KalmanEstimation (ORbit Extrapolation KIT 9.2 API)

```
public interface KalmanEstimation
```
Interface for accessing Kalman filter estimations.

Since:

9.2

Author:

Luc Maisonobe

Method Summary

All Methods Instance Methods Abstract Methods
Modifier and Type	Method	Description
`EstimatedMeasurement<?>`	`getCorrectedMeasurement()`	Get the estimated measurement.
`SpacecraftState[]`	`getCorrectedSpacecraftStates()`	Get the corrected spacecraft states.
`AbsoluteDate`	`getCurrentDate()`	Get the current date.
`int`	`getCurrentMeasurementNumber()`	Get the current measurement number.
`ParameterDriversList`	`getEstimatedMeasurementsParameters()`	Get the list of estimated measurements parameters.
`ParameterDriversList`	`getEstimatedOrbitalParameters()`	Get the list of estimated orbital parameters.
`ParameterDriversList`	`getEstimatedPropagationParameters()`	Get the list of estimated propagation parameters.
`RealMatrix`	`getPhysicalEstimatedCovarianceMatrix()`	Get the "physical" estimated covariance matrix (i.e.
`RealVector`	`getPhysicalEstimatedState()`	Get the "physical" estimated state (i.e.
`EstimatedMeasurement<?>`	`getPredictedMeasurement()`	Get the predicted measurement.
`SpacecraftState[]`	`getPredictedSpacecraftStates()`	Get the predicted spacecraft states.

- Method Detail
  - getEstimatedOrbitalParameters
```
ParameterDriversList getEstimatedOrbitalParameters()
```
    Get the list of estimated orbital parameters.
    
    Returns:
    
    the list of estimated orbital parameters
  - getEstimatedPropagationParameters
```
ParameterDriversList getEstimatedPropagationParameters()
```
    Get the list of estimated propagation parameters.
    
    Returns:
    
    the list of estimated propagation parameters
  - getEstimatedMeasurementsParameters
```
ParameterDriversList getEstimatedMeasurementsParameters()
```
    Get the list of estimated measurements parameters.
    
    Returns:
    
    the list of estimated measurements parameters
  - getPredictedSpacecraftStates
```
SpacecraftState[] getPredictedSpacecraftStates()
```
    Get the predicted spacecraft states.
    
    Returns:
    
    predicted spacecraft states
  - getCorrectedSpacecraftStates
```
SpacecraftState[] getCorrectedSpacecraftStates()
```
    Get the corrected spacecraft states.
    
    Returns:
    
    corrected spacecraft states
  - getPhysicalEstimatedState
```
RealVector getPhysicalEstimatedState()
```
    Get the "physical" estimated state (i.e. not normalized)
    
    Returns:
    
    the "physical" estimated state
  - getPhysicalEstimatedCovarianceMatrix
```
RealMatrix getPhysicalEstimatedCovarianceMatrix()
```
    Get the "physical" estimated covariance matrix (i.e. not normalized)
    
    Returns:
    
    the "physical" estimated covariance matrix
  - getCurrentMeasurementNumber
```
int getCurrentMeasurementNumber()
```
    Get the current measurement number.
    
    Returns:
    
    current measurement number
  - getCurrentDate
```
AbsoluteDate getCurrentDate()
```
    Get the current date.
    
    Returns:
    
    current date
  - getPredictedMeasurement
```
EstimatedMeasurement<?> getPredictedMeasurement()
```
    Get the predicted measurement.
    This estimation has been evaluated on the last predicted orbits
    
    Returns:
    
    predicted measurement
  - getCorrectedMeasurement
```
EstimatedMeasurement<?> getCorrectedMeasurement()
```
    Get the estimated measurement.
    This estimation has been evaluated on the last corrected orbits
    
    Returns:
    
    corrected measurement

Interface KalmanEstimation

Method Summary

Method Detail

getEstimatedOrbitalParameters

getEstimatedPropagationParameters

getEstimatedMeasurementsParameters

getPredictedSpacecraftStates

getCorrectedSpacecraftStates

getPhysicalEstimatedState

getPhysicalEstimatedCovarianceMatrix

getCurrentMeasurementNumber

getCurrentDate

getPredictedMeasurement

getCorrectedMeasurement