FieldCircularOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement) |   | 97% |   | 75% | 1 | 3 | 2 | 64 | 0 | 1 |
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement) |   | 93% |   | 83% | 2 | 9 | 2 | 40 | 0 | 1 |
addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[]) |  | 96% |   | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
computeJacobianMeanWrtCartesian() |  | 100% | | n/a | 0 | 1 | 0 | 111 | 0 | 1 |
computePVWithoutA() |  | 100% |  | 100% | 0 | 2 | 0 | 39 | 0 | 1 |
FieldCircularOrbit(FieldOrbit) |  | 100% |  | 100% | 0 | 4 | 0 | 38 | 0 | 1 |
initPosition() |  | 100% | | n/a | 0 | 1 | 0 | 28 | 0 | 1 |
nonKeplerianAcceleration() |  | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
computeJacobianTrueWrtCartesian() |  | 100% |  | 100% | 0 | 2 | 0 | 24 | 0 | 1 |
FieldCircularOrbit(Field, CircularOrbit) |  | 100% |  | 100% | 0 | 2 | 0 | 22 | 0 | 1 |
shiftedBy(CalculusFieldElement) |  | 100% |  | 100% | 0 | 2 | 0 | 18 | 0 | 1 |
meanToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) |  | 100% |   | 75% | 1 | 3 | 0 | 15 | 0 | 1 |
toOrbit() |  | 100% |  | 100% | 0 | 2 | 0 | 11 | 0 | 1 |
computeJacobianEccentricWrtCartesian() |  | 100% |  | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
getHxDot() |  | 100% |  | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
getHyDot() |  | 100% |  | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
eccentricToTrue(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
trueToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
toString() |  | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
initPVCoordinates() |  | 100% |  | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
getAlphaMDot() |  | 100% |  | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
getEquinoctialExDot() |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getEquinoctialEyDot() |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getAlphaEDot() |  | 100% |  | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
getHx() |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getHy() |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
removeRates() |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getEDot() |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getEquinoctialEx() |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEquinoctialEy() |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
eccentricToMean(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getE() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAlpha(PositionAngleType) |  | 100% |  | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
getAlphaDot(PositionAngleType) |  | 100% |  | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
getAlphaM() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLvDot() |  | 100% |  | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getLEDot() |  | 100% |  | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getLMDot() |  | 100% |  | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
FieldCircularOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldCircularOrbit(Field, Orbit) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getAlphaE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
shiftedBy(double) | | 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 |
hasDerivatives() | | 100% |  | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getADot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getCircularEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getCircularExDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getCircularEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getCircularEyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAlphaV() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAlphaVDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getIDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRightAscensionOfAscendingNode() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRightAscensionOfAscendingNodeDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
hasRates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getCachedPositionAngleType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |