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 |