OrbitPhysicalProperties

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 316100%0 of 4100%0540108052
setInertiaMatrixEntry(int, int, double)31100%2100%020701
getManeuversPerYear()13100%2100%020101
OrbitPhysicalProperties(AbsoluteDate, CcsdsFrameMapper)10100%n/a010301
setDragConstantArea(double)7100%n/a010301
setDragCoefficient(double)7100%n/a010301
setDragUncertainty(double)7100%n/a010301
setInitialWetMass(double)7100%n/a010301
setWetMass(double)7100%n/a010301
setDryMass(double)7100%n/a010301
setMinAreaForCollisionProbability(double)7100%n/a010301
setMaxAreaForCollisionProbability(double)7100%n/a010301
setTypAreaForCollisionProbability(double)7100%n/a010301
setSrpConstantArea(double)7100%n/a010301
setSrpCoefficient(double)7100%n/a010301
setSrpUncertainty(double)7100%n/a010301
setAttitudeKnowledgeAccuracy(double)7100%n/a010301
setAttitudeControlAccuracy(double)7100%n/a010301
setAttitudePointingAccuracy(double)7100%n/a010301
setManeuversFrequency(double)7100%n/a010301
setMaxThrust(double)7100%n/a010301
setBolDv(double)7100%n/a010301
setRemainingDv(double)7100%n/a010301
setManufacturer(String)6100%n/a010301
setBusModel(String)6100%n/a010301
setDockedWith(List)6100%n/a010301
setAttitudeControlMode(String)6100%n/a010301
setAttitudeActuatorType(String)6100%n/a010301
getManufacturer()4100%n/a010101
getBusModel()4100%n/a010101
getDragConstantArea()4100%n/a010101
getDragCoefficient()4100%n/a010101
getDragUncertainty()4100%n/a010101
getInitialWetMass()4100%n/a010101
getWetMass()4100%n/a010101
getDryMass()4100%n/a010101
getMinAreaForCollisionProbability()4100%n/a010101
getMaxAreaForCollisionProbability()4100%n/a010101
getTypAreaForCollisionProbability()4100%n/a010101
getSrpConstantArea()4100%n/a010101
getSrpCoefficient()4100%n/a010101
getSrpUncertainty()4100%n/a010101
getAttitudeControlMode()4100%n/a010101
getAttitudeActuatorType()4100%n/a010101
getAttitudeKnowledgeAccuracy()4100%n/a010101
getAttitudeControlAccuracy()4100%n/a010101
getAttitudePointingAccuracy()4100%n/a010101
getManeuversFrequency()4100%n/a010101
getMaxThrust()4100%n/a010101
getBolDv()4100%n/a010101
getRemainingDv()4100%n/a010101
getInertiaMatrix()4100%n/a010101
getDockedWith()3100%n/a010101