org.orekit.estimation.measurements.generation

Class AngularRaDecBuilder

java.lang.Object

org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder<AngularRaDec>

org.orekit.estimation.measurements.generation.AngularRaDecBuilder

All Implemented Interfaces:

MeasurementBuilder<AngularRaDec>

public class AngularRaDecBuilder
extends AbstractMeasurementBuilder<AngularRaDec>

Builder for AngularRaDec measurements.

Since:

9.3

Author:

Luc Maisonobe

Constructor Summary

Constructors

Constructor and Description
AngularRaDecBuilder(CorrelatedRandomVectorGenerator noiseSource, GroundStation station, Frame referenceFrame, double[] sigma, double[] baseWeight, ObservableSatellite satellite) Simple constructor.

Method Summary

Modifier and Type	Method and Description
AngularRaDec	build(SpacecraftState[] states) Generate a single measurement.

Methods inherited from class org.orekit.estimation.measurements.generation.AbstractMeasurementBuilder

addModifier, getBaseWeight, getEnd, getModifiers, getNoise, getSatellites, getStart, getTheoreticalStandardDeviation, init

Methods inherited from class java.lang.Object

clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait

Constructor Detail

AngularRaDecBuilder

public AngularRaDecBuilder(CorrelatedRandomVectorGenerator noiseSource,
                           GroundStation station,
                           Frame referenceFrame,
                           double[] sigma,
                           double[] baseWeight,
                           ObservableSatellite satellite)

Simple constructor.

Parameters:

noiseSource - noise source, may be null for generating perfect measurements

station - ground station from which measurement is performed

referenceFrame - Reference frame in which the right ascension - declination angles are given

sigma - theoretical standard deviation

baseWeight - base weight

satellite - satellite related to this builder

Method Detail

build

public AngularRaDec build(SpacecraftState[] states)

Generate a single measurement.

Parameters:

states - spacecraft states

Returns:

generated measurement