VarList (psimu 11.5 API)

java.lang.Object
- java.lang.Enum<VarList>
- - calc.output.VarList

All Implemented Interfaces:

Serializable, Comparable<VarList>
```
public enum VarList
extends Enum<VarList>
```
Enumerate for all JPSIMU available output variables.

Author:

sumelzi

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.
`EX` First component of the eccentricity vector.
`EY` 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.
`VXIN` Velocity in inertial x coordinates.
`VXREL` X component of the relative velocity in rotating frame.
`VYIN` Velocity in inertial y coordinates.
`VYREL` Y component of the relative velocity in rotating frame.
`VZIN` Velocity in inertial z coordinates.
`VZREL` Z component of the relative velocity in rotating frame.
`XIN` Inertial x coordinates.
`XREL` X component of the relative position in rotating frame.
`XSPIN` Spin rate about x satellite axis.
`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.
`ZIN` Inertial z coordinates.
`ZREL` Z component of the relative position in rotating frame.
`ZSPIN` Spin rate about z satellite axis.

Method Summary

All Methods Static Methods Instance Methods Concrete Methods
Modifier and Type	Method and Description
`String`	`getDescription()` Get description of the output variable.
`Double`	`getGapThreshold()` Get the gap threshold value.
`fr.cnes.genius.sqlite.ColumnInfo.ColumnType`	`getType()` Get the column type.
`String`	`getUnit()` Get units.
`boolean`	`isUserVisible()` Get if the variable shall be displayed in the userLsit.
`static VarList`	`valueOf(String name)` Returns the enum constant of this type with the specified name.
`static VarList[]`	`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
  - DATE
```
public static final VarList DATE
```
    Date.
  - TIME
```
public static final VarList TIME
```
    Duration.
  - TMASS
```
public static final VarList TMASS
```
    Total mass.
  - PMASS
```
public static final VarList PMASS
```
    Propellant mass.
  - XIN
```
public static final VarList XIN
```
    Inertial x coordinates.
  - YIN
```
public static final VarList YIN
```
    Inertial y coordinates.
  - ZIN
```
public static final VarList ZIN
```
    Inertial z coordinates.
  - VXIN
```
public static final VarList VXIN
```
    Velocity in inertial x coordinates.
  - VYIN
```
public static final VarList VYIN
```
    Velocity in inertial y coordinates.
  - VZIN
```
public static final VarList VZIN
```
    Velocity in inertial z coordinates.
  - POSIN
```
public static final VarList POSIN
```
    Position norm in inertial frame.
  - VIN
```
public static final VarList VIN
```
    Velocity norm in inertial frame.
  - XREL
```
public static final VarList XREL
```
    X component of the relative position in rotating frame.
  - YREL
```
public static final VarList YREL
```
    Y component of the relative position in rotating frame.
  - ZREL
```
public static final VarList ZREL
```
    Z component of the relative position in rotating frame.
  - VXREL
```
public static final VarList VXREL
```
    X component of the relative velocity in rotating frame.
  - VYREL
```
public static final VarList VYREL
```
    Y component of the relative velocity in rotating frame.
  - VZREL
```
public static final VarList VZREL
```
    Z component of the relative velocity in rotating frame.
  - VREL
```
public static final VarList VREL
```
    Relative velocity in rotating frame.
  - A
```
public static final VarList A
```
    Semi-major axis.
  - E
```
public static final VarList E
```
    Eccentricity.
  - I
```
public static final VarList I
```
    Inclination.
  - AOP
```
public static final VarList AOP
```
    Perigee argument.
  - RAAN
```
public static final VarList RAAN
```
    Argument of the ascending node.
  - TA
```
public static final VarList TA
```
    True anomaly.
  - MA
```
public static final VarList MA
```
    Mean anomaly.
  - EA
```
public static final VarList EA
```
    Eccentric anomaly.
  - EX
```
public static final VarList EX
```
    First component of the eccentricity vector.
  - EY
```
public static final VarList EY
```
    Second component of eccentricity vector.
  - HX
```
public static final VarList HX
```
    First component of the inclination vector.
  - HY
```
public static final VarList HY
```
    Second component of the inclination vector.
  - TAOL
```
public static final VarList TAOL
```
    True latitude argument.
  - MAOL
```
public static final VarList MAOL
```
    Mean latitude argument.
  - EAOL
```
public static final VarList EAOL
```
    Eccentric latitude argument.
  - PERI
```
public static final VarList PERI
```
    Periapsis.
  - APO
```
public static final VarList APO
```
    Apoapsis.
  - PERIALT
```
public static final VarList PERIALT
```
    Periapsis.
  - APOALT
```
public static final VarList APOALT
```
    Apoapsis.
  - LATG
```
public static final VarList LATG
```
    Geodetic latitude.
  - LON
```
public static final VarList LON
```
    Geodetic longitude.
  - ALTG
```
public static final VarList ALTG
```
    Geodetic altitude.
  - LATS
```
public static final VarList LATS
```
    Geocentric latitude.
  - ALTS
```
public static final VarList ALTS
```
    Geocentric altitude.
  - AZIA
```
public static final VarList AZIA
```
    Velocity elevation in ITRF.
  - FPAA
```
public static final VarList FPAA
```
    Velocity elevation in ITRF.
  - AZIR
```
public static final VarList AZIR
```
    Velocity azimut in rotating frame.
  - FPAR
```
public static final VarList FPAR
```
    Velocity elevation in rotating frame.
  - PSI
```
public static final VarList PSI
```
    First elementary rotation in inertial frame.
  - THETA
```
public static final VarList THETA
```
    Second elementary rotation in inertial frame.
  - PHI
```
public static final VarList PHI
```
    Third elementary rotation in inertial frame.
  - PSIL
```
public static final VarList PSIL
```
    First elementary rotation in local frame.
  - THETAL
```
public static final VarList THETAL
```
    Second elementary rotation in local frame.
  - PHIL
```
public static final VarList PHIL
```
    Third elementary rotation in local frame.
  - Q0
```
public static final VarList Q0
```
    First quaternion component.
  - Q1
```
public static final VarList Q1
```
    Second quaternion component.
  - Q2
```
public static final VarList Q2
```
    Thrid quaternion component.
  - Q3
```
public static final VarList Q3
```
    Fourth quaternion component.
  - AOA
```
public static final VarList AOA
```
    Angle of attack.
  - BETA
```
public static final VarList BETA
```
    Sideslip.
  - BANK
```
public static final VarList BANK
```
    Roll velocity.
  - YAW
```
public static final VarList YAW
```
    Yaw in aircraft frame.
  - PITCH
```
public static final VarList PITCH
```
    Pitch in aircraft frame.
  - ROLL
```
public static final VarList ROLL
```
    Roll in aircraft frame.
  - SPIN
```
public static final VarList SPIN
```
    Spin rate.
  - XSPIN
```
public static final VarList XSPIN
```
    Spin rate about x satellite axis.
  - YSPIN
```
public static final VarList YSPIN
```
    Spin rate about y satellite axis.
  - ZSPIN
```
public static final VarList ZSPIN
```
    Spin rate about z satellite axis.
  - ACCN
```
public static final VarList ACCN
```
    Newtonian acceleration in propagation frame.
  - ACCNX
```
public static final VarList ACCNX
```
    X component of the newtonian acceleration.
  - ACCNY
```
public static final VarList ACCNY
```
    Y component of the newtonian acceleration.
  - ACCNZ
```
public static final VarList ACCNZ
```
    Z component of the newtonian acceleration.
  - ACCP
```
public static final VarList ACCP
```
    Earth potential acceleration.
  - ACCPX
```
public static final VarList ACCPX
```
    X component of the earth potential acceleration.
  - ACCPY
```
public static final VarList ACCPY
```
    Y component of the earth potential acceleration.
  - ACCPZ
```
public static final VarList ACCPZ
```
    Z component of the earth potential acceleration.
  - ACCM
```
public static final VarList ACCM
```
    Moon acceleration.
  - ACCMX
```
public static final VarList ACCMX
```
    X component of the moon acceleration.
  - ACCMY
```
public static final VarList ACCMY
```
    Y component of the moon acceleration.
  - ACCMZ
```
public static final VarList ACCMZ
```
    Z component of the moon acceleration.
  - ACCS
```
public static final VarList ACCS
```
    Sun acceleration.
  - ACCSX
```
public static final VarList ACCSX
```
    X component of the sun acceleration.
  - ACCSY
```
public static final VarList ACCSY
```
    Y component of the moon acceleration.
  - ACCSZ
```
public static final VarList ACCSZ
```
    Z component of the moon acceleration.
  - ACCA
```
public static final VarList ACCA
```
    Aerodynamic acceleration.
  - ACCAX
```
public static final VarList ACCAX
```
    X component of the aerodynamic acceleration.
  - ACCAY
```
public static final VarList ACCAY
```
    Y component of the aerodynamic acceleration.
  - ACCAZ
```
public static final VarList ACCAZ
```
    Z component of the aerodynamic acceleration.
  - ACCR
```
public static final VarList ACCR
```
    Solar radiation pressure acceleration.
  - ACCRX
```
public static final VarList ACCRX
```
    X component of the solar radiation pressure acceleration.
  - ACCRY
```
public static final VarList ACCRY
```
    Y component of the solar radiation pressure acceleration.
  - ACCRZ
```
public static final VarList ACCRZ
```
    Z component of the solar radiation pressure acceleration.
  - ACCT
```
public static final VarList ACCT
```
    Thrust acceleration.
  - ACCTX
```
public static final VarList ACCTX
```
    X component of the solar radiation pressure acceleration.
  - ACCTY
```
public static final VarList ACCTY
```
    Y component of the solar radiation pressure acceleration.
  - ACCTZ
```
public static final VarList ACCTZ
```
    Z component of the solar radiation pressure acceleration.
  - THRUST
```
public static final VarList THRUST
```
    Thrust.
  - USED_DV
```
public static final VarList USED_DV
```
    Thrust.
  - RHO
```
public static final VarList RHO
```
    Atmospheric density.
  - CX
```
public static final VarList CX
```
    Drag coefficient.
  - CZ
```
public static final VarList CZ
```
    Lift coefficient.
  - MACH
```
public static final VarList MACH
```
    Mach number.
  - MLT
```
public static final VarList MLT
```
    Mean local time in TIRF.
  - TLT
```
public static final VarList TLT
```
    True local time in TIRF.
  - VTS_DATE
```
public static final VarList VTS_DATE
```
    Date for VTS files in EME2000.
  - VTS_XIN
```
public static final VarList VTS_XIN
```
    Inertial EME2000 x position coordinate.
  - VTS_YIN
```
public static final VarList VTS_YIN
```
    Inertial EME2000 y position coordinate.
  - VTS_ZIN
```
public static final VarList VTS_ZIN
```
    Inertial EME2000 z position coordinate.
  - VTS_VXIN
```
public static final VarList VTS_VXIN
```
    Inertial EME2000 x velocity coordinate.
  - VTS_VYIN
```
public static final VarList VTS_VYIN
```
    Inertial EME2000 y velocity coordinate.
  - VTS_VZIN
```
public static final VarList VTS_VZIN
```
    Inertial EME2000 y velocity coordinate.
  - VTS_PSI
```
public static final VarList VTS_PSI
```
    First elementary rotation in EME2000 frame.
  - VTS_THETA
```
public static final VarList VTS_THETA
```
    Second elementary rotation in EME2000 frame.
  - VTS_PHI
```
public static final VarList VTS_PHI
```
    Third elementary rotation in EME2000 frame.
  - LSSAT
```
public static final VarList LSSAT
```
    Percentage of the illuminated surface of the spacecraft.
  - LSPAN
```
public static final VarList LSPAN
```
    Percentage of the illuminated surface of the solar panels.
  - AM
```
public static final VarList AM
```
    Mean (Secular Lyddane model) semi-major axis.
  - EM
```
public static final VarList EM
```
    Mean (Secular Lyddane model) eccentricity.
  - IM
```
public static final VarList IM
```
    Mean (Secular Lyddane model) inclination.
  - AOPM
```
public static final VarList AOPM
```
    Mean (Secular Lyddane model) argument of perigee.
  - RAANM
```
public static final VarList RAANM
```
    Mean (Secular Lyddane model) right ascension of the ascending node.
  - MAM
```
public static final VarList MAM
```
    Mean (Secular Lyddane model) mean anomaly.
  - F107
```
public static final VarList F107
```
    Solar flux.
  - AP
```
public static final VarList AP
```
    Geomagnetic index.
- Method Detail
  - values
```
public static VarList[] 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 (VarList c : VarList.values())
    System.out.println(c);
```
    Returns:
    
    an array containing the constants of this enum type, in the order they are declared
  - valueOf
```
public static VarList 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
  - getDescription
```
public String getDescription()
```
    Get description of the output variable.
    
    Returns:
    
    the description
  - getUnit
```
public String getUnit()
```
    Get units.
    
    Returns:
    
    the units
  - getType
```
public fr.cnes.genius.sqlite.ColumnInfo.ColumnType getType()
```
    Get the column type.
    
    Returns:
    
    the column type.
  - isUserVisible
```
public boolean isUserVisible()
```
    Get if the variable shall be displayed in the userLsit.
    
    Returns:
    
    if the variable shall be displayed in the userLsit.
  - getGapThreshold
```
public Double getGapThreshold()
```
    Get the gap threshold value.
    
    Returns:
    
    gap threshold value.

Enum VarList

Enum Constant Summary

Method Summary

Methods inherited from class java.lang.Enum

Methods inherited from class java.lang.Object

Enum Constant Detail

DATE

TIME

TMASS

PMASS

XIN

YIN

ZIN

VXIN

VYIN

VZIN

POSIN

VIN

XREL

YREL

ZREL

VXREL

VYREL

VZREL

VREL

A

E

I

AOP

RAAN

TA

MA

EA

EX

EY

HX

HY

TAOL

MAOL

EAOL

PERI

APO

PERIALT

APOALT

LATG

LON

ALTG

LATS

ALTS

AZIA

FPAA

AZIR

FPAR

PSI

THETA

PHI

PSIL

THETAL

PHIL

Q0

Q1

Q2

Q3

AOA

BETA

BANK

YAW

PITCH

ROLL

SPIN

XSPIN

YSPIN

ZSPIN

ACCN

ACCNX

ACCNY

ACCNZ

ACCP

ACCPX

ACCPY