| validate(double) |   | 83% | | 87% | 2 | 9 | 2 | 17 | 0 | 1 |
| setInRotationAngles(boolean) | | 0% | | n/a | 1 | 1 | 3 | 3 | 1 | 1 |
| inRotationAngles() | | 0% | | n/a | 1 | 1 | 1 | 1 | 1 | 1 |
| isSpacecraftBodyRate() | | 84% | | 50% | 1 | 2 | 0 | 1 | 0 | 1 |
| setAngleOrRate(double[], char, double) | | 100% | | 85% | 2 | 8 | 0 | 9 | 0 | 1 |
| Euler() | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| hasRates() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| rateFrameIsA() | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
| setRotationAngle(char, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setRotationRate(char, double) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setRateFrameIsA(boolean) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| setEulerRotSeq(RotationOrder) | | 100% | | n/a | 0 | 1 | 0 | 3 | 0 | 1 |
| getRotationAngles() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getRotationRates() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEndpoints() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getEulerRotSeq() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |