ThrustPropulsionModel

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total16 of 10785%0 of 6100%1922316
getIsp(SpacecraftState)160%n/a112211
getAcceleration(FieldSpacecraftState, FieldAttitude, CalculusFieldElement[])32100%2100%020701
getAcceleration(SpacecraftState, Attitude, double[])30100%2100%020701
getDirection(SpacecraftState)19100%2100%020501
getMassDerivatives(SpacecraftState, double[])5100%n/a010101
getMassDerivatives(FieldSpacecraftState, CalculusFieldElement[])5100%n/a010101