AbstractStateTransitionMatrixGenerator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 440100%0 of 38100%037087018
setInitialStateTransitionMatrix(SpacecraftState, RealMatrix, OrbitType, PositionAngleType)94100%8100%0501901
computePartials(SpacecraftState)86100%6100%0401501
updateFactorForParameters(ForceModel, NumericalGradientConverter, Gradient[], DoubleArrayDictionary, SpacecraftState, double[])69100%10100%0601201
updateDictionaryEntry(DoubleArrayDictionary, TimeSpanMap.Span, Gradient[], int)47100%4100%030901
flatten(RealMatrix)32100%4100%030601
combinedDerivatives(SpacecraftState)26100%n/a010501
AbstractStateTransitionMatrixGenerator(String, List, AttitudeProvider, int)25100%n/a010801
wrapAttitudeProviderIfPossible()13100%2100%020301
yields(SpacecraftState)9100%2100%020101
addObserver(String, AbstractStateTransitionMatrixGenerator.PartialsObserver)7100%n/a010201
getDecompositionSolver(RealMatrix)7100%n/a010101
lambda$computePartials$0(ForceModel)7100%2100%020101
getName()3100%n/a010101
getDimension()3100%n/a010101
getStateDimension()3100%n/a010101
getForceModels()3100%n/a010101
getPartialsObservers()3100%n/a010101
static {...}3100%n/a010101