getThrustVector(AbsoluteDate) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
getFlowRate(AbsoluteDate) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
BasicConstantThrustPropulsionModel(double, double, Vector3D, Control3DVectorCostType, String) |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
getParametersDrivers() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getThrustVector(CalculusFieldElement[]) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
static {...} |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
BasicConstantThrustPropulsionModel(double, double, Vector3D, String) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getThrustVector() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getThrustVector(double[]) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFlowRate() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFlowRate(double[]) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFlowRate(CalculusFieldElement[]) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |