isStateDerivative(FieldSpacecraftState) |  | 98% |   | 65% | 7 | 11 | 0 | 14 | 0 | 1 |
isVariable(DerivativeStructure, int) |  | 97% |   | 83% | 1 | 4 | 0 | 5 | 0 | 1 |
getDensityWrtStateUsingFiniteDifferences(AbsoluteDate, Frame, FieldVector3D) |  | 100% |  | 100% | 0 | 2 | 0 | 28 | 0 | 1 |
acceleration(FieldSpacecraftState, RealFieldElement[]) |  | 100% |  | 100% | 0 | 2 | 0 | 10 | 0 | 1 |
acceleration(SpacecraftState, double[]) |  | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
DragForce(Atmosphere, DragSensitive) |  | 100% | | n/a | 0 | 1 | 0 | 4 | 0 | 1 |
getParametersDrivers() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
dependsOnPositionOnly() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getEventsDetectors() |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getFieldEventsDetectors(Field) |  | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |