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Satellite Orbit and Ephemeris Determination using Inter Satellite Links

Satellite Orbit and Ephemeris Determination using Inter Satellite Links

Satellite Orbit and Ephemeris Determination using Inter Satellite Links

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<strong>Inter</strong> <strong>Satellite</strong> <strong>Links</strong>J2Earths Oblateness CoefficientJGM-2/3 Joint Gravity Model (Type 2 or 3)JPLJet Propulsion LaboratoryLEOLow Earth <strong>Orbit</strong>LOSLine of SightMEOMedium Earth <strong>Orbit</strong>MMHMonometyl-HydrazinMOPSMinimum Operational Performance St<strong>and</strong>ardsMSASMSAT Space Augmentation SystemNO GO Integrity Flag State (= Unhealthy)NTONitro-TetroxideOCSOperational Control SystemPLLPhase Lock LoopPRPseudo RangePRARE Precise Range <strong>and</strong> Range-Rate EquipmentRAIMReceiver Autonomous Integrity MonitoringRKRunge-KuttaRMSRoot Mean SquareS/CSpacecraftS/VSpace VehicleSBASSpace Based Augmentation SystemSDMASpace Division Multiple AccessTDMATime Division Multiple AccessTECTotal Elctron Content (of the Ionosphere)UREUser Range ErrorUTUniversal TimeUT1Universal Time 1(Siderial Time)UTCUniversal Time CoordinatedWAASWide Area Augmentation SystemWGS-84 World Geodetic System of 1984XIPSXenon Ion Propulsion SystemR. Wolf Page xi

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