org.orekit.propagation.events
Class SolarTimeAngleDetector

java.lang.Object
  extended by org.orekit.propagation.events.AbstractDetector
      extended by org.orekit.propagation.events.SolarTimeAngleDetector
All Implemented Interfaces:
Serializable, EventDetector

public class SolarTimeAngleDetector
extends AbstractDetector

Detects when the solar time angle of a spacecraft is equal to a predetermined value.
The solar time is represented by the angle between the projections of the Sun in the osculator orbital plane and the satellite position; therefore this angle is equal to zero when the solar time is 12.00h and Π when the solar time is 0.00h (Solar Time In Hours = 12.00h + solar time angle * 12 / Π).

The default implementation is to stop propagation when the solar time is reached. This can be changed by using provided constructors.

Since:
1.2
Version:
$Id: SolarTimeAngleDetector.java 17582 2017-05-10 12:58:16Z bignon $
Author:
Tiziana Sabatini
See Also:
EventDetector, Serialized Form
Concurrency :
not thread-safe
Concurrency comment :
attributes are mutable and related to propagation.

Nested Class Summary
 
Nested classes/interfaces inherited from interface org.orekit.propagation.events.EventDetector
EventDetector.Action
 
Field Summary
 
Fields inherited from class org.orekit.propagation.events.AbstractDetector
DEFAULT_MAXCHECK, DEFAULT_THRESHOLD
 
Fields inherited from interface org.orekit.propagation.events.EventDetector
DECREASING, INCREASING, INCREASING_DECREASING
 
Constructor Summary
SolarTimeAngleDetector(double solarTimeAngle)
          Constructor for a SolarTimeDetector instance.
SolarTimeAngleDetector(double solarTimeAngle, double maxCheck, double threshold)
          Constructor for a SolarTimeDetector instance with complimentary parameters.
SolarTimeAngleDetector(double solarTimeAngle, double maxCheck, double threshold, EventDetector.Action action)
          Constructor for a SolarTimeDetector instance with complimentary parameters.
SolarTimeAngleDetector(double solarTimeAngle, double maxCheck, double threshold, EventDetector.Action action, boolean remove)
          Constructor for a SolarTimeDetector instance with complimentary parameters.
 
Method Summary
 EventDetector.Action eventOccurred(SpacecraftState s, boolean increasing, boolean forward)
          Handle a solar time angle event and choose what to do next.
 double g(SpacecraftState s)
          Compute the value of the switching function.
 double getTime()
          Get solar time angle to detect.
 void init(SpacecraftState s0, AbsoluteDate t)
          Initialize event handler at the start of a propagation.
 boolean shouldBeRemoved()
          This method is called after EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered.
 
Methods inherited from class org.orekit.propagation.events.AbstractDetector
getMaxCheckInterval, getMaxIterationCount, getSlopeSelection, getThreshold, resetState
 
Methods inherited from class java.lang.Object
clone, equals, finalize, getClass, hashCode, notify, notifyAll, toString, wait, wait, wait
 

Constructor Detail

SolarTimeAngleDetector

public SolarTimeAngleDetector(double solarTimeAngle)
                       throws OrekitException
Constructor for a SolarTimeDetector instance.

Parameters:
solarTimeAngle - satellite solar time angle triggering the event (in the range [-Π, Π[). Angle between the projection of the Sun in the osculator orbital plane and the satellite position (Solar Time In Hours = 12.00h + solar time angle * 12 / Π).
Throws:
OrekitException - error when loading the ephemeris files or solar time angle not in the range [-Π, Π[

SolarTimeAngleDetector

public SolarTimeAngleDetector(double solarTimeAngle,
                              double maxCheck,
                              double threshold)
                       throws OrekitException
Constructor for a SolarTimeDetector instance with complimentary parameters.

Parameters:
solarTimeAngle - satellite solar time angle triggering the event (in the range [-Π, Π[). Angle between the projection of the Sun in the osculator orbital plane and the satellite position (Solar Time In Hours = 12.00h + solar time angle * 12 / Π).
maxCheck - maximum check (see AbstractDetector)
threshold - threshold (see AbstractDetector)
Throws:
OrekitException - error when loading the ephemeris files or solar time angle not in the range [-Π, Π[

SolarTimeAngleDetector

public SolarTimeAngleDetector(double solarTimeAngle,
                              double maxCheck,
                              double threshold,
                              EventDetector.Action action)
                       throws OrekitException
Constructor for a SolarTimeDetector instance with complimentary parameters.

Parameters:
solarTimeAngle - satellite solar time angle triggering the event (in the range [-Π, Π[). Angle between the projection of the Sun in the osculator orbital plane and the satellite position (Solar Time In Hours = 12.00h + solar time angle * 12 / Π).
maxCheck - maximum check (see AbstractDetector)
threshold - threshold (see AbstractDetector)
action - action performed at solar time detection
Throws:
OrekitException - error when loading the ephemeris files or solar time angle not in the range [-Π, Π[

SolarTimeAngleDetector

public SolarTimeAngleDetector(double solarTimeAngle,
                              double maxCheck,
                              double threshold,
                              EventDetector.Action action,
                              boolean remove)
                       throws OrekitException
Constructor for a SolarTimeDetector instance with complimentary parameters.

Parameters:
solarTimeAngle - satellite solar time angle triggering the event (in the range [-Π, Π[). Angle between the projection of the Sun in the osculator orbital plane and the satellite position (Solar Time In Hours = 12.00h + solar time angle * 12 / Π).
maxCheck - maximum check (see AbstractDetector)
threshold - threshold (see AbstractDetector)
action - action performed at solar time detection
remove - true if detector should be removed
Throws:
OrekitException - error when loading the ephemeris files or solar time angle not in the range [-Π, Π[
Since:
3.1
Method Detail

eventOccurred

public EventDetector.Action eventOccurred(SpacecraftState s,
                                          boolean increasing,
                                          boolean forward)
                                   throws OrekitException
Handle a solar time angle event and choose what to do next.

The default implementation behavior is to stop propagation when the solar time is reached.

Specified by:
eventOccurred in interface EventDetector
Specified by:
eventOccurred in class AbstractDetector
Parameters:
s - the current state information : date, kinematics, attitude.
increasing - if true, the value of the switching function increases when time increases around event.
forward - if true, the integration variable (time) increases during integration.
Returns:
the action performed when the expected solar time is reached
Throws:
OrekitException - if some specific error occurs

shouldBeRemoved

public boolean shouldBeRemoved()
This method is called after EventDetector.eventOccurred(org.orekit.propagation.SpacecraftState, boolean, boolean) has been triggered. It returns true if the current detector should be removed after first event detection. WARNING: this method can be called only once a event has been triggered. Before, the value is not available.

Specified by:
shouldBeRemoved in interface EventDetector
Specified by:
shouldBeRemoved in class AbstractDetector
Returns:
true if the current detector should be removed after first event detection

g

public double g(SpacecraftState s)
         throws OrekitException
Description copied from class: AbstractDetector
Compute the value of the switching function. This function must be continuous (at least in its roots neighborhood), as the integrator will need to find its roots to locate the events.

Specified by:
g in interface EventDetector
Specified by:
g in class AbstractDetector
Parameters:
s - the current state information: date, kinematics, attitude for forces and events computation, mass provider, and additional states
Returns:
value of the switching function
Throws:
OrekitException - if some specific error occurs

init

public void init(SpacecraftState s0,
                 AbsoluteDate t)
Description copied from class: AbstractDetector
Initialize event handler at the start of a propagation.

This method is called once at the start of the propagation. It may be used by the event handler to initialize some internal data if needed.

Specified by:
init in interface EventDetector
Overrides:
init in class AbstractDetector
Parameters:
s0 - initial state
t - target time for the integration

getTime

public double getTime()
Get solar time angle to detect.

Returns:
the solar time angle triggering the event.


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