OpmData

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total1 of 12699%1 of 1291%118035012
hasManeuvers()1787%1150%120101
validate(double)62100%10100%0601601
OpmData(StateVector, KeplerianElements, SpacecraftParameters, CartesianCovariance, List, UserDefined, double)24100%n/a010901
getManeuver(int)6100%n/a010101
getNbManeuvers()4100%n/a010101
getManeuvers()4100%n/a010101
getStateVectorBlock()3100%n/a010101
getKeplerianElementsBlock()3100%n/a010101
getSpacecraftParametersBlock()3100%n/a010101
getCovarianceBlock()3100%n/a010101
getMass()3100%n/a010101
getUserDefinedBlock()3100%n/a010101