| create(FieldAdaptableInterval, CalculusFieldElement, int, FieldEventHandler) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| FieldImpulseManeuver(FieldEventDetectionSettings, FieldEventHandler, FieldEventDetector, AttitudeProvider, FieldVector3D, CalculusFieldElement, Control3DVectorCostType) |  | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| init(FieldSpacecraftState, FieldAbsoluteDate) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| FieldImpulseManeuver(FieldEventDetector, AttitudeProvider, FieldVector3D, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldImpulseManeuver(FieldEventDetector, AttitudeProvider, FieldVector3D, CalculusFieldElement, Control3DVectorCostType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| FieldImpulseManeuver(FieldEventDetector, FieldVector3D, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| g(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAttitudeOverride() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getTrigger() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDeltaVSat() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getIsp() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getControl3DVectorCostType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |