getState(ParameterDriversProvider) | | 100% | | 100% | 0 | 7 | 0 | 42 | 0 | 1 |
buildBasicGradientSpacecraftState(SpacecraftState, int, AttitudeProvider) | | 100% | | 100% | 0 | 6 | 0 | 32 | 0 | 1 |
getParametersAtStateDate(FieldSpacecraftState, ParameterDriversProvider) | | 100% | | 100% | 0 | 6 | 0 | 14 | 0 | 1 |
getParameters(FieldSpacecraftState, ParameterDriversProvider) | | 100% | | 100% | 0 | 5 | 0 | 16 | 0 | 1 |
extend(FieldRotation, int) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
extend(FieldVector3D, int) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
extend(Gradient, int) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
extend(FieldAbsoluteDate, int) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
AbstractGradientConverter(int) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
initStates(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getFreeStateParameters() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |