addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[]) | | 96% | | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
initializeCachedAlpha(CalculusFieldElement, CalculusFieldElement, PositionAngleType) | | 94% | | 91% | 1 | 8 | 1 | 16 | 0 | 1 |
getAlphaVDot() | | 94% | | 83% | 1 | 5 | 1 | 15 | 0 | 1 |
getAlphaEDot() | | 94% | | 83% | 1 | 5 | 1 | 15 | 0 | 1 |
getAlphaMDot() | | 94% | | 83% | 1 | 5 | 1 | 15 | 0 | 1 |
initializeCachedAlpha(CalculusFieldElement, PositionAngleType) | | 92% | | 91% | 1 | 8 | 1 | 13 | 0 | 1 |
getAlphaV() | | 83% | | 75% | 1 | 4 | 1 | 5 | 0 | 1 |
getAlphaE() | | 83% | | 75% | 1 | 4 | 1 | 5 | 0 | 1 |
getAlphaM() | | 83% | | 75% | 1 | 4 | 1 | 5 | 0 | 1 |
computeJacobianMeanWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 111 | 0 | 1 |
FieldCircularOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement) | | 100% | | 100% | 0 | 3 | 0 | 65 | 0 | 1 |
computePVWithoutA() | | 100% | | 100% | 0 | 2 | 0 | 39 | 0 | 1 |
FieldCircularOrbit(FieldOrbit) | | 100% | | 100% | 0 | 4 | 0 | 39 | 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 | 23 | 0 | 1 |
shiftedBy(CalculusFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 18 | 0 | 1 |
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | 100% | 0 | 3 | 0 | 24 | 0 | 1 |
computeJacobianEccentricWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
toOrbit() | | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
getHxDot() | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
getHyDot() | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
initPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
toString() | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
getEquinoctialExDot() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getEquinoctialEyDot() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getHx() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getHy() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getEDot() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
removeRates() | | 100% | | n/a | 0 | 1 | 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, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, 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 |
FieldCircularOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 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 |
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 |
eccentricToTrue(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
trueToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
meanToEccentric(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
eccentricToMean(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 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 |
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 |
getCachedPositionAngleType() | | 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 |