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 |
getPosition(Frame) |   | 69% |   | 50% | 1 | 2 | 0 | 1 | 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 | 6 | 0 | 31 | 0 | 1 |
toSpacecraftState() |  | 100% |  | 100% | 0 | 8 | 0 | 23 | 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 |
toTransform() |  | 100% | | n/a | 0 | 1 | 0 | 4 | 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 | 4 | 0 | 1 |
getAdditionalState(String) |  | 100% |  | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
getAdditionalStateDerivative(String) |  | 100% |  | 100% | 0 | 2 | 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, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, FieldAttitude) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldOrbit, CalculusFieldElement, FieldArrayDictionary) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, FieldAttitude) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldSpacecraftState(FieldAbsolutePVCoordinates, CalculusFieldElement, FieldArrayDictionary) |  | 100% | | n/a | 0 | 1 | 0 | 3 | 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 |
getDate() |  | 100% |  | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getFrame() |  | 100% |  | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getPosition() |  | 100% |  | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getPVCoordinates() |  | 100% |  | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
toStaticTransform() |  | 100% | | n/a | 0 | 1 | 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 |
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 |