StateTransitionMatrixGenerator

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total2 of 77799%1 of 4097%132198012
setInitialStateTransitionMatrix(SpacecraftState, RealMatrix, OrbitType, PositionAngleType)10398%11191%1712001
computePartials(SpacecraftState)356100%20100%01105101
multiplyMatrix(double[], double[], double[], int)234100%2100%020701
combinedDerivatives(SpacecraftState)24100%n/a010501
StateTransitionMatrixGenerator(String, List, AttitudeProvider)17100%n/a010601
wrapAttitudeProviderIfPossible(List, AttitudeProvider)10100%2100%020301
yields(SpacecraftState)9100%2100%020101
addObserver(String, StateTransitionMatrixGenerator.PartialsObserver)7100%n/a010201
lambda$computePartials$0(ForceModel)7100%2100%020101
getName()3100%n/a010101
static {...}3100%n/a010101
getDimension()100%n/a010101