NumericalTimeDerivativesEquations

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total12 of 25095%1 of 1492%11514508
addMassDerivative(double)121352%1150%121401
addKeplerContribution(double)69100%4100%0301101
computeTimeDerivatives(SpacecraftState)62100%4100%0301101
NumericalTimeDerivativesEquations(OrbitType, PositionAngleType, List)43100%2100%0201001
addNonKeplerianAcceleration(Vector3D)40100%2100%020401
setCoordinatesJacobian(double[][])4100%n/a010201
setCurrentState(SpacecraftState)4100%n/a010201
getForceModels()3100%n/a010101