DragForce

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total3 of 13897%0 of 4100%11012918
getSpacecraft()30%n/a111111
acceleration(FieldSpacecraftState, CalculusFieldElement[])69100%4100%0301201
acceleration(SpacecraftState, double[])45100%n/a010801
DragForce(Atmosphere, DragSensitive)10100%n/a010401
getParametersDrivers()4100%n/a010101
getAtmosphere()3100%n/a010101
getEventsDetectors()2100%n/a010101
getFieldEventsDetectors(Field)2100%n/a010101