Package | Description |
---|---|
org.orekit.estimation.leastsquares |
The leastsquares package provides an implementation of a batch least
squares estimator engine to perform an orbit determination.
|
org.orekit.estimation.measurements |
The measurements package defines everything that is related to orbit
determination measurements.
|
org.orekit.estimation.measurements.gnss |
This package provides methods to handle GNSS measurements.
|
org.orekit.estimation.measurements.modifiers |
This package provides measurement modifier.
|
org.orekit.estimation.sequential |
The sequential package provides an implementation of a
Kalman Filter engine to perform an orbit determination.
|
Modifier and Type | Method and Description |
---|---|
Map<ObservedMeasurement<?>,EstimatedMeasurement<?>> |
BatchLSEstimator.getLastEstimations()
Get the last estimations performed.
|
Modifier and Type | Method and Description |
---|---|
void |
AbstractBatchLSModel.fetchEvaluatedMeasurement(int index,
EstimatedMeasurement<?> evaluation)
Fetch a measurement that was evaluated during propagation.
|
Modifier and Type | Method and Description |
---|---|
void |
ModelObserver.modelCalled(Orbit[] orbits,
Map<ObservedMeasurement<?>,EstimatedMeasurement<?>> estimations)
Notification callback for orbit changes.
|
Modifier and Type | Method and Description |
---|---|
EstimatedMeasurement<T> |
ObservedMeasurement.estimate(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value of the measurement, with derivatives.
|
EstimatedMeasurement<T> |
AbstractMeasurement.estimate(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value of the measurement, with derivatives.
|
EstimatedMeasurement<?> |
EstimationsProvider.getEstimatedMeasurement(int index)
Get one estimated measurement.
|
protected EstimatedMeasurement<TurnAroundRange> |
TurnAroundRange.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<AngularAzEl> |
AngularAzEl.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<MultiplexedMeasurement> |
MultiplexedMeasurement.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<BistaticRange> |
BistaticRange.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<RangeRate> |
RangeRate.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<PV> |
PV.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<Position> |
Position.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected abstract EstimatedMeasurement<T> |
AbstractMeasurement.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<InterSatellitesRange> |
InterSatellitesRange.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<BistaticRangeRate> |
BistaticRangeRate.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<FDOA> |
FDOA.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<AngularRaDec> |
AngularRaDec.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<TDOA> |
TDOA.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<Range> |
Range.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
Modifier and Type | Method and Description |
---|---|
List<EstimatedMeasurement<?>> |
MultiplexedMeasurement.getEstimatedMeasurements()
Get the underlying estimated measurements.
|
Modifier and Type | Method and Description |
---|---|
default void |
EstimationModifier.modify(EstimatedMeasurement<T> estimated)
Apply a modifier to an estimated measurement.
|
Modifier and Type | Method and Description |
---|---|
protected EstimatedMeasurement<Phase> |
Phase.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<OneWayGNSSPhase> |
OneWayGNSSPhase.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<OneWayGNSSRange> |
OneWayGNSSRange.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
protected EstimatedMeasurement<InterSatellitesPhase> |
InterSatellitesPhase.theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states)
Estimate the theoretical value.
|
Modifier and Type | Method and Description |
---|---|
protected void |
AbstractAmbiguityModifier.doModify(EstimatedMeasurement<?> estimated)
Modify measurement.
|
void |
AberrationModifier.modify(EstimatedMeasurement<AngularRaDec> estimated)
Apply a modifier to an estimated measurement.
|
void |
BistaticRangeIonosphericDelayModifier.modify(EstimatedMeasurement<BistaticRange> estimated)
Apply a modifier to an estimated measurement.
|
void |
BistaticRangeTroposphericDelayModifier.modify(EstimatedMeasurement<BistaticRange> estimated)
Apply a modifier to an estimated measurement.
|
void |
BistaticRangeRateTroposphericDelayModifier.modify(EstimatedMeasurement<BistaticRangeRate> estimated)
Apply a modifier to an estimated measurement.
|
void |
BistaticRangeRateIonosphericDelayModifier.modify(EstimatedMeasurement<BistaticRangeRate> estimated)
Apply a modifier to an estimated measurement.
|
void |
InterSatellitesPhaseAmbiguityModifier.modify(EstimatedMeasurement<InterSatellitesPhase> estimated)
Apply a modifier to an estimated measurement.
|
void |
OneWayGNSSPhaseAmbiguityModifier.modify(EstimatedMeasurement<OneWayGNSSPhase> estimated)
Apply a modifier to an estimated measurement.
|
void |
PhaseIonosphericDelayModifier.modify(EstimatedMeasurement<Phase> estimated) |
void |
PhaseAmbiguityModifier.modify(EstimatedMeasurement<Phase> estimated) |
void |
PhaseTroposphericDelayModifier.modify(EstimatedMeasurement<Phase> estimated)
Apply a modifier to an estimated measurement.
|
void |
RangeTroposphericDelayModifier.modify(EstimatedMeasurement<Range> estimated)
Apply a modifier to an estimated measurement.
|
void |
RangeIonosphericDelayModifier.modify(EstimatedMeasurement<Range> estimated)
Apply a modifier to an estimated measurement.
|
void |
RangeRateTroposphericDelayModifier.modify(EstimatedMeasurement<RangeRate> estimated)
Apply a modifier to an estimated measurement.
|
void |
RangeRateIonosphericDelayModifier.modify(EstimatedMeasurement<RangeRate> estimated)
Apply a modifier to an estimated measurement.
|
void |
DynamicOutlierFilter.modify(EstimatedMeasurement<T> estimated)
Apply a modifier to an estimated measurement.
|
void |
Bias.modify(EstimatedMeasurement<T> estimated)
Apply a modifier to an estimated measurement.
|
static <T extends ObservedMeasurement<T>> |
RangeRateModifierUtil.modify(EstimatedMeasurement<T> estimated,
ParameterDriversProvider parametricModel,
AbstractGradientConverter converter,
GroundStation station,
org.orekit.estimation.measurements.modifiers.ParametricModelEffect modelEffect,
org.orekit.estimation.measurements.modifiers.ParametricModelEffectGradient modelEffectGradient)
Apply a modifier to an estimated measurement.
|
static <T extends ObservedMeasurement<T>> |
RangeModifierUtil.modify(EstimatedMeasurement<T> estimated,
ParameterDriversProvider parametricModel,
AbstractGradientConverter converter,
GroundStation station,
org.orekit.estimation.measurements.modifiers.ParametricModelEffect modelEffect,
org.orekit.estimation.measurements.modifiers.ParametricModelEffectGradient modelEffectGradient)
Apply a modifier to an estimated measurement.
|
void |
TDOATroposphericDelayModifier.modify(EstimatedMeasurement<TDOA> estimated)
Apply a modifier to an estimated measurement.
|
void |
TDOAIonosphericDelayModifier.modify(EstimatedMeasurement<TDOA> estimated) |
void |
TurnAroundRangeTroposphericDelayModifier.modify(EstimatedMeasurement<TurnAroundRange> estimated)
Apply a modifier to an estimated measurement.
|
void |
TurnAroundRangeIonosphericDelayModifier.modify(EstimatedMeasurement<TurnAroundRange> estimated) |
Modifier and Type | Method and Description |
---|---|
EstimatedMeasurement<?> |
UnscentedKalmanModel.getCorrectedMeasurement()
Get the estimated measurement.
|
EstimatedMeasurement<?> |
SemiAnalyticalUnscentedKalmanModel.getCorrectedMeasurement()
Get the estimated measurement.
|
EstimatedMeasurement<?> |
KalmanModel.getCorrectedMeasurement()
Get the estimated measurement.
|
EstimatedMeasurement<?> |
SemiAnalyticalKalmanModel.getCorrectedMeasurement()
Get the estimated measurement.
|
EstimatedMeasurement<?> |
KalmanEstimation.getCorrectedMeasurement()
Get the estimated measurement.
|
EstimatedMeasurement<?> |
UnscentedKalmanModel.getPredictedMeasurement()
Get the predicted measurement.
|
EstimatedMeasurement<?> |
SemiAnalyticalUnscentedKalmanModel.getPredictedMeasurement()
Get the predicted measurement.
|
EstimatedMeasurement<?> |
KalmanModel.getPredictedMeasurement()
Get the predicted measurement.
|
EstimatedMeasurement<?> |
SemiAnalyticalKalmanModel.getPredictedMeasurement()
Get the predicted measurement.
|
EstimatedMeasurement<?> |
KalmanEstimation.getPredictedMeasurement()
Get the predicted measurement.
|
Modifier and Type | Method and Description |
---|---|
static <T extends ObservedMeasurement<T>> |
KalmanEstimatorUtil.applyDynamicOutlierFilter(EstimatedMeasurement<T> measurement,
org.hipparchus.linear.RealMatrix innovationCovarianceMatrix)
Set and apply a dynamic outlier filter on a measurement.
|
static org.hipparchus.linear.RealVector |
KalmanEstimatorUtil.computeInnovationVector(EstimatedMeasurement<?> predicted)
Compute the unnormalized innovation vector from the given predicted measurement.
|
static org.hipparchus.linear.RealVector |
KalmanEstimatorUtil.computeInnovationVector(EstimatedMeasurement<?> predicted,
double[] sigma)
Compute the normalized innovation vector from the given predicted measurement.
|
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