addForceModel(ForceModel) | | 81% | | 83% | 1 | 4 | 3 | 12 | 0 | 1 |
resetInitialState(FieldSpacecraftState) | | 73% | | 50% | 1 | 2 | 1 | 5 | 0 | 1 |
removeForceModels() | | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
getOrbitType() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
getNewtonianAttractionForceModel() | | 90% | | 50% | 2 | 3 | 1 | 4 | 0 | 1 |
getForceModels() | | 87% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
tolerances(RealFieldElement, FieldOrbit, OrbitType) | | 100% | | 100% | 0 | 4 | 0 | 30 | 0 | 1 |
FieldNumericalPropagator(Field, FieldODEIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 9 | 0 | 1 |
hasNewtonianAttraction() | | 100% | | 75% | 1 | 3 | 0 | 2 | 0 | 1 |
createMapper(FieldAbsoluteDate, double, OrbitType, PositionAngle, AttitudeProvider, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setMu(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getPVCoordinates(FieldAbsoluteDate, Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMainStateEquations(FieldODEIntegrator) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
superSetMu(double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getAllForceModels() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
setOrbitType(OrbitType) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setPositionAngleType(PositionAngle) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
setInitialState(FieldSpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |