meanToHyperbolicEccentric(CalculusFieldElement, CalculusFieldElement) | | 92% | | 87% | 2 | 9 | 2 | 24 | 0 | 1 |
FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngle, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 96% | | 90% | 2 | 14 | 2 | 54 | 0 | 1 |
addKeplerContribution(PositionAngle, CalculusFieldElement, CalculusFieldElement[]) | | 95% | | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
computeJacobianMeanWrtCartesianElliptical() | | 100% | | n/a | 0 | 1 | 0 | 86 | 0 | 1 |
computeJacobianMeanWrtCartesianHyperbolic() | | 100% | | n/a | 0 | 1 | 0 | 89 | 0 | 1 |
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement, boolean) | | 100% | | 100% | 0 | 4 | 0 | 62 | 0 | 1 |
computePVWithoutA() | | 100% | | 100% | 0 | 3 | 0 | 42 | 0 | 1 |
interpolate(FieldAbsoluteDate, Stream) | | 100% | | 100% | 0 | 7 | 0 | 47 | 0 | 1 |
meanToEllipticEccentric(CalculusFieldElement, CalculusFieldElement) | | 100% | | 100% | 0 | 7 | 0 | 30 | 0 | 1 |
nonKeplerianAcceleration() | | 100% | | n/a | 0 | 1 | 0 | 22 | 0 | 1 |
shiftedBy(CalculusFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 16 | 0 | 1 |
computeJacobianTrueWrtCartesianElliptical() | | 100% | | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
computeJacobianTrueWrtCartesianHyperbolic() | | 100% | | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
toOrbit() | | 100% | | 100% | 0 | 2 | 0 | 9 | 0 | 1 |
eMeSinE(CalculusFieldElement, CalculusFieldElement) | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
computeJacobianEccentricWrtCartesianHyperbolic() | | 100% | | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
computeJacobianEccentricWrtCartesianElliptical() | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
toString() | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
getHxDot() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
getHyDot() | | 100% | | 100% | 0 | 3 | 0 | 7 | 0 | 1 |
initPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
ellipticEccentricToTrue(CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getMeanAnomalyDot() | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
trueToEllipticEccentric(CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getEccentricAnomalyDot() | | 100% | | 100% | 0 | 3 | 0 | 8 | 0 | 1 |
getEquinoctialExDot() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
getEquinoctialEyDot() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
checkParameterRangeInclusive(String, double, double, double) | | 100% | | 75% | 1 | 3 | 0 | 4 | 0 | 1 |
trueToHyperbolicEccentric(CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getHx() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getHy() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
hyperbolicEccentricToTrue(CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getMeanAnomaly() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngle, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEccentricAnomaly() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getLvDot() | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
getLEDot() | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
getLMDot() | | 100% | | 100% | 0 | 2 | 0 | 2 | 0 | 1 |
getAnomaly(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
getAnomalyDot(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
computeJacobianMeanWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
computeJacobianEccentricWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
computeJacobianTrueWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
FieldKeplerianOrbit(FieldOrbit) | | 100% | | n/a | 0 | 1 | 0 | 2 | 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 |
shiftedBy(double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
static {...} | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
FieldKeplerianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
hyperbolicEccentricToMean(CalculusFieldElement, CalculusFieldElement) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
ellipticEccentricToMean(CalculusFieldElement, CalculusFieldElement) | | 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 |
getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEDot() | | 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 |
getPerigeeArgument() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPerigeeArgumentDot() | | 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 |
getTrueAnomaly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getTrueAnomalyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |