Package | Description |
---|---|
org.orekit.estimation.measurements |
The measurements package defines everything that is related to orbit
determination measurements.
|
org.orekit.propagation.conversion |
This package provides tools to convert a given propagator or a set of
SpacecraftState into another propagator. |
org.orekit.propagation.events |
This package provides interfaces and classes dealing with events occurring during propagation.
|
org.orekit.time |
This independent package provides classes to handle epochs, time scales,
and to compare instants together.
|
Modifier and Type | Method and Description |
---|---|
double[] |
EstimatedMeasurement.getParameterDerivatives(ParameterDriver driver)
Get the partial derivatives of the
simulated measurement with respect to a parameter. |
Modifier and Type | Method and Description |
---|---|
protected void |
AbstractPropagatorBuilder.setParameters(double[] normalizedParameters)
Set the selected parameters.
|
Constructor and Description |
---|
PositionAngleDetector(double maxCheck,
double threshold,
OrbitType orbitType,
PositionAngle positionAngle,
double angle)
Build a detector.
|
PositionAngleDetector(OrbitType orbitType,
PositionAngle positionAngle,
double angle)
Build a new detector.
|
Modifier and Type | Method and Description |
---|---|
static AbsoluteDate |
AbsoluteDate.createMJDDate(int mjd,
double secondsInDay,
TimeScale timeScale)
Build an instance corresponding to a Modified Julian Day date.
|
Constructor and Description |
---|
TimeComponents(double secondInDay)
Build a time from the second number within the day.
|
TimeComponents(int secondInDayA,
double secondInDayB)
Build a time from the second number within the day.
|
Copyright © 2002-2017 CS Systèmes d'information. All rights reserved.