STMEquations

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total11 of 42797%0 of 14100%11525318
computeDerivatives(SpacecraftState, double[])110%n/a112211
derivatives(SpacecraftState)276100%6100%0402401
STMEquations(CR3BPSystem)64100%2100%0201201
getStateTransitionMatrix(SpacecraftState)41100%4100%030601
setInitialPhi(SpacecraftState)25100%2100%020501
init(SpacecraftState, AbsoluteDate)5100%n/a010201
getName()3100%n/a010101
getDimension()100%n/a010101