ThrustVectorProvider (OREKIT 13.0-SNAPSHOT API)

All Known Implementing Classes:

PolynomialThrustSegment
```
public interface ThrustVectorProvider
```
Interface defining thrust vectors depending on date and mass only. The frame is assumed to be the satellite one.

Since:

13.0

Author:

Romain Serra

Method Summary

All Methods Instance Methods Abstract Methods
Modifier and Type	Method	Description
`Vector3D`	`getThrustVector(AbsoluteDate date, double mass)`	Get thrust vector at a specified date.
`<T extends CalculusFieldElement<T>> FieldVector3D<T>`	`getThrustVector(FieldAbsoluteDate<T> date, T mass)`	Get thrust vector at a specified date.

- Method Detail
  - getThrustVector
```
Vector3D getThrustVector(AbsoluteDate date,
                         double mass)
```
    Get thrust vector at a specified date.
    
    Parameters:
    
    date - date to consider
    
    mass - current mass
    
    Returns:
    
    thrust at date (N)
  - getThrustVector
```
<T extends CalculusFieldElement<T>> FieldVector3D<T> getThrustVector(FieldAbsoluteDate<T> date,
                                                                     T mass)
```
    Get thrust vector at a specified date.
    
    Type Parameters:
    
    T - type of the field elements
    
    Parameters:
    
    date - date to consider
    
    mass - current mass
    
    Returns:
    
    thrust at date (N)