UnivariateProcessNoise(RealMatrix, LOFType, PositionAngle, UnivariateFunction[], UnivariateFunction[]) | | 55% | | 50% | 1 | 2 | 2 | 9 | 0 | 1 |
getProcessNoiseMatrix(SpacecraftState, SpacecraftState) | | 95% | | 50% | 1 | 2 | 1 | 10 | 0 | 1 |
getInertialOrbitalProcessNoiseMatrix(SpacecraftState, SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 29 | 0 | 1 |
getPropagationProcessNoiseMatrix(SpacecraftState, SpacecraftState) | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
getLofType() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPositionAngle() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getLofCartesianOrbitalParametersEvolution() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
getPropagationParametersEvolution() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |