DragForce

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 97100%0 of 0n/a0702307
acceleration(SpacecraftState, double[])37100%n/a010701
acceleration(FieldSpacecraftState, CalculusFieldElement[])34100%n/a010701
DragForce(Atmosphere, DragSensitive, boolean)8100%n/a010301
DragForce(Atmosphere, DragSensitive)7100%n/a010301
dependsOnAttitudeRate()4100%n/a010101
getParametersDrivers()4100%n/a010101
getSpacecraft()3100%n/a010101