SpacecraftState

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total107 of 1,48692%12 of 12690%1413013257267
checkConsistency(AbsolutePVCoordinates, Attitude)361529%2250%235801
toString()320%n/a111111
SpacecraftState(AbsolutePVCoordinates, double)190%n/a113311
getAbsPVA()7646%1150%121301
getOrbit()7646%1150%121301
ensureCompatibleAdditionalStates(SpacecraftState)219398%42083%41323101
getA()888%1150%120101
getEquinoctialEx()888%1150%120101
getEquinoctialEy()888%1150%120101
getE()888%1150%120101
interpolate(AbsoluteDate, Stream)217100%18100%01004201
lambda$interpolate$0(AbsoluteDate, List, List, List, HermiteInterpolator, Map, Map, SpacecraftState)94100%6100%0401401
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
toTransform()24100%n/a010401
getAdditionalState(String)21100%2100%020401
getAdditionalStateDerivative(String)21100%2100%020401
SpacecraftState(Orbit)19100%n/a010401
SpacecraftState(Orbit, double)19100%n/a010401
SpacecraftState(AbsolutePVCoordinates)19100%n/a010301
SpacecraftState(Orbit, DoubleArrayDictionary)18100%n/a010401
SpacecraftState(Orbit, double, DoubleArrayDictionary)18100%n/a010301
SpacecraftState(AbsolutePVCoordinates, DoubleArrayDictionary)18100%n/a010301
SpacecraftState(AbsolutePVCoordinates, double, DoubleArrayDictionary)18100%n/a010301
writeReplace()15100%2100%020101
getPVCoordinates(Frame)13100%2100%020101
getDate()11100%2100%020101
getFrame()11100%2100%020101
getPVCoordinates()11100%2100%020101
SpacecraftState(Orbit, Attitude, double, Map)10100%n/a010201
SpacecraftState(AbsolutePVCoordinates, Attitude, double, Map)10100%n/a010201
SpacecraftState(Orbit, Attitude, Map)9100%n/a010201
SpacecraftState(Orbit, double, Map)9100%n/a010201
SpacecraftState(AbsolutePVCoordinates, Attitude, Map)9100%n/a010201
SpacecraftState(AbsolutePVCoordinates, double, Map)9100%n/a010201
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, Map)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, Map)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
getAdditionalStates()4100%n/a010101
getAdditionalStatesValues()4100%n/a010101
getAdditionalStatesDerivatives()4100%n/a010101
getAttitude()3100%n/a010101
getMass()3100%n/a010101