java.lang.Object
- java.lang.Enum<OrbitPhysicalPropertiesKey>
- - org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey

All Implemented Interfaces:

Serializable, Comparable<OrbitPhysicalPropertiesKey>
```
public enum OrbitPhysicalPropertiesKey
extends Enum<OrbitPhysicalPropertiesKey>
```
Keys for physical properties data entries.

Since:

11.0

Author:

Luc Maisonobe

Enum Constant Summary

Enum Constants
Enum Constant	Description
`AREA_ALONG_OEB_INT`	Cross-sectional area of Optimally Enclosing Box along Y-OEB.
`AREA_ALONG_OEB_MAX`	Cross-sectional area of Optimally Enclosing Box along X-OEB.
`AREA_ALONG_OEB_MIN`	Cross-sectional area of Optimally Enclosing Box along Z-OEB.
`AREA_MAX_FOR_PC`	Maximum cross-sectional area for collision probability estimation purposes.
`AREA_MIN_FOR_PC`	Minimum cross-sectional area for collision probability estimation purposes.
`AREA_TYP_FOR_PC`	Typical (50th percentile) cross-sectional area for collision probability estimation purposes.
`ATT_ACTUATOR_TYPE`	Type of actuator for attitude control.
`ATT_CONTROL`	Accuracy of attitude control.
`ATT_CONTROL_MODE`	Attitude control mode.
`ATT_KNOWLEDGE`	Accuracy of attitude knowledge.
`ATT_POINTING`	Overall accuracy of spacecraft to maintain attitude.
`AVG_MANEUVER_FREQ`	Average number of orbit or attitude maneuvers per year.
`BUS_MODEL`	Bus model name.
`COMMENT`	Comment entry.
`DOCKED_WITH`	Other space objects this object is docked to.
`DRAG_COEFF_NOM`	Nominal drag coefficient.
`DRAG_CONST_AREA`	Attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
`DRAG_UNCERTAINTY`	Drag coefficient 1σ uncertainty.
`DRY_MASS`	Mass without propellant.
`DV_BOL`	Total ΔV capability at beginning of life.
`DV_REMAINING`	Total ΔV remaining for spacecraft.
`INITIAL_WET_MASS`	Total mass at beginning of life.
`IXX`	Moment of inertia about X-axis.
`IXY`	Inertia cross product of the X and Y axes.
`IXZ`	Inertia cross product of the X and Z axes.
`IYY`	Moment of inertia about Y-axis.
`IYZ`	Inertia cross product of the Y and Z axes.
`IZZ`	Moment of inertia about Z-axis.
`MANUFACTURER`	Satellite manufacturer name.
`MAX_THRUST`	Maximum composite thrust the spacecraft can accomplish.
`OEB_INT`	Dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
`OEB_MAX`	Dimensions of Optimally Enclosing Box along X-OEB (i.e max).
`OEB_MIN`	Dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
`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).
`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.
`SOLAR_RAD_COEFF`	Nominal SRP coefficient.
`SOLAR_RAD_UNCERTAINTY`	SRP coefficient 1σ uncertainty.
`SRP_CONST_AREA`	Attitude-independent SRP area, not already into attitude-dependent area along OEB.
`VM_ABSOLUTE`	Typical (50th percentile) visual magnitude.
`VM_APPARENT`	Typical (50th percentile) apparent visual magnitude.
`VM_APPARENT_MAX`	Maximum apparent visual magnitude.
`VM_APPARENT_MIN`	Minimum apparent visual magnitude.
`WET_MASS`	Total mass at T₀.

Method Summary

All Methods Static Methods Instance Methods Concrete Methods
Modifier and Type	Method	Description
`boolean`	`process(ParseToken token, ContextBinding context, OrbitPhysicalProperties data)`	Process an token.
`static OrbitPhysicalPropertiesKey`	`valueOf(String name)`	Returns the enum constant of this type with the specified name.
`static OrbitPhysicalPropertiesKey[]`	`values()`	Returns an array containing the constants of this enum type, in the order they are declared.

Methods inherited from class java.lang.Enum
clone, compareTo, equals, finalize, getDeclaringClass, hashCode, name, ordinal, toString, valueOf

Methods inherited from class java.lang.Object
getClass, notify, notifyAll, wait, wait, wait

- Enum Constant Detail
  - COMMENT
```
public static final OrbitPhysicalPropertiesKey COMMENT
```
    Comment entry.
  - MANUFACTURER
```
public static final OrbitPhysicalPropertiesKey MANUFACTURER
```
    Satellite manufacturer name.
  - BUS_MODEL
```
public static final OrbitPhysicalPropertiesKey BUS_MODEL
```
    Bus model name.
  - DOCKED_WITH
```
public static final OrbitPhysicalPropertiesKey DOCKED_WITH
```
    Other space objects this object is docked to.
  - DRAG_CONST_AREA
```
public static final OrbitPhysicalPropertiesKey DRAG_CONST_AREA
```
    Attitude-independent drag cross-sectional area, not already into attitude-dependent area along OEB.
  - DRAG_COEFF_NOM
```
public static final OrbitPhysicalPropertiesKey DRAG_COEFF_NOM
```
    Nominal drag coefficient.
  - DRAG_UNCERTAINTY
```
public static final OrbitPhysicalPropertiesKey DRAG_UNCERTAINTY
```
    Drag coefficient 1σ uncertainty.
  - INITIAL_WET_MASS
```
public static final OrbitPhysicalPropertiesKey INITIAL_WET_MASS
```
    Total mass at beginning of life.
  - WET_MASS
```
public static final OrbitPhysicalPropertiesKey WET_MASS
```
    Total mass at T₀.
  - DRY_MASS
```
public static final OrbitPhysicalPropertiesKey DRY_MASS
```
    Mass without propellant.
  - OEB_PARENT_FRAME
```
public static final OrbitPhysicalPropertiesKey OEB_PARENT_FRAME
```
    Optimally Enclosing Box parent reference frame.
  - OEB_PARENT_FRAME_EPOCH
```
public static final OrbitPhysicalPropertiesKey OEB_PARENT_FRAME_EPOCH
```
    Optimally Enclosing Box parent reference frame epoch.
  - OEB_Q1
```
public static final OrbitPhysicalPropertiesKey OEB_Q1
```
    Quaternion defining Optimally Enclosing Box (first vectorial component).
  - OEB_Q2
```
public static final OrbitPhysicalPropertiesKey OEB_Q2
```
    Quaternion defining Optimally Enclosing Box (second vectorial component).
  - OEB_Q3
```
public static final OrbitPhysicalPropertiesKey OEB_Q3
```
    Quaternion defining Optimally Enclosing Box (third vectorial component).
  - OEB_QC
```
public static final OrbitPhysicalPropertiesKey OEB_QC
```
    Quaternion defining Optimally Enclosing Box (scalar component).
  - OEB_MAX
```
public static final OrbitPhysicalPropertiesKey OEB_MAX
```
    Dimensions of Optimally Enclosing Box along X-OEB (i.e max).
  - OEB_INT
```
public static final OrbitPhysicalPropertiesKey OEB_INT
```
    Dimensions of Optimally Enclosing Box along Y-OEB (i.e intermediate).
  - OEB_MIN
```
public static final OrbitPhysicalPropertiesKey OEB_MIN
```
    Dimensions of Optimally Enclosing Box along Z-OEB (i.e min).
  - AREA_ALONG_OEB_MAX
```
public static final OrbitPhysicalPropertiesKey AREA_ALONG_OEB_MAX
```
    Cross-sectional area of Optimally Enclosing Box along X-OEB.
  - AREA_ALONG_OEB_INT
```
public static final OrbitPhysicalPropertiesKey AREA_ALONG_OEB_INT
```
    Cross-sectional area of Optimally Enclosing Box along Y-OEB.
  - AREA_ALONG_OEB_MIN
```
public static final OrbitPhysicalPropertiesKey AREA_ALONG_OEB_MIN
```
    Cross-sectional area of Optimally Enclosing Box along Z-OEB.
  - AREA_MIN_FOR_PC
```
public static final OrbitPhysicalPropertiesKey AREA_MIN_FOR_PC
```
    Minimum cross-sectional area for collision probability estimation purposes.
  - AREA_MAX_FOR_PC
```
public static final OrbitPhysicalPropertiesKey AREA_MAX_FOR_PC
```
    Maximum cross-sectional area for collision probability estimation purposes.
  - AREA_TYP_FOR_PC
```
public static final OrbitPhysicalPropertiesKey AREA_TYP_FOR_PC
```
    Typical (50th percentile) cross-sectional area for collision probability estimation purposes.
  - RCS
```
public static final OrbitPhysicalPropertiesKey RCS
```
    Typical (50th percentile) radar cross-section.
  - RCS_MIN
```
public static final OrbitPhysicalPropertiesKey RCS_MIN
```
    Minimum radar cross-section.
  - RCS_MAX
```
public static final OrbitPhysicalPropertiesKey RCS_MAX
```
    Maximum radar cross-section.
  - SRP_CONST_AREA
```
public static final OrbitPhysicalPropertiesKey SRP_CONST_AREA
```
    Attitude-independent SRP area, not already into attitude-dependent area along OEB.
  - SOLAR_RAD_COEFF
```
public static final OrbitPhysicalPropertiesKey SOLAR_RAD_COEFF
```
    Nominal SRP coefficient.
  - SOLAR_RAD_UNCERTAINTY
```
public static final OrbitPhysicalPropertiesKey SOLAR_RAD_UNCERTAINTY
```
    SRP coefficient 1σ uncertainty.
  - VM_ABSOLUTE
```
public static final OrbitPhysicalPropertiesKey VM_ABSOLUTE
```
    Typical (50th percentile) visual magnitude.
  - VM_APPARENT_MIN
```
public static final OrbitPhysicalPropertiesKey VM_APPARENT_MIN
```
    Minimum apparent visual magnitude.
  - VM_APPARENT
```
public static final OrbitPhysicalPropertiesKey VM_APPARENT
```
    Typical (50th percentile) apparent visual magnitude.
  - VM_APPARENT_MAX
```
public static final OrbitPhysicalPropertiesKey VM_APPARENT_MAX
```
    Maximum apparent visual magnitude.
  - REFLECTANCE
```
public static final OrbitPhysicalPropertiesKey REFLECTANCE
```
    Typical (50th percentile) coefficient of reflectance.
  - ATT_CONTROL_MODE
```
public static final OrbitPhysicalPropertiesKey ATT_CONTROL_MODE
```
    Attitude control mode.
  - ATT_ACTUATOR_TYPE
```
public static final OrbitPhysicalPropertiesKey ATT_ACTUATOR_TYPE
```
    Type of actuator for attitude control.
  - ATT_KNOWLEDGE
```
public static final OrbitPhysicalPropertiesKey ATT_KNOWLEDGE
```
    Accuracy of attitude knowledge.
  - ATT_CONTROL
```
public static final OrbitPhysicalPropertiesKey ATT_CONTROL
```
    Accuracy of attitude control.
  - ATT_POINTING
```
public static final OrbitPhysicalPropertiesKey ATT_POINTING
```
    Overall accuracy of spacecraft to maintain attitude.
  - AVG_MANEUVER_FREQ
```
public static final OrbitPhysicalPropertiesKey AVG_MANEUVER_FREQ
```
    Average number of orbit or attitude maneuvers per year.
  - MAX_THRUST
```
public static final OrbitPhysicalPropertiesKey MAX_THRUST
```
    Maximum composite thrust the spacecraft can accomplish.
  - DV_BOL
```
public static final OrbitPhysicalPropertiesKey DV_BOL
```
    Total ΔV capability at beginning of life.
  - DV_REMAINING
```
public static final OrbitPhysicalPropertiesKey DV_REMAINING
```
    Total ΔV remaining for spacecraft.
  - IXX
```
public static final OrbitPhysicalPropertiesKey IXX
```
    Moment of inertia about X-axis.
  - IYY
```
public static final OrbitPhysicalPropertiesKey IYY
```
    Moment of inertia about Y-axis.
  - IZZ
```
public static final OrbitPhysicalPropertiesKey IZZ
```
    Moment of inertia about Z-axis.
  - IXY
```
public static final OrbitPhysicalPropertiesKey IXY
```
    Inertia cross product of the X and Y axes.
  - IXZ
```
public static final OrbitPhysicalPropertiesKey IXZ
```
    Inertia cross product of the X and Z axes.
  - IYZ
```
public static final OrbitPhysicalPropertiesKey IYZ
```
    Inertia cross product of the Y and Z axes.
- Method Detail
  - values
```
public static OrbitPhysicalPropertiesKey[] 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 (OrbitPhysicalPropertiesKey c : OrbitPhysicalPropertiesKey.values()) System.out.println(c);
    Returns:
    
    an array containing the constants of this enum type, in the order they are declared
  - valueOf
```
public static OrbitPhysicalPropertiesKey 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,
                       OrbitPhysicalProperties data)
```
    Process an token.
    
    Parameters:
    
    token - token to process
    
    context - context binding
    
    data - data to fill
    
    Returns:
    
    true of token was accepted

Enum OrbitPhysicalPropertiesKey

Enum Constant Summary

Method Summary

Methods inherited from class java.lang.Enum

Methods inherited from class java.lang.Object

Enum Constant Detail

COMMENT

MANUFACTURER

BUS_MODEL

DOCKED_WITH

DRAG_CONST_AREA

DRAG_COEFF_NOM

DRAG_UNCERTAINTY

INITIAL_WET_MASS

WET_MASS

DRY_MASS

OEB_PARENT_FRAME

OEB_PARENT_FRAME_EPOCH

OEB_Q1

OEB_Q2

OEB_Q3

OEB_QC

OEB_MAX

OEB_INT

OEB_MIN

AREA_ALONG_OEB_MAX

AREA_ALONG_OEB_INT

AREA_ALONG_OEB_MIN

AREA_MIN_FOR_PC

AREA_MAX_FOR_PC

AREA_TYP_FOR_PC

RCS

RCS_MIN

RCS_MAX

SRP_CONST_AREA

SOLAR_RAD_COEFF

SOLAR_RAD_UNCERTAINTY

VM_ABSOLUTE

VM_APPARENT_MIN

VM_APPARENT

VM_APPARENT_MAX

REFLECTANCE

ATT_CONTROL_MODE

ATT_ACTUATOR_TYPE

ATT_KNOWLEDGE

ATT_CONTROL

ATT_POINTING

AVG_MANEUVER_FREQ

MAX_THRUST

DV_BOL

DV_REMAINING

IXX

IYY

IZZ

IXY

IXZ

IYZ

Method Detail

values

valueOf

process