OrbitManeuver

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 200100%0 of 0n/a047075047
OrbitManeuver()19100%n/a010601
getAcceleration()6100%n/a010101
setAcceleration(int, double)6100%n/a010201
getDv()6100%n/a010101
setDv(int, double)6100%n/a010201
getThrust()6100%n/a010101
setThrust(int, double)6100%n/a010201
getDeployDv()6100%n/a010101
setDeployDv(int, double)6100%n/a010201
setDate(AbsoluteDate)4100%n/a010201
setDuration(double)4100%n/a010201
setDeltaMass(double)4100%n/a010201
setAccelerationInterpolation(OnOff)4100%n/a010201
setAccelerationMagnitudeSigma(double)4100%n/a010201
setAccelerationDirectionSigma(double)4100%n/a010201
setDvMagSigma(double)4100%n/a010201
setDvDirSigma(double)4100%n/a010201
setThrustEfficiency(double)4100%n/a010201
setThrustInterpolation(OnOff)4100%n/a010201
setThrustIsp(double)4100%n/a010201
setThrustMagnitudeSigma(double)4100%n/a010201
setThrustDirectionSigma(double)4100%n/a010201
setDeployId(String)4100%n/a010201
setDeployMass(double)4100%n/a010201
setDeployDvSigma(double)4100%n/a010201
setDeployDirSigma(double)4100%n/a010201
setDeployDvRatio(double)4100%n/a010201
setDeployDvCda(double)4100%n/a010201
getDate()3100%n/a010101
getDuration()3100%n/a010101
getDeltaMass()3100%n/a010101
getAccelerationInterpolation()3100%n/a010101
getAccelerationMagnitudeSigma()3100%n/a010101
getAccelerationDirectionSigma()3100%n/a010101
getDvMagSigma()3100%n/a010101
getDvDirSigma()3100%n/a010101
getThrustEfficiency()3100%n/a010101
getThrustInterpolation()3100%n/a010101
getThrustIsp()3100%n/a010101
getThrustMagnitudeSigma()3100%n/a010101
getThrustDirectionSigma()3100%n/a010101
getDeployId()3100%n/a010101
getDeployMass()3100%n/a010101
getDeployDvSigma()3100%n/a010101
getDeployDirSigma()3100%n/a010101
getDeployDvRatio()3100%n/a010101
getDeployDvCda()3100%n/a010101