GPSPropagator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total105 of 61883%6 of 1866%102519100516
eMeSinE(DerivativeStructure)540%20%22101011
getEccentricAnomaly(DerivativeStructure)2721188%3975%3743001
resetInitialState(SpacecraftState)70%n/a111111
resetIntermediateState(SpacecraftState, boolean)70%n/a111111
getTk(AbsoluteDate)52180%1375%131601
getFrame()30%n/a111111
getMU()20%n/a111111
propagateInEcef(AbsoluteDate)178100%n/a0102601
GPSPropagator(GPSPropagator.Builder)33100%n/a010801
getTrueAnomaly(DerivativeStructure)25100%n/a010301
propagateOrbit(AbsoluteDate)22100%n/a010301
static {...}11100%n/a010601
getGPSOrbitalElements()3100%n/a010101
getECI()3100%n/a010101
getECEF()3100%n/a010101
getMass(AbsoluteDate)3100%n/a010101