sat.sa

STK在计算机仿真中的应用程序第十九个程序

stk.v.5.0

BEGIN Satellite

Name		Sat

BEGIN VehiclePath
	CentralBody				Earth

    BEGIN Interval

         StartTime            1 Jun 2003 12:00:00.000000000
         StopTime             2 Jun 2003 12:00:00.000000000

    END Interval

	StoreEphemeris				Yes
	SmoothInterp				No

    BEGIN J4Perturbation

    EphemEpoch          1 Jun 2003 12:00:00.000000000

    StartTime           1 Jun 2003 12:00:00.000000000
    StopTime            2 Jun 2003 12:00:00.000000000
    SemiMajorAxis       0.000000000000e+000
    AltitudeOfApogee    0.000000000000e+000
    AltitudeOfPerigee   0.000000000000e+000
    RadiusOfApogee      0.000000000000e+000
    RadiusOfPerigee     6.878137000000e+006
    PeriodOfOrbit       0.000000000000e+000
    MeanMotion          0.000000000000e+000
    Inclination         4.500000000000e+001
    Eccentricity        0.000000000000e+000
    ArgOfPerigee        0.000000000000e+000
    LongAscenNode       2.904824963282e+002
    RightAscension      0.000000000000e+000
    TrueAnomaly         0.000000000000e+000
    MeanAnomaly         0.000000000000e+000
    TimePastAscenNode   0.000000000000e+000
    TimePastPerigee     0.000000000000e+000
    TimeStep            60.000000
    OrbitGranularity    0.000000000000e+000
    NumberOfPasses      0

    DisplayCoordType    4
    DisplayCoordSys     J2000
    EllipseType         Osculating
    BEGIN DisplayFlags
        SizeShapeType       SMAEcc
        AscenNodeType       RightAscension
        AnomalyType         TrueAnomaly
        DelLType            L
        DelGType            G
        DelHType            H
        EquiOrbType         SMA
        FPAType             HorizontalFPA
        MixFPAType          HorizontalFPA
    END DisplayFlags

    END J4Perturbation

BEGIN PassDefn

    Break               Ascending
    CoordSystem         Inertial
    BreakType           Latitude
    BreakAngle          0.000000000000e+000
    PartialPassMethod   ByMeanArgLatitude
    DisplayFlag         Both
    FirstPass           1
    FirstPath           1
    RepeatCycle         1
    MaintainPassNum     No
    RangeFirstPass      1
    RangeLastPass       2147483647
    DisplayScheme       AllEphemeris
    ScenarioEpoch       1 Jun 2003 12:00:00.00
    Passes
    END Passes
END PassDefn

END VehiclePath

BEGIN Ephemeris

NumberOfEphemerisPoints 1441

ScenarioEpoch           1 Jun 2003 12:00:00.00

InterpolationMethod     Lagrange

InterpolationSamplesM1      5

CentralBody             Earth

CoordinateSystem        Fixed 

BlockingFactor          20

EphemerisTimePosVel