SpacecraftState

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total112 of 1,10489%14 of 10686%1611313183260
checkConsistency(AbsolutePVCoordinates, Attitude)361529%2250%235801
toString()320%n/a111111
SpacecraftState(AbsolutePVCoordinates, double)160%n/a113311
getAbsPVA()7646%1150%121301
getOrbit()7646%1150%121301
getPosition(Frame)4969%1150%120101
getPVCoordinates(Frame)4969%1150%120101
ensureCompatibleAdditionalStates(SpacecraftState)219398%42083%41323101
getA()888%1150%120101
getEquinoctialEx()888%1150%120101
getEquinoctialEy()888%1150%120101
getE()888%1150%120101
checkConsistency(Orbit, Attitude)51100%4100%030801
SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary)46100%4100%0301301
SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary, DoubleArrayDictionary)43100%4100%0301301
addAdditionalState(String, double[])41100%2100%020501
addAdditionalStateDerivative(String, double[])41100%2100%020501
shiftedBy(double)41100%2100%020501
shiftAdditional(double)39100%6100%040901
getAdditionalState(String)21100%2100%020401
getAdditionalStateDerivative(String)21100%2100%020401
SpacecraftState(Orbit)16100%n/a010301
SpacecraftState(Orbit, double)16100%n/a010301
SpacecraftState(AbsolutePVCoordinates)16100%n/a010301
SpacecraftState(Orbit, DoubleArrayDictionary)15100%n/a010301
SpacecraftState(Orbit, double, DoubleArrayDictionary)15100%n/a010301
SpacecraftState(AbsolutePVCoordinates, DoubleArrayDictionary)15100%n/a010301
SpacecraftState(AbsolutePVCoordinates, double, DoubleArrayDictionary)15100%n/a010301
writeReplace()15100%2100%020101
toTransform()14100%n/a010201
getDate()11100%2100%020101
getFrame()11100%2100%020101
getPosition()11100%2100%020101
getPVCoordinates()11100%2100%020101
toStaticTransform()10100%n/a010101
hasAdditionalState(String)9100%2100%020101
hasAdditionalStateDerivative(String)9100%2100%020101
getMu()9100%2100%020101
getKeplerianPeriod()9100%2100%020101
getKeplerianMeanMotion()9100%2100%020101
getHx()9100%2100%020101
getHy()9100%2100%020101
getLv()9100%2100%020101
getLE()9100%2100%020101
getLM()9100%2100%020101
getI()9100%2100%020101
SpacecraftState(Orbit, Attitude)8100%n/a010201
SpacecraftState(Orbit, Attitude, double)8100%n/a010201
SpacecraftState(Orbit, Attitude, double, DoubleArrayDictionary)8100%n/a010201
SpacecraftState(AbsolutePVCoordinates, Attitude)8100%n/a010201
SpacecraftState(AbsolutePVCoordinates, Attitude, double)8100%n/a010201
SpacecraftState(AbsolutePVCoordinates, Attitude, double, DoubleArrayDictionary)8100%n/a010201
SpacecraftState(Orbit, Attitude, DoubleArrayDictionary)7100%n/a010201
SpacecraftState(AbsolutePVCoordinates, Attitude, DoubleArrayDictionary)7100%n/a010201
isOrbitDefined()7100%2100%020101
getDefaultAttitudeProvider(Frame)5100%n/a010101
getAdditionalStatesValues()4100%n/a010101
getAdditionalStatesDerivatives()4100%n/a010101
getAttitude()3100%n/a010101
getMass()3100%n/a010101