CircularOrbit(TimeStampedPVCoordinates, Frame, double) | | 97% | | 75% | 1 | 3 | 2 | 63 | 0 | 1 |
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) | | 93% | | 83% | 2 | 9 | 2 | 41 | 0 | 1 |
addKeplerContribution(PositionAngle, double, double[]) | | 95% | | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
computeJacobianMeanWrtCartesian() | | 100% | | n/a | 0 | 1 | 0 | 80 | 0 | 1 |
interpolate(AbsoluteDate, Stream) | | 100% | | 100% | 0 | 7 | 0 | 42 | 0 | 1 |
computePVWithoutA() | | 100% | | 100% | 0 | 2 | 0 | 35 | 0 | 1 |
CircularOrbit(Orbit) | | 100% | | 100% | 0 | 4 | 0 | 37 | 0 | 1 |
nonKeplerianAcceleration() | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
computeJacobianTrueWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 24 | 0 | 1 |
shiftedBy(double) | | 100% | | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
meanToEccentric(double, double, double) | | 100% | | 75% | 1 | 3 | 0 | 15 | 0 | 1 |
computeJacobianEccentricWrtCartesian() | | 100% | | 100% | 0 | 2 | 0 | 12 | 0 | 1 |
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, TimeStampedPVCoordinates, Frame, double) | | 100% | | n/a | 0 | 1 | 0 | 16 | 0 | 1 |
initPVCoordinates() | | 100% | | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
toString() | | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
eccentricToTrue(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
trueToEccentric(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getHxDot() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getHyDot() | | 100% | | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getAlphaMDot() | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
getAlphaEDot() | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
getEquinoctialExDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEquinoctialEyDot() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getHx() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
getHy() | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
CircularOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getAlpha(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
getAlphaDot(PositionAngle) | | 100% | | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
eccentricToMean(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAlphaM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
CircularOrbit(PVCoordinates, Frame, AbsoluteDate, double) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getAlphaE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLv() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLvDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLEDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLM() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLMDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
writeReplace() | | 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 |
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 |
getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |