satellite1.sa

来自「STK航空仿真程序」· SA 代码 · 共 501 行 · 第 1/5 页

SA
501 行
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stk.v.4.3BEGIN SatelliteName		Satellite1BEGIN 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 TwoBodyBEGIN 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 PassesEND PassDefnEND VehiclePathBEGIN EphemerisNumberOfEphemerisPoints 1441ScenarioEpoch           1 Jun 2002 12:00:00.000000000InterpolationMethod     LagrangeInterpolationOrder      5CentralBody             EarthCoordinateSystem        Fixed BlockingFactor          20EphemerisTimePosVel
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satellite1.sa - 源码说明

本页面展示了「STK航空仿真程序」中的 satellite1.sa 源码文件，采用 SA 编程语言编写，共 501 行代码。您可以在线阅读完整代码内容，也可以返回资源详情页下载完整源码包进行本地学习和开发。

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