Enum AdditionalParametersKey

    • Enum Constant Summary

      Enum Constants 
      Enum Constant Description
      APOAPSIS_ALTITUDE
      The distance of the furthest point in the objects orbit above the equatorial radius of the central body.
      AREA_ALONG_OEB_INT
      Cross-sectional area of Optimally Enclosing Box when viewed along the intermediate OEB direction.
      AREA_ALONG_OEB_MAX
      Cross-sectional area of Optimally Enclosing Box when viewed along the maximum OEB direction.
      AREA_ALONG_OEB_MIN
      Cross-sectional area of Optimally Enclosing Box when viewed along the minimum OEB direction.
      AREA_DRG
      The effective area of the object exposed to atmospheric drag.
      AREA_PC
      The actual area of the object.
      AREA_PC_MAX
      Maximum area (or cross-section) of the object to be used in the calculation of the probability of collision.
      AREA_PC_MIN
      Minimum area (or cross-section) of the object to be used in the calculation of the probability of collision.
      AREA_SRP
      The effective area of the object exposed to solar radiation pressure.
      CD_AREA_OVER_MASS
      The object’s Cd x A/m used to propagate the state vector and covariance to TCA.
      COMMENT
      Comment entry.
      COV_CONFIDENCE
      A measure of the confidence in the covariance errors matching reality.
      COV_CONFIDENCE_METHOD
      The method used for the calculation of COV_CONFIDENCE.
      CR_AREA_OVER_MASS
      The object’s Cr x A/m used to propagate the state vector and covariance to TCA.
      HBR
      Object hard body radius.
      INCLINATION
      The angle between the objects orbit plane and the orbit centers equatorial plane.
      MASS
      The mass of the object.
      OEB_INT
      Intermediate physical dimension of Optimally Enclosing Box.
      OEB_MAX
      Maximum physical dimension of Optimally Enclosing Box.
      OEB_MIN
      Minium physical dimension of Optimally Enclosing Box.
      OEB_PARENT_FRAME
      Optimally Enclosing Box parent reference frame.
      OEB_PARENT_FRAME_EPOCH
      Optimally Enclosing Box parent reference frame epoch.
      OEB_Q1
      Quaternion defining Optimally Enclosing Box (first vectorial component).
      OEB_Q2
      Quaternion defining Optimally Enclosing Box (second vectorial component).
      OEB_Q3
      Quaternion defining Optimally Enclosing Box (third vectorial component).
      OEB_QC
      Quaternion defining Optimally Enclosing Box (scalar component).
      PERIAPSIS_ALTITUDE
      The distance of the closest point in the objects orbit above the equatorial radius of the central body.
      RCS
      Typical (50th percentile) radar cross-section.
      RCS_MAX
      Maximum radar cross-section.
      RCS_MIN
      Minimum radar cross-section.
      REFLECTANCE
      Typical (50th percentile) coefficient of reflectance.
      SEDR
      The amount of energy being removed from the object’s orbit by atmospheric drag.
      THRUST_ACCELERATION
      The object’s acceleration due to in-track thrust used to propagate the state vector and covariance to TCA.
      VM_ABSOLUTE
      Typical (50th percentile) absolute visual magnitude.
      VM_APPARENT
      Typical (50th percentile) apparent visual magnitude.
      VM_APPARENT_MAX
      Maximum apparent visual magnitude.
      VM_APPARENT_MIN
      Minimum apparent visual magnitude.
    • Enum Constant Detail

      • AREA_PC_MIN

        public static final AdditionalParametersKey AREA_PC_MIN
        Minimum area (or cross-section) of the object to be used in the calculation of the probability of collision.
      • AREA_PC_MAX

        public static final AdditionalParametersKey AREA_PC_MAX
        Maximum area (or cross-section) of the object to be used in the calculation of the probability of collision.
      • AREA_DRG

        public static final AdditionalParametersKey AREA_DRG
        The effective area of the object exposed to atmospheric drag.
      • AREA_SRP

        public static final AdditionalParametersKey AREA_SRP
        The effective area of the object exposed to solar radiation pressure.
      • OEB_PARENT_FRAME

        public static final AdditionalParametersKey OEB_PARENT_FRAME
        Optimally Enclosing Box parent reference frame.
      • OEB_PARENT_FRAME_EPOCH

        public static final AdditionalParametersKey OEB_PARENT_FRAME_EPOCH
        Optimally Enclosing Box parent reference frame epoch.
      • OEB_Q1

        public static final AdditionalParametersKey OEB_Q1
        Quaternion defining Optimally Enclosing Box (first vectorial component).
      • OEB_Q2

        public static final AdditionalParametersKey OEB_Q2
        Quaternion defining Optimally Enclosing Box (second vectorial component).
      • OEB_Q3

        public static final AdditionalParametersKey OEB_Q3
        Quaternion defining Optimally Enclosing Box (third vectorial component).
      • OEB_QC

        public static final AdditionalParametersKey OEB_QC
        Quaternion defining Optimally Enclosing Box (scalar component).
      • OEB_MAX

        public static final AdditionalParametersKey OEB_MAX
        Maximum physical dimension of Optimally Enclosing Box.
      • OEB_INT

        public static final AdditionalParametersKey OEB_INT
        Intermediate physical dimension of Optimally Enclosing Box.
      • OEB_MIN

        public static final AdditionalParametersKey OEB_MIN
        Minium physical dimension of Optimally Enclosing Box.
      • AREA_ALONG_OEB_MAX

        public static final AdditionalParametersKey AREA_ALONG_OEB_MAX
        Cross-sectional area of Optimally Enclosing Box when viewed along the maximum OEB direction.
      • AREA_ALONG_OEB_INT

        public static final AdditionalParametersKey AREA_ALONG_OEB_INT
        Cross-sectional area of Optimally Enclosing Box when viewed along the intermediate OEB direction.
      • AREA_ALONG_OEB_MIN

        public static final AdditionalParametersKey AREA_ALONG_OEB_MIN
        Cross-sectional area of Optimally Enclosing Box when viewed along the minimum OEB direction.
      • VM_ABSOLUTE

        public static final AdditionalParametersKey VM_ABSOLUTE
        Typical (50th percentile) absolute visual magnitude.
      • VM_APPARENT

        public static final AdditionalParametersKey VM_APPARENT
        Typical (50th percentile) apparent visual magnitude.
      • REFLECTANCE

        public static final AdditionalParametersKey REFLECTANCE
        Typical (50th percentile) coefficient of reflectance.
      • CD_AREA_OVER_MASS

        public static final AdditionalParametersKey CD_AREA_OVER_MASS
        The object’s Cd x A/m used to propagate the state vector and covariance to TCA.
      • CR_AREA_OVER_MASS

        public static final AdditionalParametersKey CR_AREA_OVER_MASS
        The object’s Cr x A/m used to propagate the state vector and covariance to TCA.
      • THRUST_ACCELERATION

        public static final AdditionalParametersKey THRUST_ACCELERATION
        The object’s acceleration due to in-track thrust used to propagate the state vector and covariance to TCA.
      • SEDR

        public static final AdditionalParametersKey SEDR
        The amount of energy being removed from the object’s orbit by atmospheric drag. This value is an average calculated during the OD.
      • APOAPSIS_ALTITUDE

        public static final AdditionalParametersKey APOAPSIS_ALTITUDE
        The distance of the furthest point in the objects orbit above the equatorial radius of the central body.
      • PERIAPSIS_ALTITUDE

        public static final AdditionalParametersKey PERIAPSIS_ALTITUDE
        The distance of the closest point in the objects orbit above the equatorial radius of the central body.
      • INCLINATION

        public static final AdditionalParametersKey INCLINATION
        The angle between the objects orbit plane and the orbit centers equatorial plane.
      • COV_CONFIDENCE

        public static final AdditionalParametersKey COV_CONFIDENCE
        A measure of the confidence in the covariance errors matching reality.
      • COV_CONFIDENCE_METHOD

        public static final AdditionalParametersKey COV_CONFIDENCE_METHOD
        The method used for the calculation of COV_CONFIDENCE.
    • Method Detail

      • values

        public static AdditionalParametersKey[] values()
        Returns an array containing the constants of this enum type, in the order they are declared. This method may be used to iterate over the constants as follows:
        for (AdditionalParametersKey c : AdditionalParametersKey.values())
            System.out.println(c);
        
        Returns:
        an array containing the constants of this enum type, in the order they are declared
      • valueOf

        public static AdditionalParametersKey valueOf​(String name)
        Returns the enum constant of this type with the specified name. The string must match exactly an identifier used to declare an enum constant in this type. (Extraneous whitespace characters are not permitted.)
        Parameters:
        name - the name of the enum constant to be returned.
        Returns:
        the enum constant with the specified name
        Throws:
        IllegalArgumentException - if this enum type has no constant with the specified name
        NullPointerException - if the argument is null
      • process

        public boolean process​(ParseToken token,
                               ContextBinding context,
                               AdditionalParameters container)
        Process one token.
        Parameters:
        token - token to process
        context - context binding
        container - container to fill
        Returns:
        true of token was accepted