| validate(double) |   | 93% | | 96% | 1 | 14 | 1 | 19 | 0 | 1 |
| getAttitude(Frame, PVCoordinatesProvider) | | 100% | | 100% | 0 | 13 | 0 | 74 | 0 | 1 |
| ApmData(CommentsContainer, AbsoluteDate, ApmQuaternion, Euler, AngularVelocity, SpinStabilized, Inertia) | | 100% | | n/a | 0 | 1 | 0 | 10 | 0 | 1 |
| hasManeuvers() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| getManeuver(int) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| addManeuver(Maneuver) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getComments() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getNbManeuvers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getManeuvers() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEpoch() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getQuaternionBlock() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEulerBlock() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAngularVelocityBlock() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getSpinStabilizedBlock() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInertiaBlock() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |