BasicConstantThrustPropulsionModel

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total13 of 13090%0 of 0n/a212219212
getThrustVector(AbsoluteDate)80%n/a111111
getFlowRate(AbsoluteDate)50%n/a111111
BasicConstantThrustPropulsionModel(double, double, Vector3D, Control3DVectorCostType, String)50100%n/a010601
getParametersDrivers()15100%n/a010101
getThrustVector(CalculusFieldElement[])9100%n/a010101
static {...}9100%n/a010201
BasicConstantThrustPropulsionModel(double, double, Vector3D, String)8100%n/a010201
getThrustVector()7100%n/a010101
getThrustVector(double[])7100%n/a010101
getFlowRate()4100%n/a010101
getFlowRate(double[])4100%n/a010101
getFlowRate(CalculusFieldElement[])4100%n/a010101