| getFieldDensity(FieldSpacecraftState) |   | 87% | | 87% | 1 | 5 | 1 | 12 | 0 | 1 |
| isDSStateDerivative(FieldSpacecraftState) | | 98% | | 60% | 8 | 11 | 0 | 14 | 0 | 1 |
| isVariable(DerivativeStructure, int) | | 97% | | 83% | 1 | 4 | 0 | 5 | 0 | 1 |
| getDSDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D) | | 100% | | 100% | 0 | 2 | 0 | 27 | 0 | 1 |
| getGradientDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D) | | 100% | | 100% | 0 | 2 | 0 | 24 | 0 | 1 |
| getDSDensityWrtState(AbsoluteDate, Frame, FieldVector3D) | | 100% | | n/a | 0 | 1 | 0 | 13 | 0 | 1 |
| isGradientStateDerivative(FieldSpacecraftState) | | 100% | | 72% | 5 | 10 | 0 | 13 | 0 | 1 |
| getGradientDensityWrtState(AbsoluteDate, Frame, FieldVector3D) | | 100% | | n/a | 0 | 1 | 0 | 12 | 0 | 1 |
| isVariable(Gradient, int) | | 100% | | 100% | 0 | 4 | 0 | 5 | 0 | 1 |
| AbstractDragForceModel(Atmosphere, boolean) | | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
| AbstractDragForceModel(Atmosphere) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getAtmosphere() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| dependsOnPositionOnly() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |