| iterate(double, double[]) |   | 94% | | 75% | 2 | 5 | 1 | 22 | 0 | 1 |
| createFieldStateWithMassAndAdjoint(double, double[]) | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
| checkConvergence(SpacecraftState) | | 100% | | 100% | 0 | 4 | 0 | 9 | 0 | 1 |
| buildInitialStateTemplate(Orbit) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| AbstractFixedBoundaryCartesianSingleShooting(ShootingPropagationSettings, FixedTimeCartesianBoundaryStates, CartesianBoundaryConditionChecker) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| AbstractFixedBoundaryCartesianSingleShooting(ShootingPropagationSettings, FixedTimeBoundaryOrbits, CartesianBoundaryConditionChecker) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| buildInitialStateTemplate(AbsolutePVCoordinates) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| buildFieldPropagator(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
| createStateWithMass(double) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| computeCandidateSolution(SpacecraftState, int) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| buildPropagator(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| solve(double, double[]) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| createStateWithMassAndAdjoint(double, double[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setToleranceMassAdjoint(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setScalePositionDefects(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| setScaleVelocityDefects(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getScalePositionDefects() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getScaleVelocityDefects() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getConditionChecker() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTerminalCartesianState() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |