轨道转移飞行器轨迹优化与制导分析

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1、-------Abstracttheeffectofdifferentheliocentricvelocityisconsidered,andconsideringtheinfluenceofaeroheat,theconvectiveheatingratesofthevehicleisconstraint.Simulationresultshowsthat,comparedwiththesituationwithoutrestraint,theprovidedturningangleandheliocentricvelocityincrementarealldecrea

2、sed.Sowhenwedesigntheoptimaltrajectoriesforvehicles,weshouldnotonlymaketheperformancefunctionoptimal,butalsokeepconvectiveheatingratesinaaffordableleveltothevehiclesduringaflight,toavoiddoingthermaldamagetothem.Finally,combinedatmosphericguidancemethodisusedfortheaero-gravityassistorbital

3、maneuverproblemresearch,andtheeffectivenessofthealgorithmisverifiedthroughsimulation.Inconclusion,inthisthesis,wehavemadeatheoreticalanalysisonsomerelatedissueslikedynamicmodeling,trajectoryoptimizationandguidanceoftheorbitaltransfervehicle,andmaderesearchanddiscussionontheseproblemsbycom

4、biningtrajectoryoptimizationmethodwithsimulationtechnology.ThisresearchwillplayanimportantrolewhenitappliedinChina’sspacetransportationsystem.Keywords:orbitaltransfervehicle,dynamicmodeling,trajectoryoptimization,combinedatmosphericguidance,thepsedospectralmethod-III------------目录目录摘要....

5、...................................................................................................................IAbstract.............................................................................................................................II第1章绪论.................................

6、................................................................................11.1课题来源及研究意义...........................................................................................11.2课题国内外研究现状...........................................................................................2

7、1.2.1OTV的研究现状.............................................................................................21.2.2气动辅助轨道转移（AOT）机动国内外研究现状....................................31.2.3气动引力辅助（AGA）轨道机动国内外现状...........................................41.3本文研究内容及安排..............