secular trends of perturbations explored numerically

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Oblateness trends,Orbits,Satellite,Visual

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  • ResultsOblatenessTrendsAsimulationwasrunfor25orbits,giventhefollowinginitialorbitalelements:

    Oncethesimulationswerecomplete,orbitalelementswerecalculatedfromthepositionandvelocitytimehistories.

    Above:Changeininitialorbitduetooblatenessperturbation.Below:Animationofchangeinorbitovertime.

    Secular Trends of Perturbations Explored NumericallyKyle Litzer CU Boulder ASEN 5050

    Home | Overview | Oblateness | Atmospheric Drag | Solar Radiation Pressure | Results | Code | References

  • Above:Timehistoryofsemimajoraxis,eccentricity,radiusofperigee,andradiusofapogee.Below:Timehistoryofinclination,rightascensionoftheascendingnode,andargumentofperiapse.

  • Asseenabove,semimajoraxis,eccentricity,radiusofapogee,radiusofperigeeandinclinationareallunaffectedsecularlybyoblateness.Thereisauniquetradeoffwitnessedbetweenradiusatapogeeandperigee.Whenoneisataminimum,theotherisatamaximum.

    Aspredictedanalytically,thetimehistoriesshowaseculartrendinbothrightascensionoftheascendingnode(RAAN)andduringtheapproximately65hoursimulationtimespan.RAANdecreasesbyapprox.7.5,whileargumentofperiapserisesbyapprox.13.

    Asmentionedbefore,inhistextValladogivesanalyticalexpressionsfortheseculartrendsintheorbitalelementsduetotheoblatenessofEarth.ItisshownthattheonlyorbitalelementsaffectedinasecularwayaretheRAAN,theargumentofperiapseandthereference(initial)meananomaly.

    Comparingtheseequationstothebehaviorwitnessedabove,thenetchangeinRAANandargumentofperiapseagreewiththeanalyticalexpressions.

    DragTrendsAsimulationwasrunfor100orbits,giventhefollowinginitialorbitalelements:

    Oncethesimulationswerecomplete,orbitalelementswerecalculatedfromthepositionandvelocitytimehistories.

  • Above:Changeininitialorbitduetodragperturbation.Below:Animationofchangeinorbitovertime.

  • Above:Timehistoryofsemimajoraxis,eccentricity,radiusofperigee,andradiusofapogee.Below:Timehistoryofinclination,rightascensionoftheascendingnode,andargumentofperiapse.

  • Above:Detailoftimehistoryofsemimajoraxis,eccentricity,radiusofperigee,andradiusofapogee.Below:Detailoftimehistoryofinclination,rightascensionoftheascendingnode,andargumentofperiapse.

    Theperturbationsduetodragyieldquiteinterestingresults.Allsevenelementsplottedfollowadefiniteseculartrend.Allsixelementsasidefromargumentofperiapseshowadownwardtrend.ItalmostappearsasiftheorbitistryingtoalignitsperigeedirectiontobecomeparallelwithtotheEarth/Sundirection.Themagnitudeofchangeinradiusofapogeeversusperigeeshouldalsobenoted.Thenetchangeinapogeeisontheorderof30km,whilethenetchangeinperigeeisontheorderof200m.Thiscanbeconceptuallyverifiedifwecomparethelossofspeedduetodragwithacircularizingantivelocitydirectionburnperformedatperiapse.Sinceperiapseisthemostefficientplacetoperformorbitchangingmaneuvers(duetohighspeeds),smallerchangesinvelocityatperigeebecomelargerchangesintheorbit,especiallyatapogee.

    Uponcloserinspection(referringtothezoomedinplots),itcanbeseenthattheelementsallremainrelativelyunchanging.Sincethisorbitiseccentric,andasareasonablylowperigeealtitudethatdipssignificantlyintotheEarthsatmosphere,theeffectsofdragareonlywitnessedduringshortspurtsoftimeneartheorbitsperigee.Curiously,theargumentofperiapsetimehistoryshowssharpspikeseverytimethespacecraftiswithintheatmosphere.Furtherinvestigationwouldneedtobeperformedtofindthereasonforsuchhighrateofchange.

    SolarRadiationPressureTrends

  • Asimulationwasrunfor100orbits,giventhefollowinginitialorbitalelements:

    Oncethesimulationswerecomplete,orbitalelementswerecalculatedfromthepositionandvelocitytimehistories.

    Above:ChangeininitialorbitduetoSRPperturbation.Below:Animationofchangeinorbitovertime.

  • Above:Timehistoryofsemimajoraxis,eccentricity,radiusofperigee,andradiusofapogee.Below:Timehistoryofinclination,rightascensionoftheascendingnode,andargumentofperiapse.

  • Theonlyoftheorbitalelementsinduringthissimulationthatshowsnoseculartrendisthesemimajoraxis.Itisverypeculiarthateventhougheccentricity,radiusofapogeeandperigeechange,thesemimajoraxisremainsrelativelyconstant.Furtherinvestigationwouldbenecessarytounderstandthisrelationship.

    ItcanalsobeseenthatthetrendsforRAANandargumentofperiapsemirrorthatoftheoblatenessperturbation.

    Finally,itshouldbetakenintoconsiderationthatthemagnitudeofsecularchangeintheorbitalelementsduetoSRPismuchsmallerinmagnitudethanthesecularchangesduetoEarthsoblateness.