ensureCompatibleAdditionalStates(SpacecraftState) |  | 99% |   | 83% | 2 | 7 | 0 | 12 | 0 | 1 |
interpolate(AbsoluteDate, Collection) |  | 100% |  | 100% | 0 | 6 | 0 | 23 | 0 | 1 |
SpacecraftState(Orbit, Attitude, double, Map) |  | 100% |  | 100% | 0 | 3 | 0 | 11 | 0 | 1 |
checkConsistency(Orbit, Attitude) |  | 100% |  | 100% | 0 | 3 | 0 | 5 | 0 | 1 |
addAdditionalState(String, double[]) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getAdditionalState(String) |  | 100% |  | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
toTransform() |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit, Map) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit, double, Map) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
shiftedBy(double) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
SpacecraftState(Orbit, Attitude) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit, Attitude, double) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
SpacecraftState(Orbit, Attitude, Map) |  | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
hasAdditionalState(String) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPVCoordinates(Frame) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDate() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFrame() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAdditionalStates() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMu() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getKeplerianPeriod() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getKeplerianMeanMotion() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getA() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEx() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEquinoctialEy() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHx() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getHy() |  | 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 |
getE() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getI() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPVCoordinates() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getOrbit() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getAttitude() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getMass() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |