SpacecraftState

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total1 of 654100%2 of 3294%2541116038
ensureCompatibleAdditionalStates(SpacecraftState)9899%21083%2711501
interpolate(AbsoluteDate, Collection)174100%10100%0602801
checkConsistency(Orbit, Attitude)51100%4100%030801
SpacecraftState(Orbit, Attitude, double, Map)50100%4100%0301201
addAdditionalState(String, double[])30100%n/a010401
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
shiftedBy(double)16100%n/a010101
SpacecraftState(Orbit, Attitude)7100%n/a010201
SpacecraftState(Orbit, Attitude, double)7100%n/a010201
SpacecraftState(Orbit, Attitude, Map)7100%n/a010201
writeReplace()6100%n/a010101
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