setInitialStateTransitionMatrix(SpacecraftState, RealMatrix, OrbitType, PositionAngleType) | | 98% | | 91% | 1 | 7 | 1 | 20 | 0 | 1 |
computePartials(SpacecraftState) | | 100% | | 100% | 0 | 11 | 0 | 51 | 0 | 1 |
multiplyMatrix(double[], double[], double[], int) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
combinedDerivatives(SpacecraftState) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
StateTransitionMatrixGenerator(String, List, AttitudeProvider) | | 100% | | n/a | 0 | 1 | 0 | 6 | 0 | 1 |
wrapAttitudeProviderIfPossible(List, AttitudeProvider) | | 100% | | 100% | 0 | 2 | 0 | 3 | 0 | 1 |
yields(SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
addObserver(String, StateTransitionMatrixGenerator.PartialsObserver) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
lambda$computePartials$0(ForceModel) | | 100% | | 100% | 0 | 2 | 0 | 1 | 0 | 1 |
getName() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
static {...} | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getDimension() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |