September-October 1997.en_US
dc.description.abstractA study was conducted to determine the closed-loop tail-sizing criteria for a High Speed Civil Transport using a newly developed integrated aircraft/controller design methodology. The key idea is to cast closed loop requirements as linear matrix inequalities, for which ef cient numerical solvers are available. In particular, the effects of certain feedback specifications, and of actuator amplitude and rate constraints on the maximum allowable c.g. travel for a given set of tail sizes are studied. A constant gain state feedback controller is designed as a part of the tail-sizing process.en_US
dc.identifier.citationI. Kaminer, R. M. Howard, and C. Buttrill, "Development of Closed-Loop Tail-Sizing Criteria for a High Speed Civil Transport'', Journal of Aircraft, Vol. 34, No. 5, September-October 1997.
dc.identifier.urihttps://hdl.handle.net/10945/52707
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleDevelopment of Closed-Loop Tail-Sizing Criteria for a High Speed Civil Transporten_US
dc.typeArticleen_US
dspace.entity.typePublication
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