可控结构半弹道式再入飞行器的跟踪及充满空间的模型集设计

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1、136ò111ÏgÄzÆVol.36,No.11201011ACTAAUTOMATICASINICANovember,2010(ª21ìl9¿÷m.8111ù℄Û¸Âè℄Ádu2§¥(Cz±96

2、Ø(½ÏǑ,C(ª21ì(Semi-ballisticreentryvehicle,SBRV)ª9ÙCzªÏ~Ǒ´.©3©Û(SBRV2$ÄAƱ9ªAÆÄ:þ,Ñ¿÷ªm.8,#.8âHicknell,T.8MonteCarlo{)¤.8'Øäkp&ÝÚ°Ý,éÅÄA(¯.nØ©

3、ÛÚý(y²ù«¿÷m.8éuTÅÄl¯Ün5k5.'ª21ì,·ÜXÚ,õ.{,MonteCarlo{,¿÷m.8DOI10.3724/SP.J.1004.2010.01534Controllable-structureSemi-ballisticReentryVehicleTrackingandSpace-fillingModel-setDesign111LIANGYong-QiHANChong-ZhaoSHIYongAbstractDuetouncertaintyinstructureanduncertaintyofflowfield,t

4、hemodeofthecontrollable-structuresemi-ballisticreentryvehicle(SBRV)isusuallyunknown.Basedontheanalysisofthecharacteristicsofthecontrollable-′structureSBRVsmotionandmode,thespace-fillingmodelsetisproposed.Thenewmodelsetisdesignedaccordingto′Hicknellscriterion.Comparedwiththemodelsetgen

5、eratedbytheMonteCarlomethod,thenewmodelsethasahighercredibilityandasmallerestimationerror,andismoresensitivetomaneuver.Theoreticalanalysisandsimulationresultsshowthereasonablenessandefficiencyofthespace-fillingmodelsetforthemaneuvertrackingproblem.KeywordsSemi-ballisticreentryvehicle(SB

6、RV),hybridsystem,multiple-modelapproach,MonteCarlomethod,uni-formmodelset28
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9、,½(2,2§¥SBRV/Ú(ëY¤©¡Ä,ÙCz´ëY;lѤ©¡CzÙ;,!á:±91Cz,Óª,ÙCz´lÑ.¤±SBRV2§G(:Äk,1ì(Ú/Czþ´«·ÜXÚ.·ÜXÚÌ6{Ǒm!ª9rÝÏ~´;Ùg,6

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[9]ÂvFÏ2009-12-04¹^FÏ2010-07-01ManuscriptreceivedDecember4,2009;acceptedJuly1,2010l
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