addKeplerContribution(CalculusFieldElement) | | 23% | | 75% | 1 | 3 | 7 | 11 | 0 | 1 |
addMassDerivative(CalculusFieldElement) | | 60% | | 50% | 1 | 2 | 1 | 4 | 0 | 1 |
computeDerivatives(FieldSpacecraftState) | | 100% | | 100% | 0 | 4 | 0 | 14 | 0 | 1 |
FieldNumericalPropagator.Main(FieldNumericalPropagator, FieldODEIntegrator) | | 100% | | 100% | 0 | 4 | 0 | 11 | 0 | 1 |
addNonKeplerianAcceleration(FieldVector3D) | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
init(FieldSpacecraftState, FieldAbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
lambda$new$0(FieldODEIntegrator, FieldEventDetector) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
lambda$init$1(FieldSpacecraftState, FieldAbsoluteDate, ForceModel) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |