Aerospace Mechatronics and Control Technology: Selected Contributions from 2021 7th Asia Conference on Mechanical Engineering and Aerospace Engineering

187 Pages·2022·8.953 MB·English

by  Huafeng Ding

Springer Aerospace Technology
Huafeng Ding Editor
Aerospace
Mechatronics
and Control
Technology
Selected Contributions from 2021 7th
Asia Conference on Mechanical
Engineering and Aerospace Engineering
Springer Aerospace Technology
SeriesEditors
SergioDeRosa,DII,UniversityofNaplesFedericoII,NAPOLI,Italy
YaoZheng,SchoolofAeronauticsandAstronautics,ZhejiangUniversity,
Hangzhou,Zhejiang,China
ElenaPopova,AirNavigationBridgeRussia,Russia,Russia
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The volumes of the series present the fundamentals, the applications and the
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aerodynamics,
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aeroelasticity,
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aeroacoustics,
(cid:129)
flightmechanicsanddynamics
(cid:129)
orbitalmaneuvers,
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avionics,
(cid:129)
systemsdesign,
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materialstechnology,
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launchtechnology,
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payloadandsatellitetechnology,
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Huafeng Ding
Editor
Aerospace Mechatronics
and Control Technology
Selected Contributions from 2021 7th Asia
Conference on Mechanical Engineering
and Aerospace Engineering
Editor
HuafengDing
SchoolofMechanicalEngineering
andElectronicInformation
ChinaUniversityofGeosciences
Wuhan,Hubei,China
ISSN1869-1730 ISSN1869-1749 (electronic)
SpringerAerospaceTechnology
ISBN978-981-16-6639-1 ISBN978-981-16-6640-7 (eBook)
https://doi.org/10.1007/978-981-16-6640-7
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Preface
This proceeding records the papers presented at 2021 7th Asia Conference on
Mechanical Engineering and Aerospace Engineering (MEAE 2021), which was
held on June 11–13, 2021 in Wuhan, China. It’s organized by China University
of Geosciences (Wuhan) and hosted by School of Mechanical Engineering and
ElectronicInformationofCUG(Wuhan).
Thesuccessoftheconferenceisinseparablefromtheunremittingeffortsofadedi-
catedconferenceteamandthestrongsupportofChinaUniversityofGeosciences.We
inviteallsuccessfullyregisteredauthorsandlistenerstojoinus,interactwithkeynote
speakers and invited experts, and most importantly, interact with all fellow partic-
ipants. Without the hard work of many volunteers and the organizing committee,
therewouldbenosuchhigh-qualitymeeting.Inparticular,wewouldliketoexpress
oursincerethankstotheoutstandingsessionchairteamandTPCmembers.
ThesuccessofMEAE2021dependsonthecontributionsofmanyindividualsand
organizations. With that in mind, we thank all authors who submitted work to the
conference.Thequalityofsubmissionsthisyearremainshighandwearesatisfied
with the quality of the results procedure. The organizing committee also thanked
themembersoftheTechnicalPlanningCommitteeandthechairmanofthemeeting
fortheirstrongsupport.Theorganizingcommitteeisresponsibleforreviewers,who
voluntarily sacrifice valuable time to evaluate the manuscript and provide authors
withusefulfeedback.
Finally,wehopethatparticipantswilllikethisconferenceandhavetheopportunity
to establish contacts with colleagues from all over the world. We also hope that
all participants can learn from this conference and contribute more to your future
explorationandresearch.
Bestwishes,
Wuhan,China MEAEConferenceCommittee
v
Contents
AircraftControlandTesting
NumericalStudyonAerodynamicPerformanceofHypersonic
VehiclewithAerospikes ............................................ 3
YangXu,ShuZhouFang,andShuaiZhang
TerminalMulti-ConstrainedFiniteTimeSlidingModeGuidance
LawBasedonTruncationFunctionforHypersonicVehicle ............ 14
ShenghuiCui,ChengHu,XinbinBai,andShifengZhang
Dynamic Performance Test and System Identification of Air
RudderforBoost-GlideAircraft .................................... 26
XiaoshuaiFan,XibinBai,ZhenyuJiang,andShifengZhang
DSMCStudyforEffectsofAnglesofAttackonClosedCavity
ofSpaceVehicleinHypersonicRarefiedFlow ........................ 43
ShaoJinXiangandShuZhouFang
NewEngineDesignandDevelopment
TheCauseandEffectAnalysisofAero-EngineRollerBearing
SkidBasedonAssemblyProcessInspectionandTrialRun ............ 59
QingZhenGaoandDaoYuanPan
Dynamic Detection Method for Blade Tip Clearance
ofAero-EngineinAssembledStateBasedonLinearStructured
Light ............................................................. 67
GangZhao,MaochengXu,WenleiXiao,HuiWang,BingZhang,
andPengfeiZhang
An Aero-Engine Assembly Deviation Analysis Method Based
onSkinModelShapes ............................................. 78
GangZhao, JinyueLi, BingZhang, PengfeiZhang, HuiWang,
andWenleiXiao
vii
viii Contents
ParametersOnlineIdentificationandPredictionofSolidRocket
Motor ............................................................ 90
ZhenyuJiangandRundongMa
AerospaceandSatelliteEngineering
AMulti-missileCoverageInterceptionStrategy ...................... 105
BaoSong,JianqiaoYu,XiChen,KangNiu,andZiyuanLi
Design and Optimization of the Flexible Support Structure
forSpaceMirror .................................................. 119
YixuanSun,ShikuiLuo,JieBai,ZijiaLiu,andShaofanTang
Experimental Research on the Influence of the Bulk Swirl
ontheCompressor ................................................ 129
FengLu-ning,ChengBang-qin,WangJia-le,TaoPing,andWuQiang
TargetLocalizationonImage-GuidedMissile ........................ 140
HengboQi,SimeiJi,JunminZhao,JiyuNie,andChenruiNie
AttitudeUpdatingAlgorithmBasedonAgileMicro-NanoSatellites .... 156
YajingChen,YunFei,TaoMeng,andZhongheJin
Autonomous Navigation and Attitude Determination System
DesignforMicro-NanoSatelliteswithLimitedSensors ................ 167
ChaoyuDu,TaoMeng,JunWang,andZhongheJin
AuthorIndex ...................................................... 181
Aircraft Control and Testing
Numerical Study on Aerodynamic Performance
of Hypersonic Vehicle with Aerospikes
B
YangXu( ),ShuZhouFang,andShuaiZhang
SchoolofAerospaceandEngineering,BeijingInstituteofTechnology,Beijing100081,China
[email protected], [email protected]
Abstract. Thedragandheatfluxreductionhavebecomeanincreasingcrucial
characteristicforthehypersonicvehicles.Numericalsimulationsofthehypersonic
flow around the blunt body with aerospike are investigated for the aerospike’s
changingL/DratioswithfreedomMachnumberof5.75.Theeffectofthecharac-
teristicsoftheflowfieldandtheaerospike’sL/Dratiosonthedragcoefficientof
modelandthesurfacepressurecoefficientofthenoseconeareanalysedusinga
two-dimensionalaxisymmetricReynolds-averagedNavier–Stokes(RANS)equa-
tionscoupledwiththetwoequationk-ωshearstresstransport(SST)turbulence
model.Thenumericalsimulationresultsshowthattheinstallationoftheaerospike
changestheflowfieldstructureofthebluntbodyvehiclehead,whichreducesthe
dragofthebluntbodyvehiclesignificantlyinhypersonicflight.Thesizeofthe
recirculationregiondependsontheaerospike’sL/Dratios.Amongthedifferent
aerospikeconfigurationsstudied,thedragreductioneffectofaerospikewhenthe
L/D=1isthebest,andthemaximumvalueofthedragreductionefficiencyis
36.4%.Withinthescopeofthisstudy,astheL/Dratiooftheaerospikeincreases,
thedragreductionefficiencyincreasesgradually.
Keywords: Hypersonicflow·Aerospike·Dragreduction
1 Introduction
Hypersonicvehiclewillencounterseriousaerodynamicdragandaerodynamicheating
when it re-enters the atmosphere. The severe aerodynamic heating phenomenon will
damagetheinternalelectronicequipmentofthevehicle,andthehugeshockwavedrag
alsohindersfurtherimprovementofthevehiclespeed.Hence,thestudyofheatfluxand
dragreductionofhypersonicvehicleisofgreatsignificancetothehypersonicvehicle’s
aerodynamicperformanceandsafetyperformance.
Agreatdealofthermalprotectionmethodsanddragreductiontechniqueswerepro-
posedandstudiedindetail.Forexample,theforward-facingcavity[1],counterflowing
jet [2], the energy deposition [3] and the different combinations of them [4]. Besides
the methods above, attaching an aerospike to the head of the vehicle which flights at
hypersonicspeedappearstobeasimplesttechniquewhichalsohasahigherefficiency.
Theexperimentalinvestigationsoftheaerospikestructurebeganinthe1950s.
Kalimuthu et al. [5] studied the effects of hemispherical model with aerospike on
drag reduction, and the parameters of model in detail. The experimental data indicate
©TheAuthor(s),underexclusivelicensetoSpringerNatureSingaporePteLtd.2022
H.Ding(ed.),AerospaceMechatronicsandControlTechnology,SpringerAerospaceTechnology,
https://doi.org/10.1007/978-981-16-6640-7_1