interpolate(FieldAbsoluteDate, Stream) | | 0% | | 0% | 4 | 4 | 19 | 19 | 1 | 1 |
lambda$interpolate$0(FieldAbsoluteDate, List, List, FieldHermiteInterpolator, Map, FieldSpacecraftState) | | 0% | | 0% | 2 | 2 | 10 | 10 | 1 | 1 |
ensureCompatibleAdditionalStates(FieldSpacecraftState) | | 96% | | 66% | 4 | 7 | 3 | 15 | 0 | 1 |
FieldSpacecraftState(Field, SpacecraftState) | | 100% | | 100% | 0 | 8 | 0 | 28 | 0 | 1 |
toSpacecraftState() | | 100% | | 100% | 0 | 4 | 0 | 10 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldAttitude, RealFieldElement, Map) | | 100% | | 100% | 0 | 3 | 0 | 12 | 0 | 1 |
checkConsistency(FieldOrbit, FieldAttitude) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
addAdditionalState(String, RealFieldElement[]) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
FieldSpacecraftState(FieldOrbit) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, Map) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getAdditionalState(String) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
toTransform() | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, RealFieldElement, Map) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
shiftedBy(RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldAttitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldAttitude, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldAttitude, RealFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
hasAdditionalState(String) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPVCoordinates(Frame) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDate() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFrame() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAdditionalStates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMu() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getKeplerianPeriod() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getKeplerianMeanMotion() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPVCoordinates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOrbit() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAttitude() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMass() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |