| findSwitchEventAndUpdateState(AbsoluteDate, Gradient[], AbsoluteDate, ControlSwitchDetector, AdjointDynamicsProvider) |   | 95% | | 50% | 3 | 4 | 2 | 17 | 0 | 1 |
| iterate(ShootingBoundaryOutput) | | 96% | | 83% | 1 | 4 | 1 | 19 | 0 | 1 |
| propagateField(FieldSpacecraftState) | | 100% | | 90% | 1 | 6 | 0 | 24 | 0 | 1 |
| createFieldState(FieldAbsoluteDate, CalculusFieldElement[], CalculusFieldElement, CalculusFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 18 | 0 | 1 |
| invertTaylorMap(Gradient[], Gradient) | | 100% | | 100% | 0 | 3 | 0 | 18 | 0 | 1 |
| updateStateWithTaylorMapInversion(AbsoluteDate, Gradient[], AbsoluteDate, FieldControlSwitchDetector, String) | | 100% | | 100% | 0 | 2 | 0 | 14 | 0 | 1 |
| createFieldInitialStateWithMassAndAdjoint(double, double[]) | | 100% | | 100% | 0 | 2 | 0 | 9 | 0 | 1 |
| formatToArray(FieldSpacecraftState, AdjointDynamicsProvider) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
| formatFromArray(AbsoluteDate, Gradient[]) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| buildPropagator(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| solve(double, double[], double[]) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| buildFieldODE(FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| AbstractFixedInitialCartesianSingleShooting(ShootingPropagationSettings, SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| createStateWithMassAndAdjoint(double, double[]) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getUnitScales() | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| solve(double, double[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$buildPropagator$0(NumericalPropagator, EventDetector) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| createInitialStateWithMass(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getScales() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |