fr.cnes.genius.vts

Enum AbstractVTSWriter.ColumnId

java.lang.Object

java.lang.Enum<AbstractVTSWriter.ColumnId>

fr.cnes.genius.vts.AbstractVTSWriter.ColumnId

All Implemented Interfaces:

Serializable, Comparable<AbstractVTSWriter.ColumnId>

Enclosing class:

AbstractVTSWriter

public static enum AbstractVTSWriter.ColumnId
extends Enum<AbstractVTSWriter.ColumnId>

Column identifiers.

Author:

fjammet

Enum Constant Summary

Enum Constants

Enum Constant and Description
A Semi-major axis.
ACCA Aerodynamic acceleration.
ACCAX X component of the aerodynamic acceleration.
ACCAY Y component of the aerodynamic acceleration.
ACCAZ Z component of the aerodynamic acceleration.
ACCM Moon acceleration.
ACCMX X component of the moon acceleration.
ACCMY Y component of the moon acceleration.
ACCMZ Z component of the moon acceleration.
ACCN Newtonian acceleration in propagation frame.
ACCNX X component of the newtonian acceleration.
ACCNY Y component of the newtonian acceleration.
ACCNZ Z component of the newtonian acceleration.
ACCP Earth potential acceleration.
ACCPX X component of the earth potential acceleration.
ACCPY Y component of the earth potential acceleration.
ACCPZ Z component of the earth potential acceleration.
ACCR Solar radiation pressure acceleration.
ACCRX X component of the solar radiation pressure acceleration.
ACCRY Y component of the solar radiation pressure acceleration.
ACCRZ Z component of the solar radiation pressure acceleration.
ACCS Sun acceleration.
ACCSX X component of the sun acceleration.
ACCSY Y component of the moon acceleration.
ACCSZ Z component of the moon acceleration.
ACCT Thrust acceleration.
ACCTX X component of the solar radiation pressure acceleration.
ACCTY Y component of the solar radiation pressure acceleration.
ACCTZ Z component of the solar radiation pressure acceleration.
ALTG Geodetic altitude.
ALTS Geocentric altitude.
AM Mean (Secular Lyddane model) semi-major axis.
AOA Angle of attack.
AOP Perigee argument.
AOPM Mean (Secular Lyddane model) argument of perigee.
AP Geomagnetic index.
APO Apoapsis.
APOALT Apoapsis.
AZIA Velocity elevation in ITRF.
AZIR Velocity azimut in rotating frame.
BANK Roll velocity.
BETA Sideslip.
CX Drag coefficient.
CZ Lift coefficient.
DATE Date.
E Eccentricity.
EA Eccentric anomaly.
EAOL Eccentric latitude argument.
EM Mean (Secular Lyddane model) eccentricity.
EUL0 EUL0
EUL1 EUL1
EUL2 EUL2
EVENT EVENT
EVENT_INFO_FIELD_0 EVENT_INFO_FIELD_0
EVENT_INFO_FIELD_1 EVENT_INFO_FIELD_1
EVENT_INFO_FIELD_2 EVENT_INFO_FIELD_2
EVENT_INFO_FIELD_3 EVENT_INFO_FIELD_3
EVENT_INFO_FIELD_4 EVENT_INFO_FIELD_4
EX First component of the circular eccentricity vector.
EXM First component of the eccentricity vector.
EY Second component of the circular eccentricity vector.
EYM Second component of eccentricity vector.
F107 Solar flux.
FPAA Velocity elevation in ITRF.
FPAR Velocity elevation in rotating frame.
HX First component of the inclination vector.
HY Second component of the inclination vector.
I Inclination.
IM Mean (Secular Lyddane model) inclination.
LATG Geodetic latitude.
LATS Geocentric latitude.
LON Geodetic longitude.
LSPAN Percentage of the illuminated surface of the solar panels.
LSSAT Percentage of the illuminated surface of the spacecraft.
MA Mean anomaly.
MACH Mach number.
MAM Mean (Secular Lyddane model) mean anomaly.
MAOL Mean latitude argument.
MLT Mean local time in TIRF.
PERI Periapsis.
PERIALT Periapsis.
PHI Third elementary rotation in inertial frame.
PHIL Third elementary rotation in local frame.
PITCH Pitch in aircraft frame.
PMASS Propellant mass.
POSIN Position norm in inertial frame.
PSI First elementary rotation in inertial frame.
PSIL First elementary rotation in local frame.
Q0 First quaternion component.
Q1 Second quaternion component.
Q2 Thrid quaternion component.
Q3 Fourth quaternion component.
RAAN Argument of the ascending node.
RAANM Mean (Secular Lyddane model) right ascension of the ascending node.
RHO Atmospheric density.
ROLL Roll in aircraft frame.
SPIN Spin rate.
TA True anomaly.
TAOL True latitude argument.
THETA Second elementary rotation in inertial frame.
THETAL Second elementary rotation in local frame.
THRUST Thrust.
TIME Duration.
TLT True local time in TIRF.
TMASS Total mass.
USED_DV Thrust.
VIN Velocity norm in inertial frame.
VREL Relative velocity in rotating frame.
VTS_DATE Date for VTS files in EME2000.
VTS_PHI Third elementary rotation in EME2000 frame.
VTS_PSI First elementary rotation in EME2000 frame.
VTS_THETA Second elementary rotation in EME2000 frame.
VTS_VXIN Inertial EME2000 x velocity coordinate.
VTS_VYIN Inertial EME2000 y velocity coordinate.
VTS_VZIN Inertial EME2000 y velocity coordinate.
VTS_XIN Inertial EME2000 x position coordinate.
VTS_YIN Inertial EME2000 y position coordinate.
VTS_ZIN Inertial EME2000 z position coordinate.
VX VX
VXIN Velocity in inertial x coordinates.
VXREL X component of the relative velocity in rotating frame.
VY VY
VYIN Velocity in inertial y coordinates.
VYREL Y component of the relative velocity in rotating frame.
VZ VZ
VZIN Velocity in inertial z coordinates.
VZREL Z component of the relative velocity in rotating frame.
X X
XIN Inertial x coordinates.
XREL X component of the relative position in rotating frame.
XSPIN Spin rate about x satellite axis.
Y Y
YAW Yaw in aircraft frame.
YIN Inertial y coordinates.
YREL Y component of the relative position in rotating frame.
YSPIN Spin rate about y satellite axis.
Z Z
ZIN Inertial z coordinates.
ZREL Z component of the relative position in rotating frame.
ZSPIN Spin rate about z satellite axis.

Method Summary

Modifier and Type	Method and Description
static AbstractVTSWriter.ColumnId	valueOf(String name) Returns the enum constant of this type with the specified name.
static AbstractVTSWriter.ColumnId[]	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

X

public static final AbstractVTSWriter.ColumnId X

X

Y

public static final AbstractVTSWriter.ColumnId Y

Y

Z

public static final AbstractVTSWriter.ColumnId Z

Z

VX

public static final AbstractVTSWriter.ColumnId VX

VX

VY

public static final AbstractVTSWriter.ColumnId VY

VY

VZ

public static final AbstractVTSWriter.ColumnId VZ

VZ

EUL0

public static final AbstractVTSWriter.ColumnId EUL0

EUL0

EUL1

public static final AbstractVTSWriter.ColumnId EUL1

EUL1

EUL2

public static final AbstractVTSWriter.ColumnId EUL2

EUL2

EVENT

public static final AbstractVTSWriter.ColumnId EVENT

EVENT

EVENT_INFO_FIELD_0

public static final AbstractVTSWriter.ColumnId EVENT_INFO_FIELD_0

EVENT_INFO_FIELD_0

EVENT_INFO_FIELD_1

public static final AbstractVTSWriter.ColumnId EVENT_INFO_FIELD_1

EVENT_INFO_FIELD_1

EVENT_INFO_FIELD_2

public static final AbstractVTSWriter.ColumnId EVENT_INFO_FIELD_2

EVENT_INFO_FIELD_2

EVENT_INFO_FIELD_3

public static final AbstractVTSWriter.ColumnId EVENT_INFO_FIELD_3

EVENT_INFO_FIELD_3

EVENT_INFO_FIELD_4

public static final AbstractVTSWriter.ColumnId EVENT_INFO_FIELD_4

EVENT_INFO_FIELD_4

DATE

public static final AbstractVTSWriter.ColumnId DATE

Date.

TIME

public static final AbstractVTSWriter.ColumnId TIME

Duration.

TMASS

public static final AbstractVTSWriter.ColumnId TMASS

Total mass.

PMASS

public static final AbstractVTSWriter.ColumnId PMASS

Propellant mass.

XIN

public static final AbstractVTSWriter.ColumnId XIN

Inertial x coordinates.

YIN

public static final AbstractVTSWriter.ColumnId YIN

Inertial y coordinates.

ZIN

public static final AbstractVTSWriter.ColumnId ZIN

Inertial z coordinates.

VXIN

public static final AbstractVTSWriter.ColumnId VXIN

Velocity in inertial x coordinates.

VYIN

public static final AbstractVTSWriter.ColumnId VYIN

Velocity in inertial y coordinates.

VZIN

public static final AbstractVTSWriter.ColumnId VZIN

Velocity in inertial z coordinates.

POSIN

public static final AbstractVTSWriter.ColumnId POSIN

Position norm in inertial frame.

VIN

public static final AbstractVTSWriter.ColumnId VIN

Velocity norm in inertial frame.

XREL

public static final AbstractVTSWriter.ColumnId XREL

X component of the relative position in rotating frame.

YREL

public static final AbstractVTSWriter.ColumnId YREL

Y component of the relative position in rotating frame.

ZREL

public static final AbstractVTSWriter.ColumnId ZREL

Z component of the relative position in rotating frame.

VXREL

public static final AbstractVTSWriter.ColumnId VXREL

X component of the relative velocity in rotating frame.

VYREL

public static final AbstractVTSWriter.ColumnId VYREL

Y component of the relative velocity in rotating frame.

VZREL

public static final AbstractVTSWriter.ColumnId VZREL

Z component of the relative velocity in rotating frame.

VREL

public static final AbstractVTSWriter.ColumnId VREL

Relative velocity in rotating frame.

A

public static final AbstractVTSWriter.ColumnId A

Semi-major axis.

E

public static final AbstractVTSWriter.ColumnId E

Eccentricity.

I

public static final AbstractVTSWriter.ColumnId I

Inclination.

AOP

public static final AbstractVTSWriter.ColumnId AOP

Perigee argument.

RAAN

public static final AbstractVTSWriter.ColumnId RAAN

Argument of the ascending node.

TA

public static final AbstractVTSWriter.ColumnId TA

True anomaly.

MA

public static final AbstractVTSWriter.ColumnId MA

Mean anomaly.

EA

public static final AbstractVTSWriter.ColumnId EA

Eccentric anomaly.

EX

public static final AbstractVTSWriter.ColumnId EX

First component of the circular eccentricity vector.

EY

public static final AbstractVTSWriter.ColumnId EY

Second component of the circular eccentricity vector.

HX

public static final AbstractVTSWriter.ColumnId HX

First component of the inclination vector.

HY

public static final AbstractVTSWriter.ColumnId HY

Second component of the inclination vector.

TAOL

public static final AbstractVTSWriter.ColumnId TAOL

True latitude argument.

MAOL

public static final AbstractVTSWriter.ColumnId MAOL

Mean latitude argument.

EAOL

public static final AbstractVTSWriter.ColumnId EAOL

Eccentric latitude argument.

PERI

public static final AbstractVTSWriter.ColumnId PERI

Periapsis.

APO

public static final AbstractVTSWriter.ColumnId APO

Apoapsis.

PERIALT

public static final AbstractVTSWriter.ColumnId PERIALT

Periapsis.

APOALT

public static final AbstractVTSWriter.ColumnId APOALT

Apoapsis.

LATG

public static final AbstractVTSWriter.ColumnId LATG

Geodetic latitude.

LON

public static final AbstractVTSWriter.ColumnId LON

Geodetic longitude.

ALTG

public static final AbstractVTSWriter.ColumnId ALTG

Geodetic altitude.

LATS

public static final AbstractVTSWriter.ColumnId LATS

Geocentric latitude.

ALTS

public static final AbstractVTSWriter.ColumnId ALTS

Geocentric altitude.

AZIA

public static final AbstractVTSWriter.ColumnId AZIA

Velocity elevation in ITRF.

FPAA

public static final AbstractVTSWriter.ColumnId FPAA

Velocity elevation in ITRF.

AZIR

public static final AbstractVTSWriter.ColumnId AZIR

Velocity azimut in rotating frame.

FPAR

public static final AbstractVTSWriter.ColumnId FPAR

Velocity elevation in rotating frame.

PSI

public static final AbstractVTSWriter.ColumnId PSI

First elementary rotation in inertial frame.

THETA

public static final AbstractVTSWriter.ColumnId THETA

Second elementary rotation in inertial frame.

PHI

public static final AbstractVTSWriter.ColumnId PHI

Third elementary rotation in inertial frame.

PSIL

public static final AbstractVTSWriter.ColumnId PSIL

First elementary rotation in local frame.

THETAL

public static final AbstractVTSWriter.ColumnId THETAL

Second elementary rotation in local frame.

PHIL

public static final AbstractVTSWriter.ColumnId PHIL

Third elementary rotation in local frame.

Q0

public static final AbstractVTSWriter.ColumnId Q0

First quaternion component.

Q1

public static final AbstractVTSWriter.ColumnId Q1

Second quaternion component.

Q2

public static final AbstractVTSWriter.ColumnId Q2

Thrid quaternion component.

Q3

public static final AbstractVTSWriter.ColumnId Q3

Fourth quaternion component.

AOA

public static final AbstractVTSWriter.ColumnId AOA

Angle of attack.

BETA

public static final AbstractVTSWriter.ColumnId BETA

Sideslip.

BANK

public static final AbstractVTSWriter.ColumnId BANK

Roll velocity.

YAW

public static final AbstractVTSWriter.ColumnId YAW

Yaw in aircraft frame.

PITCH

public static final AbstractVTSWriter.ColumnId PITCH

Pitch in aircraft frame.

ROLL

public static final AbstractVTSWriter.ColumnId ROLL

Roll in aircraft frame.

SPIN

public static final AbstractVTSWriter.ColumnId SPIN

Spin rate.

XSPIN

public static final AbstractVTSWriter.ColumnId XSPIN

Spin rate about x satellite axis.

YSPIN

public static final AbstractVTSWriter.ColumnId YSPIN

Spin rate about y satellite axis.

ZSPIN

public static final AbstractVTSWriter.ColumnId ZSPIN

Spin rate about z satellite axis.

ACCN

public static final AbstractVTSWriter.ColumnId ACCN

Newtonian acceleration in propagation frame.

ACCNX

public static final AbstractVTSWriter.ColumnId ACCNX

X component of the newtonian acceleration.

ACCNY

public static final AbstractVTSWriter.ColumnId ACCNY

Y component of the newtonian acceleration.

ACCNZ

public static final AbstractVTSWriter.ColumnId ACCNZ

Z component of the newtonian acceleration.

ACCP

public static final AbstractVTSWriter.ColumnId ACCP

Earth potential acceleration.

ACCPX

public static final AbstractVTSWriter.ColumnId ACCPX

X component of the earth potential acceleration.

ACCPY

public static final AbstractVTSWriter.ColumnId ACCPY

Y component of the earth potential acceleration.

ACCPZ

public static final AbstractVTSWriter.ColumnId ACCPZ

Z component of the earth potential acceleration.

ACCM

public static final AbstractVTSWriter.ColumnId ACCM

Moon acceleration.

ACCMX

public static final AbstractVTSWriter.ColumnId ACCMX

X component of the moon acceleration.

ACCMY

public static final AbstractVTSWriter.ColumnId ACCMY

Y component of the moon acceleration.

ACCMZ

public static final AbstractVTSWriter.ColumnId ACCMZ

Z component of the moon acceleration.

ACCS

public static final AbstractVTSWriter.ColumnId ACCS

Sun acceleration.

ACCSX

public static final AbstractVTSWriter.ColumnId ACCSX

X component of the sun acceleration.

ACCSY

public static final AbstractVTSWriter.ColumnId ACCSY

Y component of the moon acceleration.

ACCSZ

public static final AbstractVTSWriter.ColumnId ACCSZ

Z component of the moon acceleration.

ACCA

public static final AbstractVTSWriter.ColumnId ACCA

Aerodynamic acceleration.

ACCAX

public static final AbstractVTSWriter.ColumnId ACCAX

X component of the aerodynamic acceleration.

ACCAY

public static final AbstractVTSWriter.ColumnId ACCAY

Y component of the aerodynamic acceleration.

ACCAZ

public static final AbstractVTSWriter.ColumnId ACCAZ

Z component of the aerodynamic acceleration.

ACCR

public static final AbstractVTSWriter.ColumnId ACCR

Solar radiation pressure acceleration.

ACCRX

public static final AbstractVTSWriter.ColumnId ACCRX

X component of the solar radiation pressure acceleration.

ACCRY

public static final AbstractVTSWriter.ColumnId ACCRY

Y component of the solar radiation pressure acceleration.

ACCRZ

public static final AbstractVTSWriter.ColumnId ACCRZ

Z component of the solar radiation pressure acceleration.

ACCT

public static final AbstractVTSWriter.ColumnId ACCT

Thrust acceleration.

ACCTX

public static final AbstractVTSWriter.ColumnId ACCTX

X component of the solar radiation pressure acceleration.

ACCTY

public static final AbstractVTSWriter.ColumnId ACCTY

Y component of the solar radiation pressure acceleration.

ACCTZ

public static final AbstractVTSWriter.ColumnId ACCTZ

Z component of the solar radiation pressure acceleration.

THRUST

public static final AbstractVTSWriter.ColumnId THRUST

Thrust.

USED_DV

public static final AbstractVTSWriter.ColumnId USED_DV

Thrust.

RHO

public static final AbstractVTSWriter.ColumnId RHO

Atmospheric density.

CX

public static final AbstractVTSWriter.ColumnId CX

Drag coefficient.

CZ

public static final AbstractVTSWriter.ColumnId CZ

Lift coefficient.

MACH

public static final AbstractVTSWriter.ColumnId MACH

Mach number.

MLT

public static final AbstractVTSWriter.ColumnId MLT

Mean local time in TIRF.

TLT

public static final AbstractVTSWriter.ColumnId TLT

True local time in TIRF.

VTS_DATE

public static final AbstractVTSWriter.ColumnId VTS_DATE

Date for VTS files in EME2000.

VTS_XIN

public static final AbstractVTSWriter.ColumnId VTS_XIN

Inertial EME2000 x position coordinate.

VTS_YIN

public static final AbstractVTSWriter.ColumnId VTS_YIN

Inertial EME2000 y position coordinate.

VTS_ZIN

public static final AbstractVTSWriter.ColumnId VTS_ZIN

Inertial EME2000 z position coordinate.

VTS_VXIN

public static final AbstractVTSWriter.ColumnId VTS_VXIN

Inertial EME2000 x velocity coordinate.

VTS_VYIN

public static final AbstractVTSWriter.ColumnId VTS_VYIN

Inertial EME2000 y velocity coordinate.

VTS_VZIN

public static final AbstractVTSWriter.ColumnId VTS_VZIN

Inertial EME2000 y velocity coordinate.

VTS_PSI

public static final AbstractVTSWriter.ColumnId VTS_PSI

First elementary rotation in EME2000 frame.

VTS_THETA

public static final AbstractVTSWriter.ColumnId VTS_THETA

Second elementary rotation in EME2000 frame.

VTS_PHI

public static final AbstractVTSWriter.ColumnId VTS_PHI

Third elementary rotation in EME2000 frame.

LSSAT

public static final AbstractVTSWriter.ColumnId LSSAT

Percentage of the illuminated surface of the spacecraft.

LSPAN

public static final AbstractVTSWriter.ColumnId LSPAN

Percentage of the illuminated surface of the solar panels.

AM

public static final AbstractVTSWriter.ColumnId AM

Mean (Secular Lyddane model) semi-major axis.

EM

public static final AbstractVTSWriter.ColumnId EM

Mean (Secular Lyddane model) eccentricity.

IM

public static final AbstractVTSWriter.ColumnId IM

Mean (Secular Lyddane model) inclination.

AOPM

public static final AbstractVTSWriter.ColumnId AOPM

Mean (Secular Lyddane model) argument of perigee.

RAANM

public static final AbstractVTSWriter.ColumnId RAANM

Mean (Secular Lyddane model) right ascension of the ascending node.

MAM

public static final AbstractVTSWriter.ColumnId MAM

Mean (Secular Lyddane model) mean anomaly.

EXM

public static final AbstractVTSWriter.ColumnId EXM

First component of the eccentricity vector.

EYM

public static final AbstractVTSWriter.ColumnId EYM

Second component of eccentricity vector.

F107

public static final AbstractVTSWriter.ColumnId F107

Solar flux.

AP

public static final AbstractVTSWriter.ColumnId AP

Geomagnetic index.

Method Detail

values

public static AbstractVTSWriter.ColumnId[] 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 (AbstractVTSWriter.ColumnId c : AbstractVTSWriter.ColumnId.values())
    System.out.println(c);

Returns:

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

valueOf

public static AbstractVTSWriter.ColumnId 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