public class MultiplexedMeasurement extends AbstractMeasurement<MultiplexedMeasurement>
日期来自第一个测量,观测值和估计值来自于汇总所有基础测量值。
Modifier and Type | Field and Description |
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static String |
MEASUREMENT_TYPE
测量的类型。
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Constructor and Description |
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MultiplexedMeasurement(List<ObservedMeasurement<?>> measurements)
简单构造函数。
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Modifier and Type | Method and Description |
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List<EstimatedMeasurement<?>> |
getEstimatedMeasurements()
获取基础的估计测量值。
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List<EstimatedMeasurementBase<?>> |
getEstimatedMeasurementsWithoutDerivatives()
获取没有导数的基础估计测量值。
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List<ObservedMeasurement<?>> |
getMeasurements()
获取基础测量值。
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protected EstimatedMeasurement<MultiplexedMeasurement> |
theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
估计理论值。
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protected EstimatedMeasurementBase<MultiplexedMeasurement> |
theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)
获取没有导数的基础估计测量值。
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addModifier, addParameterDriver, estimate, estimateWithoutDerivatives, getBaseWeight, getCoordinates, getDate, getDimension, getModifiers, getObservedValue, getParametersDrivers, getSatellites, getTheoreticalStandardDeviation, isEnabled, setEnabled, signalTimeOfFlight, signalTimeOfFlight
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait
getMeasurementType
compareTo
durationFrom
getNbParametersDriversValue, getParameterDriver, getParameters, getParameters, getParameters, getParameters, getParametersAllValues, getParametersAllValues, isSupported
public MultiplexedMeasurement(List<ObservedMeasurement<?>> measurements)
measurements
- 要合并的测量
public List<ObservedMeasurement<?>> getMeasurements()
public List<EstimatedMeasurementBase<?>> getEstimatedMeasurementsWithoutDerivatives()
public List<EstimatedMeasurement<?>> getEstimatedMeasurements()
protected EstimatedMeasurementBase<MultiplexedMeasurement> theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)
理论值没有应用任何修饰符。
theoreticalEvaluationWithoutDerivatives
在类 AbstractMeasurement<MultiplexedMeasurement>
iteration
- 迭代次数
evaluation
- 评估次数
states
- 测量日期的轨道状态
AbstractMeasurement.estimate(int, int, SpacecraftState[])
protected EstimatedMeasurement<MultiplexedMeasurement> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
理论值没有应用任何修饰符。
theoreticalEvaluation
在类 AbstractMeasurement<MultiplexedMeasurement>
iteration
- 迭代次数
evaluation
- 评估次数
states
- 测量日期的轨道状态
AbstractMeasurement.estimate(int, int, SpacecraftState[])
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