FieldSpacecraftState

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total220 of 97277%12 of 5076%116639163341
interpolate(FieldAbsoluteDate, Stream)1280%60%44222211
lambda$interpolate$0(FieldAbsoluteDate, List, List, FieldHermiteInterpolator, Map, FieldSpacecraftState)720%20%22131311
shiftedBy(double)170%n/a111111
ensureCompatibleAdditionalStates(FieldSpacecraftState)39696%4866%4731501
FieldSpacecraftState(Field, SpacecraftState)180100%14100%0802801
toSpacecraftState()70100%6100%0401001
checkConsistency(FieldOrbit, FieldAttitude)53100%4100%030801
FieldSpacecraftState(FieldOrbit, FieldAttitude, RealFieldElement, Map)51100%4100%0301201
addAdditionalState(String, RealFieldElement[])30100%n/a010401
FieldSpacecraftState(FieldOrbit)25100%n/a010401
FieldSpacecraftState(FieldOrbit, Map)25100%n/a010401
getAdditionalState(String)24100%2100%020301
toTransform()24100%n/a010401
FieldSpacecraftState(FieldOrbit, RealFieldElement)18100%n/a010301
FieldSpacecraftState(FieldOrbit, RealFieldElement, Map)18100%n/a010301
shiftedBy(RealFieldElement)16100%n/a010101
FieldSpacecraftState(FieldOrbit, FieldAttitude)14100%n/a010201
FieldSpacecraftState(FieldOrbit, FieldAttitude, Map)14100%n/a010201
FieldSpacecraftState(FieldOrbit, FieldAttitude, RealFieldElement)7100%n/a010201
hasAdditionalState(String)5100%n/a010101
getPVCoordinates(Frame)5100%n/a010101
getDate()4100%n/a010101
getFrame()4100%n/a010101
getAdditionalStates()4100%n/a010101
getMu()4100%n/a010101
getKeplerianPeriod()4100%n/a010101
getKeplerianMeanMotion()4100%n/a010101
getA()4100%n/a010101
getEquinoctialEx()4100%n/a010101
getEquinoctialEy()4100%n/a010101
getHx()4100%n/a010101
getHy()4100%n/a010101
getLv()4100%n/a010101
getLE()4100%n/a010101
getLM()4100%n/a010101
getE()4100%n/a010101
getI()4100%n/a010101
getPVCoordinates()4100%n/a010101
getOrbit()3100%n/a010101
getAttitude()3100%n/a010101
getMass()3100%n/a010101