LEADER 03091oam  2200853   450 
001 9910709706703321
005 20180828113939.0
035   $a(CKB)5470000002473184
035   $a(OCoLC)761372866
035   $a(OCoLC)995470000002473184
035   $a(EXLCZ)995470000002473184
100   $a20111115j198511    ua             0
101 0 $aeng
135   $aurun||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA method to stabilize linear systems using eigenvalue gradient information /$fCarol D. Wieseman
210  1$aWashington, D.C. :$cNational Aeronautics and Space Administration, Scientific and Technical Information Branch,$dNovember 1985.
215   $a1 online resource (37 pages) $cillustrations
225 1 $aNASA/TP ;$v2479
300   $a"November 1985."
300   $aPrepared at Langley Research Center.
320   $aIncludes bibliographical references (page 13).
606   $aLinear systems$2nasat
606   $aControl stability$2nasat
606   $aEigenvalues$2nasat
606   $aSystems stability$2nasat
606   $aDynamic control$2nasat
606   $aLinear systems$xComputer simulation
606   $aAirplanes$xControl systems$xComputer simulation
606   $aFlutter (Aerodynamics)$xComputer simulation
606   $aStability of airplanes, Lateral$xAutomatic control$xComputer simulation
606   $aEigenvalues
606   $aControl theory
606   $aMathematical optimization
606   $aAirplanes$xControl systems$xComputer simulation$2fast
606   $aControl theory$2fast
606   $aEigenvalues$2fast
606   $aFlutter (Aerodynamics)$xComputer simulation$2fast
606   $aMathematical optimization$2fast
615  7$aLinear systems.
615  7$aControl stability.
615  7$aEigenvalues.
615  7$aSystems stability.
615  7$aDynamic control.
615  0$aLinear systems$xComputer simulation.
615  0$aAirplanes$xControl systems$xComputer simulation.
615  0$aFlutter (Aerodynamics)$xComputer simulation.
615  0$aStability of airplanes, Lateral$xAutomatic control$xComputer simulation.
615  0$aEigenvalues.
615  0$aControl theory.
615  0$aMathematical optimization.
615  7$aAirplanes$xControl systems$xComputer simulation.
615  7$aControl theory.
615  7$aEigenvalues.
615  7$aFlutter (Aerodynamics)$xComputer simulation.
615  7$aMathematical optimization.
700   $aWieseman$b Carol D.$01412988
712 02$aUnited States.$bNational Aeronautics and Space Administration.$bScientific and Technical Information Branch,
712 02$aLangley Research Center.
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCQ
801  2$bOCLCO
801  2$bOCLCQ
801  2$bOCLCF
801  2$bGPO
801  2$bMERUC
801  2$bGPO
906   $aBOOK
912   $a9910709706703321
996   $aA method to stabilize linear systems using eigenvalue gradient information$93508253
997   $aUNINA