DragForce

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 118100%0 of 4100%0802506
acceleration(FieldSpacecraftState, CalculusFieldElement[])61100%4100%0301101
acceleration(SpacecraftState, double[])37100%n/a010701
DragForce(Atmosphere, DragSensitive)10100%n/a010401
getParametersDrivers()4100%n/a010101
getAtmosphere()3100%n/a010101
getSpacecraft()3100%n/a010101