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003 OCoLC;

005 20131018082628.0;

006 m o d f ;

007 cr c||||||||||;

008 131018s2012 ohua obt f000 0 eng d;

040 a| GPOb| enge| rdae| pnc| GPOd| MvI;

049 a| ERE#;

074 a| 0830-D (online);

086 0 a| NAS 1.15:2012-217814;

100 1 a| May, Ryan D.,e| author.=| ^A1412438;

245 10 a| Reducing conservatism in aircraft engine response using conditionally active min-max limit regulators /c| Ryan D. May, Sanjay Garg.;

264 1 a| Cleveland, Ohio :b| National Aeronautics and Space Administration, Glenn Research Center,c| [2012];

300 a| 1 online resource (10 pages) :b| illustrations.;

336 a| textb| txt2| rdacontent;

337 a| computerb| c2| rdamedia;

338 a| online resourceb| cr2| rdacarrier;

490 1 a| NASA/TM 2012-217814;

500 a| Title from title screen (viewed Oct. 18, 2013).;

500 a| "December 2012.";

500 a| Prepared for the Turbo Expo 2012 sponsored by the American Society of Mechanical Engineers (ASME), Copenhagen, Denmark, June 11-15, 2012.;

504 a| Includes bibliographical references (page 10).;

536 d| E-18550;

536 a| Sponsored by the National Aeronautics and Space Administration, Washtingon, DCh| WBS 284848.02.06.03.02;

500 a| "GT2012-70017.";

500 a| GPO Cataloging Record Distribution Program (CRDP).;

650 7 a| Commercial aircraft.2| nasat;

650 7 a| Aircraft control.2| nasat;

650 7 a| Control systems design.2| nasat;

650 7 a| Engine control.2| nasat;

650 7 a| Sequential control.2| nasat;

650 7 a| Transient response.2| nasat;

700 1 a| Garg, Sanjay,e| author.=| ^A436709;

710 1 a| United States.b| National Aeronautics and Space Administratione| sponsoring body.=| ^A5437;

710 2 a| NASA Glenn Research Center,e| issuing body.=| ^A420740;

711 2 a| ASME Turbo Expod| (2012 :c| Copenhagen, Denmark)=| ^A1166099;

830 0 a| NASA technical memorandumv| 217814.=| ^A467613;

856 40 u| https://purl.fdlp.gov/GPO/gpo40528;

949 a| Click on web addressw| asish| joyner94;

596 a| 1;

998 a| 3387390;

999 a| CLICK ON WEB ADDRESSw| ASISc| 1i| 3387390-1001l| JNETm| JOYNERr| Ys| Yt| JNE1DOu| 11/11/2013x| EDOCUMENTz| JERESOURCE;

Reducing conservatism in aircraft engine response using conditionally active min-max limit regulators / Ryan D. May, Sanjay Garg.

Author/creator	May, Ryan D. author.
Format	Electronic
Publication	Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Description	1 online resource (10 pages) : illustrations.
Supplemental Content	https://purl.fdlp.gov/GPO/gpo40528

Other author/creator	Garg, Sanjay, author.
Other author/creator	United States. National Aeronautics and Space Administration sponsoring body.
Other author/creator	NASA Glenn Research Center, issuing body.
Other author/creator	ASME Turbo Expo (2012 : Copenhagen, Denmark)
Series	NASA/TM 2012-217814 NASA technical memorandum 217814. ^A467613
General note	Title from title screen (viewed Oct. 18, 2013).
General note	"December 2012."
General note	Prepared for the Turbo Expo 2012 sponsored by the American Society of Mechanical Engineers (ASME), Copenhagen, Denmark, June 11-15, 2012.
General note	"GT2012-70017."
General note	GPO Cataloging Record Distribution Program (CRDP).
Bibliography note	Includes bibliographical references (page 10).
Funding information	E-18550
Funding information	Sponsored by the National Aeronautics and Space Administration, Washtingon, DC WBS 284848.02.06.03.02
GPO item number	0830-D (online)
Govt. docs number	NAS 1.15:2012-217814

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Reducing conservatism in aircraft engine response using conditionally active min-max limit regulators / Ryan D. May, Sanjay Garg.

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