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181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aExtraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack /$fKenneth W. Iliff, Kon-Sheng Charles Wang
210  1$a[Washington, D.C] :$cNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center,$dFebruary 1997.
215   $a1 online resource (iii, 35 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v4786
300   $aTitle from title screen (viewed April 5, 2016).
300   $a"February 1997."
300   $a"Performing organization: NASA Dryden Flight Research Center, Edwards, California"--Report documentation page.
320   $aIncludes bibliographical references (pages 14-15).
606   $aAngle of attack$2nasat
606   $aF-18 aircraft$2nasat
606   $aMaximum likelihood estimates$2nasat
606   $aParameter identification$2nasat
606   $aWind tunnel tests$2nasat
615  7$aAngle of attack.
615  7$aF-18 aircraft.
615  7$aMaximum likelihood estimates.
615  7$aParameter identification.
615  7$aWind tunnel tests.
700   $aIliff$b Kenneth W.$013447
702   $aWang$b Kon-Sheng Charles
712 02$aNASA Dryden Flight Research Center.
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Program,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCF
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801  2$bGPO
906   $aBOOK
912   $a9910707010803321
996   $aExtraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack$93529508
997   $aUNINA