DragForce

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total12 of 35497%1 of 475%1915607
accelerationDerivatives(AbsoluteDate, Frame, FieldVector3D, FieldVector3D, FieldRotation, DerivativeStructure)1221495%1375%1313001
accelerationDerivatives(SpacecraftState, String)48100%n/a010801
addContribution(SpacecraftState, TimeDerivativesEquations)47100%n/a010801
DragForce(Atmosphere, DragSensitive)15100%n/a010401
setParameter(String, double)8100%n/a010301
getParameter(String)7100%n/a010201
getEventsDetectors()3100%n/a010101