| acceleration(FieldSpacecraftState, CalculusFieldElement[]) |  | 100% |  | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
| acceleration(SpacecraftState, double[]) |  | 100% |  | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
| addContribution(FieldSpacecraftState, FieldTimeDerivativesEquations) |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| getParametersDrivers() |  | 100% |  | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
| addContribution(SpacecraftState, TimeDerivativesEquations) |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
| getMassDerivative(FieldSpacecraftState, CalculusFieldElement[]) |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getAttitudeModelParameters(CalculusFieldElement[]) |  | 100% |  | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getMassDerivative(SpacecraftState, double[]) |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
| getAttitudeModelParameters(double[]) |  | 100% |  | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
| getManeuverTriggersParameters(CalculusFieldElement[]) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getManeuverTriggersParameters(double[]) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getName() |  | 100% |  | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| Maneuver(AttitudeRotationModel, ManeuverTriggers, PropulsionModel) |  | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| init(SpacecraftState, AbsoluteDate) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| init(FieldSpacecraftState, FieldAbsoluteDate) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getFieldEventDetectors(Field) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getPropulsionModelParameters(CalculusFieldElement[]) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEventDetectors() |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getPropulsionModelParameters(double[]) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getControl3DVectorCostType() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAttitudeOverride() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getPropulsionModel() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getManeuverTriggers() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| dependsOnPositionOnly() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |