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 |