FieldSpacecraftState

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total130 of 1,76492%13 of 12289%1511413257253
toString()270%n/a111111
FieldSpacecraftState(FieldAbsolutePVCoordinates, CalculusFieldElement)180%n/a113311
checkConsistency(FieldAbsolutePVCoordinates, FieldAttitude)173567%1375%132801
shiftedBy(double)162055%1150%121301
getEquinoctialEx()9847%1150%120101
getEquinoctialEy()9847%1150%120101
getE()9847%1150%120101
getAbsPVA()7646%1150%121301
getOrbit()7646%1150%121301
FieldSpacecraftState(Field, SpacecraftState)438798%12195%11215701
getPVCoordinates(Frame)4969%1150%120101
ensureCompatibleAdditionalStates(FieldSpacecraftState)9696%4866%4731501
interpolate(FieldAbsoluteDate, Stream)156100%12100%0702901
toSpacecraftState()87100%8100%0501401
lambda$interpolate$0(FieldAbsoluteDate, List, List, List, FieldHermiteInterpolator, Map, FieldSpacecraftState)72100%4100%0301201
FieldSpacecraftState(FieldOrbit, FieldAttitude, CalculusFieldElement, Map)54100%4100%0301301
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement, Map)53100%4100%0301301
checkConsistency(FieldOrbit, FieldAttitude)53100%4100%030801
addAdditionalState(String, CalculusFieldElement[])44100%2100%020601
shiftedBy(CalculusFieldElement)35100%2100%020301
FieldSpacecraftState(FieldOrbit)25100%n/a010401
FieldSpacecraftState(FieldOrbit, Map)25100%n/a010401
FieldSpacecraftState(FieldAbsolutePVCoordinates)25100%n/a010401
FieldSpacecraftState(FieldAbsolutePVCoordinates, Map)25100%n/a010401
getAdditionalState(String)24100%2100%020301
toTransform()24100%n/a010401
FieldSpacecraftState(FieldOrbit, CalculusFieldElement)18100%n/a010301
FieldSpacecraftState(FieldOrbit, CalculusFieldElement, Map)18100%n/a010301
FieldSpacecraftState(FieldAbsolutePVCoordinates, CalculusFieldElement, Map)18100%n/a010301
getMu()17100%2100%020101
getKeplerianPeriod()17100%2100%020101
getKeplerianMeanMotion()17100%2100%020101
getA()17100%2100%020101
getHx()17100%2100%020101
getHy()17100%2100%020101
getLv()17100%2100%020101
getLE()17100%2100%020101
getLM()17100%2100%020101
getI()17100%2100%020101
FieldSpacecraftState(FieldOrbit, FieldAttitude)14100%n/a010201
FieldSpacecraftState(FieldOrbit, FieldAttitude, Map)14100%n/a010201
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude)14100%n/a010201
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, Map)14100%n/a010201
getDate()11100%2100%020101
getFrame()11100%2100%020101
getPVCoordinates()11100%2100%020101
FieldSpacecraftState(FieldOrbit, FieldAttitude, CalculusFieldElement)7100%n/a010201
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement)7100%n/a010201
isOrbitDefined()7100%2100%020101
hasAdditionalState(String)5100%n/a010101
getAdditionalStates()4100%n/a010101
getAttitude()100%n/a010101
getMass()100%n/a010101