ti_mo
12 lines
715 B
Matlab
12 lines
715 B
Matlab
function satSim = create_satellite_sim(satConfig, stationConfig)
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satSim.sc = satelliteScenario;
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satSim.sc.StartTime = satConfig.startTime;
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satSim.sc.StopTime = satConfig.stopTime;
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satSim.sc.SampleTime = satConfig.sampleTime;
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earthRadius = physconst("EarthRadius");
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semiMajorAxis = earthRadius + satConfig.satAltitude;
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satSim.sat = satellite(satSim.sc, semiMajorAxis, satConfig.eccentricity, satConfig.inclination, satConfig.raan, satConfig.argOfPeriapsis, satConfig.trueAnomaly, Name=satConfig.name, OrbitPropagator=satConfig.orbitPropagator);
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satSim.ue = groundStation(satSim.sc, stationConfig.Lat, stationConfig.Lon, Altitude=stationConfig.Altitude, Name=stationConfig.Name);
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end |