setParameters(double[]) | | 65% | | 75% | 3 | 9 | 5 | 18 | 0 | 1 |
AbstractPropagatorBuilder(Orbit, PositionAngleType, double, boolean, AttitudeProvider) | | 100% | | 100% | 0 | 3 | 0 | 19 | 0 | 1 |
getSelectedNormalizedParameters() | | 100% | | 100% | 0 | 7 | 0 | 13 | 0 | 1 |
getNbValuesForSelected() | | 100% | | 100% | 0 | 5 | 0 | 10 | 0 | 1 |
resetOrbit(Orbit) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
createInitialOrbit() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
deselectDynamicParameters() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
AbstractPropagatorBuilder(Orbit, PositionAngleType, double, boolean) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
addSupportedParameters(List) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
addAdditionalDerivativesProvider(AdditionalDerivativesProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setAttitudeProvider(AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getOrbitType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getInitialOrbitDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOrbitalParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPropagationParametersDrivers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAttitudeProvider() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPositionScale() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAdditionalDerivativesProviders() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |