toString() |  | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
KeplerianOrbit(double, double, double, double, double, double, int, Frame, AbsoluteDate, double) |   | 75% |   | 70% | 3 | 7 | 1 | 18 | 0 | 1 |
KeplerianOrbit(double, double, double, double, double, double, PositionAngle, Frame, AbsoluteDate, double) |   | 86% |   | 83% | 2 | 8 | 2 | 21 | 0 | 1 |
meanToHyperbolicEccentric(double, double) |   | 91% |   | 81% | 3 | 9 | 1 | 22 | 0 | 1 |
addKeplerContribution(PositionAngle, double, double[]) |  | 97% |   | 75% | 1 | 4 | 1 | 15 | 0 | 1 |
getHx() |  | 90% |   | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
getHy() |  | 90% |   | 50% | 1 | 2 | 1 | 3 | 0 | 1 |
computeJacobianMeanWrtCartesianElliptical() |  | 100% | | n/a | 0 | 1 | 0 | 73 | 0 | 1 |
computeJacobianMeanWrtCartesianHyperbolic() |  | 100% | | n/a | 0 | 1 | 0 | 88 | 0 | 1 |
meanToEllipticEccentric(double) |  | 100% |  | 100% | 0 | 6 | 0 | 26 | 0 | 1 |
KeplerianOrbit(PVCoordinates, Frame, AbsoluteDate, double) |  | 100% |  | 100% | 0 | 2 | 0 | 27 | 0 | 1 |
interpolate(AbsoluteDate, Collection) |  | 100% |  | 100% | 0 | 3 | 0 | 24 | 0 | 1 |
initPVCoordinates() |  | 100% |  | 100% | 0 | 2 | 0 | 13 | 0 | 1 |
initPVCoordinatesElliptical(Vector3D, Vector3D) |  | 100% | | n/a | 0 | 1 | 0 | 11 | 0 | 1 |
computeJacobianTrueWrtCartesianElliptical() |  | 100% |  | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
computeJacobianTrueWrtCartesianHyperbolic() |  | 100% |  | 100% | 0 | 2 | 0 | 15 | 0 | 1 |
getEccentricAnomaly() |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
initPVCoordinatesHyperbolic(Vector3D, Vector3D) |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
computeJacobianEccentricWrtCartesianElliptical() |  | 100% |  | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
computeJacobianEccentricWrtCartesianHyperbolic() |  | 100% |  | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
eMeSinE(double) |  | 100% |  | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
ellipticEccentricToTrue(double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
shiftedBy(double) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMeanAnomaly() |  | 100% |  | 100% | 0 | 2 | 0 | 5 | 0 | 1 |
hyperbolicEccentricToTrue(double) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAnomaly(PositionAngle) |  | 100% |  | 100% | 0 | 3 | 0 | 1 | 0 | 1 |
KeplerianOrbit(Orbit) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 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 |
static {...} |  | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
getEquinoctialEx() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEy() |  | 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 |
getA() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getE() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPerigeeArgument() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getRightAscensionOfAscendingNode() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getTrueAnomaly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |