initializeCachedAlpha(double, double, PositionAngleType) |  | 94% |   | 91% | 1 | 8 | 1 | 16 | 0 | 1 |
getAlphaVDot() |  | 93% |   | 75% | 1 | 4 | 1 | 13 | 0 | 1 |
getAlphaEDot() |  | 93% |   | 75% | 1 | 4 | 1 | 13 | 0 | 1 |
getAlphaMDot() |  | 93% |   | 75% | 1 | 4 | 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 | 80 | 0 | 1 |
CircularOrbit(TimeStampedPVCoordinates, Frame, double) |  | 100% |  | 100% | 0 | 3 | 0 | 64 | 0 | 1 |
computePVWithoutA() |  | 100% |  | 100% | 0 | 2 | 0 | 35 | 0 | 1 |
CircularOrbit(Orbit) |  | 100% |  | 100% | 0 | 4 | 0 | 38 | 0 | 1 |
nonKeplerianAcceleration() |  | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
initPosition() |  | 100% | | n/a | 0 | 1 | 0 | 26 | 0 | 1 |
computeJacobianTrueWrtCartesian() |  | 100% |  | 100% | 0 | 2 | 0 | 24 | 0 | 1 |
shiftedBy(double) |  | 100% |  | 100% | 0 | 2 | 0 | 14 | 0 | 1 |
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) |  | 100% |  | 100% | 0 | 3 | 0 | 25 | 0 | 1 |
computeKeplerianAlphaDot(PositionAngleType, double, double, double, double, double, PositionAngleType) |  | 100% |  | 100% | 0 | 3 | 0 | 11 | 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, PositionAngleType, Frame, double) |  | 100% | | n/a | 0 | 1 | 0 | 17 | 0 | 1 |
initPVCoordinates() |  | 100% |  | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
toString() |  | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
getHxDot() |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getHyDot() |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
getEquinoctialExDot() |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getEquinoctialEyDot() |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
removeRates() |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
CircularOrbit(double, double, double, double, double, double, PositionAngleType, PositionAngleType, Frame, AbsoluteDate, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
CircularOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) |  | 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 |
addKeplerContribution(PositionAngleType, double, 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(PositionAngleType) |  | 100% |  | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
getAlphaDot(PositionAngleType) |  | 100% |  | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
getEDot() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
CircularOrbit(double, double, double, double, double, double, PositionAngleType, Frame, AbsoluteDate, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 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 |
initializeCachedAlpha(double, PositionAngleType) |  | 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 |
eccentricToTrue(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
trueToEccentric(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
meanToEccentric(double, double, double) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
eccentricToMean(double, double, double) | | 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 |