Package org.orekit.files.ccsds.ndm.odm.ocm

Enum Class OrbitPhysicalPropertiesKey

java.lang.Object

java.lang.Enum<OrbitPhysicalPropertiesKey>

org.orekit.files.ccsds.ndm.odm.ocm.OrbitPhysicalPropertiesKey

All Implemented Interfaces:

Serializable, Comparable<OrbitPhysicalPropertiesKey>, Constable

public enum OrbitPhysicalPropertiesKey
extends Enum<OrbitPhysicalPropertiesKey>

Keys for physical properties data entries.

Since:

11.0

Author:

Luc Maisonobe

Nested Class Summary

Nested classes/interfaces inherited from class java.lang.Enum

Enum.EnumDesc<E extends Enum<E>>

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

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 class with the specified name.
static OrbitPhysicalPropertiesKey[]	values()	Returns an array containing the constants of this enum class, in the order they are declared.

Methods inherited from class java.lang.Enum

clone, compareTo, describeConstable, equals, finalize, getDeclaringClass, hashCode, name, ordinal, toString, valueOf

Methods inherited from class java.lang.Object

getClass, notify, notifyAll, wait, wait, wait

Enum Constant Details

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 Details

values

public static OrbitPhysicalPropertiesKey[] values()

Returns an array containing the constants of this enum class, in the order they are declared.

Returns:

an array containing the constants of this enum class, in the order they are declared

valueOf

public static OrbitPhysicalPropertiesKey valueOf(String name)

Returns the enum constant of this class with the specified name. The string must match exactly an identifier used to declare an enum constant in this class. (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 class 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