findByName(List, String) | | 90% | | 75% | 1 | 3 | 1 | 5 | 0 | 1 |
extractParameters(CalculusFieldElement[], FieldAbsoluteDate) | | 100% | | 100% | 0 | 4 | 0 | 11 | 0 | 1 |
acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | 100% | 0 | 3 | 0 | 9 | 0 | 1 |
extractParameters(double[], AbsoluteDate) | | 100% | | 100% | 0 | 4 | 0 | 11 | 0 | 1 |
acceleration(SpacecraftState, double[]) | | 100% | | 100% | 0 | 3 | 0 | 9 | 0 | 1 |
getParametersDrivers() | | 100% | | 83% | 1 | 4 | 0 | 7 | 0 | 1 |
TimeSpanParametricAcceleration(Vector3D, boolean, AttitudeProvider, AccelerationModel) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
addAccelerationModelValidBefore(AccelerationModel, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
addAccelerationModelValidAfter(AccelerationModel, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
TimeSpanParametricAcceleration(Vector3D, boolean, AccelerationModel) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
TimeSpanParametricAcceleration(Vector3D, AttitudeProvider, AccelerationModel) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
init(SpacecraftState, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getAccelerationModel(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
extractAccelerationModelRange(AbsoluteDate, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAccelerationModelSpan(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
lambda$init$0(SpacecraftState, AbsoluteDate, AccelerationModel) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFirstSpan() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
dependsOnPositionOnly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEventDetectors() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFieldEventDetectors(Field) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |