Class NodeDetector

All Implemented Interfaces:
EventDetector

public class NodeDetector extends AbstractDetector<NodeDetector>
Finder for node crossing events.

This class finds equator crossing events (i.e. ascending or descending node crossing).

The default implementation behavior is to continue propagation at descending node crossing and to stop propagation at ascending node crossing. This can be changed by calling AbstractDetector.withHandler(EventHandler) after construction.

Beware that node detection will fail for almost equatorial orbits. If for example a node detector is used to trigger an ImpulseManeuver and the maneuver turn the orbit plane to equator, then the detector may completely fail just after the maneuver has been performed! This is a real case that has been encountered during validation ...

Author:
Luc Maisonobe
See Also:
  • Constructor Details

    • NodeDetector

      public NodeDetector(Frame frame)
      Build a new instance.

      The default max check interval is set to 1800s, it can be changed using AbstractDetector.withMaxCheck(double) in the fluent API. The default convergence threshold is set to 1.0e-3s, it can be changed using AbstractDetector.withThreshold(double) in the fluent API.

      Parameters:
      frame - frame in which the equator is defined (typical values are EME2000 or ITRF)
      Since:
      10.3
    • NodeDetector

      public NodeDetector(Orbit orbit, Frame frame)
      Build a new instance.

      The orbit is used only to set an upper bound for the max check interval to a value related to nodes separation (as computed by a Keplerian model) and to set the convergence threshold according to orbit size.

      Parameters:
      orbit - initial orbit
      frame - frame in which the equator is defined (typical values are EME2000 or ITRF)
    • NodeDetector

      public NodeDetector(double threshold, Orbit orbit, Frame frame)
      Build a new instance.

      The orbit is used only to set an upper bound for the max check interval to a value related to nodes separation (as computed by a Keplerian model).

      Parameters:
      threshold - convergence threshold (s)
      orbit - initial orbit
      frame - frame in which the equator is defined (typical values are EME2000 or ITRF)
    • NodeDetector

      public NodeDetector(EventDetectionSettings detectionSettings, EventHandler handler, Frame frame)
      Constructor with detection settings and handler.
      Parameters:
      detectionSettings - detection settings
      handler - event handler to call at event occurrences
      frame - frame in which the equator is defined (typical values are EME2000 or ITRF)
    • NodeDetector

      protected NodeDetector(NodeEventFunction nodeEventFunction, EventDetectionSettings detectionSettings, EventHandler handler)
      Protected constructor with full parameters.

      This constructor is not public as users are expected to use the builder API with the various withXxx() methods to set up the instance in a readable manner without using a huge amount of parameters.

      Parameters:
      nodeEventFunction - event function
      detectionSettings - detection settings
      handler - event handler to call at event occurrences values are EME2000 or ITRF)
      Since:
      14.0
  • Method Details

    • create

      protected NodeDetector create(EventDetectionSettings detectionSettings, EventHandler newHandler)
      Build a new instance.
      Specified by:
      create in class AbstractDetector<NodeDetector>
      Parameters:
      detectionSettings - detection settings
      newHandler - event handler to call at event occurrences
      Returns:
      a new instance of the appropriate sub-type
    • getFrame

      public Frame getFrame()
      Get the frame in which the equator is defined.
      Returns:
      the frame in which the equator is defined
    • g

      public double g(SpacecraftState s)
      Compute the value of the switching function. This function computes the Z position in the defined frame.
      Parameters:
      s - the current state information: date, kinematics, attitude
      Returns:
      value of the switching function