SpacecraftState

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total139 of 1,09187%15 of 9283%189720179351
checkConsistency(AbsolutePVCoordinates, Attitude)361529%2250%235801
toString()270%n/a111111
interpolate(AbsoluteDate, Stream)2312884%3975%3752901
SpacecraftState(AbsolutePVCoordinates, double)180%n/a113311
getAbsPVA()7646%1150%121301
getOrbit()7646%1150%121301
SpacecraftState(AbsolutePVCoordinates, Attitude)70%n/a112211
lambda$interpolate$0(AbsoluteDate, List, List, List, HermiteInterpolator, Map, SpacecraftState)56292%1375%1311101
getPVCoordinates(Frame)4969%1150%120101
ensureCompatibleAdditionalStates(SpacecraftState)9898%21083%2711501
getA()888%1150%120101
getEquinoctialEx()888%1150%120101
getEquinoctialEy()888%1150%120101
getE()888%1150%120101
SpacecraftState(Orbit, Attitude, double, Map)53100%4100%0301301
SpacecraftState(AbsolutePVCoordinates, Attitude, double, Map)53100%4100%0301301
checkConsistency(Orbit, Attitude)51100%4100%030801
addAdditionalState(String, double[])44100%2100%020601
shiftedBy(double)35100%2100%020301
getAdditionalState(String)24100%2100%020301
toTransform()24100%n/a010401
SpacecraftState(Orbit)18100%n/a010301
SpacecraftState(Orbit, double)18100%n/a010301
SpacecraftState(Orbit, Map)18100%n/a010301
SpacecraftState(Orbit, double, Map)18100%n/a010301
SpacecraftState(AbsolutePVCoordinates)18100%n/a010301
SpacecraftState(AbsolutePVCoordinates, Map)18100%n/a010301
SpacecraftState(AbsolutePVCoordinates, double, Map)18100%n/a010301
writeReplace()15100%2100%020101
getDate()11100%2100%020101
getFrame()11100%2100%020101
getPVCoordinates()11100%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)7100%n/a010201
SpacecraftState(Orbit, Attitude, double)7100%n/a010201
SpacecraftState(Orbit, Attitude, Map)7100%n/a010201
SpacecraftState(AbsolutePVCoordinates, Attitude, double)7100%n/a010201
SpacecraftState(AbsolutePVCoordinates, Attitude, Map)7100%n/a010201
isOrbitDefined()7100%2100%020101
hasAdditionalState(String)5100%n/a010101
getAdditionalStates()4100%n/a010101
getAttitude()3100%n/a010101
getMass()3100%n/a010101