OrbitPhysicalProperties

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 300100%0 of 0n/a0520122052
OrbitPhysicalProperties(AbsoluteDate)61100%n/a0102001
setInertiaMatrixEntry(int, int, double)15100%n/a010401
setManufacturer(String)6100%n/a010301
setBusModel(String)6100%n/a010301
setDockedWith(List)6100%n/a010301
setDragConstantArea(double)6100%n/a010301
setDragCoefficient(double)6100%n/a010301
setDragUncertainty(double)6100%n/a010301
setInitialWetMass(double)6100%n/a010301
setWetMass(double)6100%n/a010301
setDryMass(double)6100%n/a010301
setMinAreaForCollisionProbability(double)6100%n/a010301
setMaxAreaForCollisionProbability(double)6100%n/a010301
setTypAreaForCollisionProbability(double)6100%n/a010301
setSrpConstantArea(double)6100%n/a010301
setSrpCoefficient(double)6100%n/a010301
setSrpUncertainty(double)6100%n/a010301
setAttitudeControlMode(String)6100%n/a010301
setAttitudeActuatorType(String)6100%n/a010301
setAttitudeKnowledgeAccuracy(double)6100%n/a010301
setAttitudeControlAccuracy(double)6100%n/a010301
setAttitudePointingAccuracy(double)6100%n/a010301
setManeuversFrequency(double)6100%n/a010301
setMaxThrust(double)6100%n/a010301
setBolDv(double)6100%n/a010301
setRemainingDv(double)6100%n/a010301
getManeuversPerYear()5100%n/a010101
getManufacturer()3100%n/a010101
getBusModel()3100%n/a010101
getDockedWith()3100%n/a010101
getDragConstantArea()3100%n/a010101
getDragCoefficient()3100%n/a010101
getDragUncertainty()3100%n/a010101
getInitialWetMass()3100%n/a010101
getWetMass()3100%n/a010101
getDryMass()3100%n/a010101
getMinAreaForCollisionProbability()3100%n/a010101
getMaxAreaForCollisionProbability()3100%n/a010101
getTypAreaForCollisionProbability()3100%n/a010101
getSrpConstantArea()3100%n/a010101
getSrpCoefficient()3100%n/a010101
getSrpUncertainty()3100%n/a010101
getAttitudeControlMode()3100%n/a010101
getAttitudeActuatorType()3100%n/a010101
getAttitudeKnowledgeAccuracy()3100%n/a010101
getAttitudeControlAccuracy()3100%n/a010101
getAttitudePointingAccuracy()3100%n/a010101
getManeuversFrequency()3100%n/a010101
getMaxThrust()3100%n/a010101
getBolDv()3100%n/a010101
getRemainingDv()3100%n/a010101
getInertiaMatrix()3100%n/a010101