DragForce

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total2 of 41999%8 of 3073%825073010
isStateDerivative(FieldSpacecraftState)8198%71365%71101401
isVariable(DerivativeStructure, int)3397%1583%140501
getDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D)182100%2100%0202801
acceleration(FieldSpacecraftState, RealFieldElement[])57100%2100%0201001
acceleration(SpacecraftState, double[])45100%n/a010801
DragForce(Atmosphere, DragSensitive)9100%n/a010401
getParametersDrivers()4100%n/a010101
dependsOnPositionOnly()2100%n/a010101
getEventsDetectors()2100%n/a010101
getFieldEventsDetectors(Field)2100%n/a010101