DragForce

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 47100%0 of 0n/a0801208
DragForce(Atmosphere, DragSensitive, boolean, Atmosphere)9100%n/a010301
DragForce(Atmosphere, DragSensitive, boolean)7100%n/a010201
acceleration(SpacecraftState, double[])7100%n/a010101
acceleration(FieldSpacecraftState, CalculusFieldElement[])7100%n/a010101
DragForce(Atmosphere, DragSensitive)6100%n/a010201
dependsOnAttitudeRate()4100%n/a010101
getParametersDrivers()4100%n/a010101
getSpacecraft()3100%n/a010101