ThrustPropulsionModel

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total25 of 8470%0 of 0n/a3751737
getIsp(SpacecraftState)150%n/a113311
getDirection(SpacecraftState)50%n/a111111
getThrust(SpacecraftState)50%n/a111111
getAcceleration(FieldSpacecraftState, FieldAttitude, CalculusFieldElement[])26100%n/a010501
getAcceleration(SpacecraftState, Attitude, double[])23100%n/a010501
getMassDerivatives(SpacecraftState, double[])5100%n/a010101
getMassDerivatives(FieldSpacecraftState, CalculusFieldElement[])5100%n/a010101