normalizeAngle(RealFieldElement, RealFieldElement) |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, RealFieldElement, double, RealFieldElement, double, double, double, double, double) |  | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
computeMeanParameters(FieldCircularOrbit, RealFieldElement) |   | 95% |   | 62% | 6 | 9 | 1 | 38 | 0 | 1 |
resetIntermediateState(FieldSpacecraftState, boolean) |   | 79% |   | 50% | 1 | 2 | 1 | 7 | 0 | 1 |
resetInitialState(FieldSpacecraftState) |  | 0% | | n/a | 1 | 1 | 2 | 2 | 1 | 1 |
toCartesian(FieldAbsoluteDate, FieldUnivariateDerivative2[]) |  | 100% | | n/a | 0 | 1 | 0 | 33 | 0 | 1 |
meanToEccentric(FieldUnivariateDerivative2, FieldUnivariateDerivative2, FieldUnivariateDerivative2) |  | 100% |   | 75% | 1 | 3 | 0 | 17 | 0 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, double, RealFieldElement, double, double, double, double, double, PropagationType) |  | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
resetInitialState(FieldSpacecraftState, PropagationType) |  | 100% |  | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics, PropagationType) |  | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, UnnormalizedSphericalHarmonicsProvider, UnnormalizedSphericalHarmonicsProvider.UnnormalizedSphericalHarmonics) |  | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, double, RealFieldElement, double, double, double, double, double) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, UnnormalizedSphericalHarmonicsProvider, PropagationType) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, UnnormalizedSphericalHarmonicsProvider) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
propagateOrbit(FieldAbsoluteDate) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, double, RealFieldElement, double, double, double, double, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, UnnormalizedSphericalHarmonicsProvider) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, RealFieldElement, UnnormalizedSphericalHarmonicsProvider) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, double, RealFieldElement, double, double, double, double, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, UnnormalizedSphericalHarmonicsProvider, PropagationType) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldEcksteinHechlerPropagator(FieldOrbit, AttitudeProvider, RealFieldElement, UnnormalizedSphericalHarmonicsProvider) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getMass(FieldAbsoluteDate) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |