AbstractConstantThrustPropulsionModel

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total30 of 12676%0 of 0n/a419527419
getIsp(AbsoluteDate)160%n/a112211
getDirection(AbsoluteDate)60%n/a111111
getThrustMagnitude(AbsoluteDate)50%n/a111111
getControl3DVectorCostType()30%n/a111111
AbstractConstantThrustPropulsionModel(double, double, Vector3D, Control3DVectorCostType, String)27100%n/a010601
getIsp()14100%n/a010201
AbstractConstantThrustPropulsionModel(double, double, Vector3D, String)8100%n/a010201
getDirection()5100%n/a010101
getThrustVector(SpacecraftState)5100%n/a010101
getFlowRate(SpacecraftState)5100%n/a010101
getThrustMagnitude()4100%n/a010101
getThrustVector(SpacecraftState, double[])4100%n/a010101
getFlowRate(SpacecraftState, double[])4100%n/a010101
getThrustVector(FieldSpacecraftState, CalculusFieldElement[])4100%n/a010101
getFlowRate(FieldSpacecraftState, CalculusFieldElement[])4100%n/a010101
getInitialThrustVector()3100%n/a010101
getInitialFlowRate()3100%n/a010101
getName()3100%n/a010101
static {...}3100%n/a010101