EquinoctialOrbit(TimeStampedPVCoordinates, Frame, double) |   | 96% |   | 75% | 1 | 3 | 2 | 54 | 0 | 1 |
EquinoctialOrbit(double, double, double, double, double, double, double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) |   | 93% |   | 83% | 2 | 9 | 2 | 40 | 0 | 1 |
addKeplerContribution(PositionAngle, double, double[]) |   | 95% |   | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
computeJacobianMeanWrtCartesian() |  | 100% | | n/a | 0 | 1 | 0 | 52 | 0 | 1 |
interpolate(AbsoluteDate, Stream) |  | 100% |  | 100% | 0 | 7 | 0 | 40 | 0 | 1 |
computePVWithoutA() |  | 100% |  | 100% | 0 | 2 | 0 | 31 | 0 | 1 |
nonKeplerianAcceleration() |  | 100% | | n/a | 0 | 1 | 0 | 7 | 0 | 1 |
computeJacobianTrueWrtCartesian() |  | 100% |  | 100% | 0 | 2 | 0 | 23 | 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 | 11 | 0 | 1 |
EquinoctialOrbit(Orbit) |  | 100% | | n/a | 0 | 1 | 0 | 15 | 0 | 1 |
eccentricToTrue(double, double, double) |  | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
trueToEccentric(double, double, double) |  | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
initPVCoordinates() |  | 100% |  | 100% | 0 | 2 | 0 | 6 | 0 | 1 |
toString() |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
getLMDot() |  | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
getIDot() |  | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
getLEDot() |  | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
getEDot() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
EquinoctialOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getI() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getL(PositionAngle) |  | 100% |  | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
getLDot(PositionAngle) |  | 100% |  | 100% | 0 | 3 | 0 | 3 | 0 | 1 |
eccentricToMean(double, double, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getLM() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getE() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
EquinoctialOrbit(PVCoordinates, Frame, AbsoluteDate, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
getLE() |  | 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 |
getEquinoctialEx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialExDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEyDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHx() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHxDot() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHy() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHyDot() | | 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 |
getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |