toString() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
getEquinoctialEx() | | 47% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
getEquinoctialEy() | | 47% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
getE() | | 47% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
getAbsPVA() | | 46% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
getOrbit() | | 46% | | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
getPVCoordinates(Frame) | | 69% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
ensureCompatibleAdditionalStates(FieldSpacecraftState) | | 98% | | 83% | 4 | 13 | 2 | 31 | 0 | 1 |
FieldSpacecraftState(Field, SpacecraftState) | | 100% | | 100% | 0 | 10 | 0 | 49 | 0 | 1 |
interpolate(FieldAbsoluteDate, Stream) | | 100% | | 100% | 0 | 10 | 0 | 42 | 0 | 1 |
toSpacecraftState() | | 100% | | 100% | 0 | 8 | 0 | 23 | 0 | 1 |
lambda$interpolate$0(FieldAbsoluteDate, List, List, List, FieldHermiteInterpolator, Map, Map, FieldSpacecraftState) | | 100% | | 100% | 0 | 4 | 0 | 15 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldAttitude, CalculusFieldElement, FieldArrayDictionary, FieldArrayDictionary) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
checkConsistency(FieldOrbit, FieldAttitude) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement, FieldArrayDictionary, FieldArrayDictionary) | | 100% | | 100% | 0 | 3 | 0 | 13 | 0 | 1 |
checkConsistency(FieldAbsolutePVCoordinates, FieldAttitude) | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
shiftedBy(double) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
addAdditionalState(String, CalculusFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
addAdditionalStateDerivative(String, CalculusFieldElement[]) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
shiftedBy(CalculusFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
shiftAdditional(double) | | 100% | | 100% | 0 | 4 | 0 | 9 | 0 | 1 |
shiftAdditional(CalculusFieldElement) | | 100% | | 100% | 0 | 4 | 0 | 9 | 0 | 1 |
FieldSpacecraftState(FieldOrbit) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
toTransform() | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getAdditionalState(String) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
getAdditionalStateDerivative(String) | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, CalculusFieldElement, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, CalculusFieldElement, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getMu() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getKeplerianPeriod() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getKeplerianMeanMotion() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getA() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getHx() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getHy() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getLv() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getLE() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getLM() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getI() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldAttitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldAttitude, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldAttitude, CalculusFieldElement, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldAttitude, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, CalculusFieldElement, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, CalculusFieldElement, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, Map) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getDate() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getFrame() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
hasAdditionalState(String) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
hasAdditionalStateDerivative(String) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldAttitude, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldAttitude, CalculusFieldElement, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude, CalculusFieldElement, FieldArrayDictionary) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
isOrbitDefined() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getAdditionalStates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAdditionalStatesValues() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAdditionalStatesDerivatives() | | 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 |