Package org.orekit.files.ccsds.ndm.cdm
Enum AdditionalParametersKey
- java.lang.Object
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- java.lang.Enum<AdditionalParametersKey>
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- org.orekit.files.ccsds.ndm.cdm.AdditionalParametersKey
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- All Implemented Interfaces:
Serializable
,Comparable<AdditionalParametersKey>
public enum AdditionalParametersKey extends Enum<AdditionalParametersKey>
Keys forCDM additional parameters
entries.- Since:
- 11.2
- Author:
- Melina Vanel
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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.
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Method Summary
All Methods Static Methods Instance Methods Concrete Methods Modifier and Type Method Description boolean
process(ParseToken token, ContextBinding context, AdditionalParameters container)
Process one token.static AdditionalParametersKey
valueOf(String name)
Returns the enum constant of this type with the specified name.static AdditionalParametersKey[]
values()
Returns an array containing the constants of this enum type, in the order they are declared.
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Enum Constant Detail
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COMMENT
public static final AdditionalParametersKey COMMENT
Comment entry.
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AREA_PC
public static final AdditionalParametersKey AREA_PC
The actual area of the object.
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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.
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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.
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AREA_DRG
public static final AdditionalParametersKey AREA_DRG
The effective area of the object exposed to atmospheric drag.
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AREA_SRP
public static final AdditionalParametersKey AREA_SRP
The effective area of the object exposed to solar radiation pressure.
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OEB_PARENT_FRAME
public static final AdditionalParametersKey OEB_PARENT_FRAME
Optimally Enclosing Box parent reference frame.
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OEB_PARENT_FRAME_EPOCH
public static final AdditionalParametersKey OEB_PARENT_FRAME_EPOCH
Optimally Enclosing Box parent reference frame epoch.
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OEB_Q1
public static final AdditionalParametersKey OEB_Q1
Quaternion defining Optimally Enclosing Box (first vectorial component).
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OEB_Q2
public static final AdditionalParametersKey OEB_Q2
Quaternion defining Optimally Enclosing Box (second vectorial component).
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OEB_Q3
public static final AdditionalParametersKey OEB_Q3
Quaternion defining Optimally Enclosing Box (third vectorial component).
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OEB_QC
public static final AdditionalParametersKey OEB_QC
Quaternion defining Optimally Enclosing Box (scalar component).
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OEB_MAX
public static final AdditionalParametersKey OEB_MAX
Maximum physical dimension of Optimally Enclosing Box.
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OEB_INT
public static final AdditionalParametersKey OEB_INT
Intermediate physical dimension of Optimally Enclosing Box.
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OEB_MIN
public static final AdditionalParametersKey OEB_MIN
Minium physical dimension of Optimally Enclosing Box.
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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.
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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.
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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.
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RCS
public static final AdditionalParametersKey RCS
Typical (50th percentile) radar cross-section.
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RCS_MIN
public static final AdditionalParametersKey RCS_MIN
Minimum radar cross-section.
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RCS_MAX
public static final AdditionalParametersKey RCS_MAX
Maximum radar cross-section.
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VM_ABSOLUTE
public static final AdditionalParametersKey VM_ABSOLUTE
Typical (50th percentile) absolute visual magnitude.
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VM_APPARENT_MIN
public static final AdditionalParametersKey VM_APPARENT_MIN
Minimum apparent visual magnitude.
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VM_APPARENT
public static final AdditionalParametersKey VM_APPARENT
Typical (50th percentile) apparent visual magnitude.
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VM_APPARENT_MAX
public static final AdditionalParametersKey VM_APPARENT_MAX
Maximum apparent visual magnitude.
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REFLECTANCE
public static final AdditionalParametersKey REFLECTANCE
Typical (50th percentile) coefficient of reflectance.
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MASS
public static final AdditionalParametersKey MASS
The mass of the object.
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HBR
public static final AdditionalParametersKey HBR
Object hard body radius.
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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.
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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.
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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.
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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.
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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.
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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.
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INCLINATION
public static final AdditionalParametersKey INCLINATION
The angle between the objects orbit plane and the orbit centers equatorial plane.
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COV_CONFIDENCE
public static final AdditionalParametersKey COV_CONFIDENCE
A measure of the confidence in the covariance errors matching reality.
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COV_CONFIDENCE_METHOD
public static final AdditionalParametersKey COV_CONFIDENCE_METHOD
The method used for the calculation of COV_CONFIDENCE.
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Method Detail
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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
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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 nameNullPointerException
- if the argument is null
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process
public boolean process(ParseToken token, ContextBinding context, AdditionalParameters container)
Process one token.- Parameters:
token
- token to processcontext
- context bindingcontainer
- container to fill- Returns:
- true of token was accepted
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