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 |