Class LatitudeExtremumDetector

  • All Implemented Interfaces:
    EventDetector

    public class LatitudeExtremumDetector
    extends AbstractGeographicalDetector<LatitudeExtremumDetector>
    Detector for geographic latitude extremum.

    This detector identifies when a spacecraft reaches its extremum latitudes with respect to a central body.

    Since:
    7.1
    Author:
    Luc Maisonobe
    • Constructor Detail

      • LatitudeExtremumDetector

        public LatitudeExtremumDetector​(double maxCheck,
                                        double threshold,
                                        BodyShape body)
        Build a detector.
        Parameters:
        maxCheck - maximal checking interval (s)
        threshold - convergence threshold (s)
        body - body on which the latitude is defined
      • LatitudeExtremumDetector

        public LatitudeExtremumDetector​(LatitudeExtremumEventFunction latitudeExtremumEventFunction)
        Constructor with event function.
        Parameters:
        latitudeExtremumEventFunction - event function
        Since:
        14.0
      • LatitudeExtremumDetector

        protected LatitudeExtremumDetector​(LatitudeExtremumEventFunction latitudeExtremumEventFunction,
                                           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:
        latitudeExtremumEventFunction - event function
        detectionSettings - event detection settings
        handler - event handler to call at event occurrences
    • Method Detail

      • g

        public double g​(SpacecraftState s)
        Compute the value of the detection function.

        The value is the spacecraft latitude time derivative.

        Parameters:
        s - the current state information: date, kinematics, attitude
        Returns:
        spacecraft latitude time derivative