public class BistaticRange extends GroundReceiverMeasurement<BistaticRange>
该测量被认为是一个信号:
在信号飞行时间内考虑地面站和航天器的运动。
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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BistaticRange(GroundStation emitter, GroundStation receiver, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite satellite)
简单构造函数。
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Modifier and Type | Method and Description |
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GroundStation |
getEmitterStation()
获取发射地面站。
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GroundStation |
getReceiverStation()
获取接收地面站。
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protected EstimatedMeasurement<BistaticRange> |
theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
估算理论值。
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protected EstimatedMeasurementBase<BistaticRange> |
theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)
估算不带导数的理论值。
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computeCommonParametersWithDerivatives, computeCommonParametersWithout, getGroundStationCoordinates, getGroundStationPosition, getStation, isTwoWay
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 BistaticRange(GroundStation emitter, GroundStation receiver, AbsoluteDate date, double range, double sigma, double baseWeight, ObservableSatellite satellite)
emitter
- 执行传输的地面站
receiver
- 执行测量的地面站
date
- 测量的日期
range
- 观测值
sigma
- 理论标准偏差
baseWeight
- 基本权重
satellite
- 与此测量相关的卫星
public GroundStation getEmitterStation()
public GroundStation getReceiverStation()
protected EstimatedMeasurementBase<BistaticRange> theoreticalEvaluationWithoutDerivatives(int iteration, int evaluation, SpacecraftState[] states)
理论值没有应用任何修饰符。
theoreticalEvaluationWithoutDerivatives
在类中 AbstractMeasurement<BistaticRange>
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<BistaticRange> theoreticalEvaluation(int iteration, int evaluation, SpacecraftState[] states)
理论值没有应用任何修饰符。
theoreticalEvaluation
在类中 AbstractMeasurement<BistaticRange>
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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