MARC record from Internet Archive

LEADER: 01829nam 2200277 a 4500
001 ocn640943641
005 20100714110349.2
008 000516s1992 cau b f000|0 eng d
035 $a
035 $a
040 $aCMontNP$cCMontNP
100 1 $aMiller, Kurtis Brett.
245 10 $aDesign of robust suboptimal controllers for a generalized quadratic criterion.
260 $aMonterey, Calif. :$bNaval Postgraduate School ;$aSpringfield, Va. :$bAvailable from National Technical Information Service,$c1992.
300 $aviii, 57 p. ;$c28 cm.
500 $aThesis advisor, Won-Zon Chen.
500 $aAD-A257 746.
502 $aThesis (M.S. in Electrical Engineering) Naval Postgraduate School, June 1992.
504 $aIncludes bibliographical references (p. 56)
520 $aStandard linear quadratic regulator (LQR) designs guarantee a certain level of robustness. However, optimizing a generalized quadratic criterion produces coupled state and input terms and there are no longer any guarantees of good robustness properties. This thesis identifies how this problem arises and then presents several suboptimal, but robust controller design options which provide the control systems engineer with the ability to perform a trade-off between performance and robustness. The effectiveness of these methods is investigated and the trade-offs between performance and robustness are evaluated using computer simulation of a statically unstable fighter aircraft. Linear Quadratic Feedback Control System, Robust Control, Optimal Control, Suboptimal Control.
650 4 $aCONTROL SYSTEMS.
650 4 $aFIGHTER AIRCRAFT.
650 4 $aAERODYNAMIC STABILITY.
592 $adk/dk cc:9116 re-cataloged 5/16/00 (gutted record)
926 $aNPS-LIB$bDIGIPROJ$cM58755$dTHESIS$eNEVER$f1
926 $aNPS-LIB$bNPSARCHIVE$cM58755$dTHESIS$f2