getControl3DVectorCostType() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
getFieldEventDetectors(Field) | | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
getEventDetectors() | | 100% | | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
shortestSegmentDuration() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
getThrustVector(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
getThrustVector(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
ProfileThrustPropulsionModel(TimeSpanMap, double, Control3DVectorCostType, String) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
getFlowRate(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFlowRate(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getThrustVector(SpacecraftState, double[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFlowRate(SpacecraftState, double[]) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getName() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
lambda$getFieldEventDetectors$1(FieldSpacecraftState, FieldEventDetector, boolean) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
lambda$getEventDetectors$0(SpacecraftState, EventDetector, boolean) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |