LambertDifferentialCorrector

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total0 of 402100%1 of 1693%1360100028
iterate(AbstractPropagator)87100%6100%0402001
buildInitialState(AbstractPropagator, SpacecraftState, Vector3D)84100%2100%0201901
getCartesianStm(SpacecraftState, SpacecraftState)41100%1375%130901
init(AbstractPropagator, Vector3D)27100%2100%020501
computeNewtonCorrection(Vector3D, RealMatrix)25100%n/a010401
LambertDifferentialCorrector(LambertBoundaryConditions)24100%n/a010901
computeJacobianWrtCartesian(Orbit)12100%n/a010301
computeJacobianWrtOrbitalParameters(Orbit)12100%n/a010301
hasConverged(Vector3D)10100%2100%020101
extractVelocity(SpacecraftState)9100%n/a010201
getDecompositionSolver(RealMatrix)8100%n/a010101
solve(AbstractPropagator, Vector3D)8100%n/a010201
setInitialMass(double)4100%n/a010201
setPositionTolerance(double)4100%n/a010201
setThresholdMatrixSolver(double)4100%n/a010201
setStmName(String)4100%n/a010201
setMaxIter(int)4100%n/a010201
setCurrentIter(int)4100%n/a010201
create6x6Array()4100%n/a010101
getLambertBoundaryConditions()3100%n/a010101
getInitialMass()3100%n/a010101
getPositionTolerance()3100%n/a010101
getThresholdMatrixSolver()3100%n/a010101
getStmName()3100%n/a010101
getMaxIter()3100%n/a010101
getCurrentIter()3100%n/a010101
getMatricesHarvester()3100%n/a010101
createRealMatrix(double[][])3100%n/a010101