| copy(double) |   | 95% | | 80% | 2 | 6 | 1 | 22 | 0 | 1 |
| checkMandatoryEntriesExceptDatesAndExternalFrame(double) | | 100% | | 100% | 0 | 8 | 0 | 10 | 0 | 1 |
| validate(double) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| isSpacecraftBodyRate() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| AemMetadata(int) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| getStart() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| getStop() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| rateFrameIsA() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| isFirst() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| setRateFrameIsA(boolean) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setIsFirst(boolean) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setAttitudeType(AttitudeType) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setEulerRotSeq(RotationOrder) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setStartTime(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setStopTime(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setUseableStartTime(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setUseableStopTime(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setInterpolationMethod(String) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setInterpolationDegree(int) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getInterpolationSamples() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEndpoints() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getAttitudeType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEulerRotSeq() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getStartTime() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getStopTime() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getUseableStartTime() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getUseableStopTime() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInterpolationMethod() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getInterpolationDegree() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |