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MARC record from Internet Archive

LEADER: 02872cam 2200397 a 45 0
001 ocm640618250
005 19950204104459.0
007 c|br|dc|en|fu
008 920226s1994 cau f00000 eng d
037 $aADA283398
090 $aN4917
040 $aCMontNP$cCMontNP
100 10 $aNicholson, John C.
245 10 $aNumerical optimization of synergetic maneuvers /$c John C. Nicholson.
260 0 $aMonterey, Calif. :$bNaval Postgraduate School ;$aSpringfield, Va. :$bAvailable from National Technical Information Service,$c1994.
300 $a172 p. ;$c28 cm.
500 $aThesis advisor(s): I. Michael Ross.
500 $a."June 1994."
502 $aThesis (Degree of Aeronautical and Astronautical Engineer) Naval Postgraduate School, June 1994.
504 $aBibliography: p. 79-80.
506 $aApproved for public release; distribution unlimited.
520 $aThe use of atmospheric forces to produce an orbital plane change requires less energy than a pure exoatmospheric propulsion maneuver. The combination of aerodynamic and propulsive forces to cause a change in orbital inclination is termed a synergetic maneuver. Several methods have been proposed to control the critical heating rate while performing the procedure. This thesis examines these control methods by numerically optimizing the trajectory for several fuel weights and heat rate constraints. The Program to Optimize Simulated Trajectories (POST) is used to simulate the maneuvers and control schemes and to perform the optimization. For no active heat constraints, it is shown that a gliding atmospheric entry followed by a maximum throttle bang produces significantly more inclination change than other proposed maneuvers. If the heat constraints are active, the recently proposed aerobang maneuvers produces a substantial inclination change while providing significant heating rate control and shows definite advantages over the long-studied aerocruise maneuver.
530 $aAlso available online.
538 $aMode of access: World Wide Web.
538 $aSystem requirements: Adobe Acrobat Reader.
590 $aUS Navy (USN) author.
992 $aAERODYNAMIC FORCES, TRANSFER TRAJECTORIES, CONTROL, OPTIMIZATION, ENERGY, RATES, FUEL CONSUMPTION, HEAT, GLIDING, ATMOSPHERICS, AERODYNAMICS, SYNERGISM, MANEUVERS, THESES, FUELS, HEATING, WEIGHT.
992 $aIDE: POST(PROGRAM TO OPTIMIZE SIMULATED TRAJECTORIES), FUEL EFFICIENCY
856 41 $uhttp://handle.dtic.mil/100.2/ADA283398 $zWorks best in Firefox.
998 $adk/dk cc:9996
949 $lthes$nT$aN4917$s1$tnorm$u00001$i32768003118696
999 $a N4917 $i32768003118696$hTHESIS$wT
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999 $a N4917 $i32768003030453$hTHESIS$wT
926 $aNPS-LIB$bDIGIPROJ$cN4917$dTHESIS$eNEVER$f1
926 $aNPS-LIB$bNPSARCHIVE$cN4917$dTHESIS$f2