Comparable<Range>
, ComparableMeasurement
, ObservedMeasurement<Range>
, TimeStamped
public class Range extends AbstractMeasurement<Range>
For two-way measurements, the measurement is considered to be a signal emitted from a ground station, reflected on spacecraft, and received on the same ground station. Its value is the elapsed time between emission and reception divided by 2c were c is the speed of light.
For one-way measurements, a signal is emitted by the satellite and received by the ground station. The measurement value is the elapsed time between emission and reception divided by the speed of light.
The motion of both the station and the spacecraft during the signal flight time are taken into account. The date of the measurement corresponds to the reception on ground of the emitted or reflected signal.
Constructor | Description |
---|---|
Range(GroundStation station,
boolean twoWay,
AbsoluteDate date,
double range,
double sigma,
double baseWeight,
int propagatorIndex) |
Simple constructor.
|
Range(GroundStation station,
AbsoluteDate date,
double range,
double sigma,
double baseWeight) |
Simple constructor.
|
Range(GroundStation station,
AbsoluteDate date,
double range,
double sigma,
double baseWeight,
boolean twoWay) |
Simple constructor.
|
Range(GroundStation station,
AbsoluteDate date,
double range,
double sigma,
double baseWeight,
int propagatorIndex) |
Simple constructor.
|
Modifier and Type | Method | Description |
---|---|---|
GroundStation |
getStation() |
Get the ground station from which measurement is performed.
|
boolean |
isTwoWay() |
Check if the instance represents a two-way measurement.
|
protected EstimatedMeasurement<Range> |
theoreticalEvaluation(int iteration,
int evaluation,
SpacecraftState[] states) |
Estimate the theoretical value.
|
addModifier, estimate, getBaseWeight, getCoordinates, getDate, getDimension, getModifiers, getObservedValue, getParametersDrivers, getPropagatorsIndices, getTheoreticalStandardDeviation, isEnabled, setEnabled, signalTimeOfFlight, signalTimeOfFlight
compareTo
public Range(GroundStation station, AbsoluteDate date, double range, double sigma, double baseWeight) throws OrekitException
This constructor uses 0 as the index of the propagator related to this measurement, thus being well suited for mono-satellite orbit determination.
station
- ground station from which measurement is performeddate
- date of the measurementrange
- observed valuesigma
- theoretical standard deviationbaseWeight
- base weightOrekitException
- if a ParameterDriver
name conflict occurspublic Range(GroundStation station, AbsoluteDate date, double range, double sigma, double baseWeight, boolean twoWay) throws OrekitException
This constructor uses 0 as the index of the propagator related to this measurement, thus being well suited for mono-satellite orbit determination.
station
- ground station from which measurement is performeddate
- date of the measurementrange
- observed valuesigma
- theoretical standard deviationbaseWeight
- base weighttwoWay
- flag indicating whether it is a two-way measurementOrekitException
- if a ParameterDriver
name conflict occurspublic Range(GroundStation station, AbsoluteDate date, double range, double sigma, double baseWeight, int propagatorIndex) throws OrekitException
station
- ground station from which measurement is performeddate
- date of the measurementrange
- observed valuesigma
- theoretical standard deviationbaseWeight
- base weightpropagatorIndex
- index of the propagator related to this measurementOrekitException
- if a ParameterDriver
name conflict occurspublic Range(GroundStation station, boolean twoWay, AbsoluteDate date, double range, double sigma, double baseWeight, int propagatorIndex) throws OrekitException
station
- ground station from which measurement is performedtwoWay
- flag indicating whether it is a two-way measurementdate
- date of the measurementrange
- observed valuesigma
- theoretical standard deviationbaseWeight
- base weightpropagatorIndex
- index of the propagator related to this measurementOrekitException
- if a ParameterDriver
name conflict occurspublic GroundStation getStation()
public boolean isTwoWay()
protected EstimatedMeasurement<Range> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states) throws OrekitException
The theoretical value does not have any modifiers applied.
theoreticalEvaluation
in class AbstractMeasurement<Range>
iteration
- iteration numberevaluation
- evaluation numberstates
- orbital states at measurement dateOrekitException
- if value cannot be computedAbstractMeasurement.estimate(int, int, SpacecraftState[])
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