satellite1.sa

STK航空仿真程序

stk.v.4.3

BEGIN Satellite

Name		Satellite1

BEGIN VehiclePath
	CentralBody				Earth

    BEGIN Interval

         StartTime            1 Jun 2002 12:00:00.000000000
         StopTime             2 Jun 2002 12:00:00.000000000

    END Interval

	StoreEphemeris				Yes
	SmoothInterp				No

    BEGIN TwoBody

    EphemEpoch          1 Jun 2002 12:00:00.000000000

    StartTime           1 Jun 2002 12:00:00.000000000
    StopTime            2 Jun 2002 12:00:00.000000000
    SemiMajorAxis       0.000000000000e+000
    AltitudeOfApogee    0.000000000000e+000
    AltitudeOfPerigee   0.000000000000e+000
    RadiusOfApogee      0.000000000000e+000
    RadiusOfPerigee     4.216416963714e+007
    PeriodOfOrbit       0.000000000000e+000
    MeanMotion          0.000000000000e+000
    Inclination         0.000000000000e+000
    Eccentricity        0.000000000000e+000
    ArgOfPerigee        0.000000000000e+000
    LongAscenNode       0.000000000000e+000
    RightAscension      1.697696437620e+002
    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       PeriodEcc
        AscenNodeType       Longitude
        AnomalyType         TrueAnomaly
        DelLType            L
        DelGType            G
        DelHType            H
        EquiOrbType         SMA
        FPAType             HorizontalFPA
        MixFPAType          HorizontalFPA
    END DisplayFlags

    END TwoBody

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 2002 12:00:00.000000000
    Passes
    END Passes
END PassDefn

END VehiclePath

BEGIN Ephemeris

NumberOfEphemerisPoints 1441

ScenarioEpoch           1 Jun 2002 12:00:00.000000000

InterpolationMethod     Lagrange

InterpolationOrder      5

CentralBody             Earth

CoordinateSystem        Fixed 

BlockingFactor          20

EphemerisTimePosVel