AdapterPropagator.DifferentialEffect (OREKIT 13.1.2 API)

All Known Implementing Classes:

J2DifferentialEffect, SmallManeuverAnalyticalModel

Enclosing class:

AdapterPropagator
```
public static interface AdapterPropagator.DifferentialEffect
```
Interface for orbit differential effects.

- Method Summary
  
  All Methods Instance Methods Abstract Methods
  Modifier and Type Method Description
  
  SpacecraftState apply(SpacecraftState original)
  Apply the effect to a spacecraft state.

- Method Detail
  - apply
```
SpacecraftState apply(SpacecraftState original)
```
    Apply the effect to a spacecraft state.
    Applying the effect may be a no-op in some cases. A typical example is maneuvers, for which the state is changed only for time after the maneuver occurrence.
    
    Parameters:
    
    original - original state without the effect
    
    Returns:
    
    updated state at the same date, taking the effect into account if meaningful