AttitudeEntryKey (ORbit Extrapolation KIT 11.1.2 API)

java.lang.Object
- java.lang.Enum<AttitudeEntryKey>
- - org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntryKey

All Implemented Interfaces:

Serializable, Comparable<AttitudeEntryKey>
```
public enum AttitudeEntryKey
extends Enum<AttitudeEntryKey>
```
Keys for attitude entries in XML messages.

Since:

11.0

Author:

Luc Maisonobe

Enum Constant Summary

Enum Constants
Enum Constant and Description
`EPOCH` Entry epoch.
`eulerAngle` Euler angle sub-section.
`eulerAngleRate` Euler angle/rate sub-section.
`NUTATION` Nutation angle entry.
`NUTATION_PER` Nutation period entry.
`NUTATION_PHASE` Nutation phase entry.
`Q1` Quaternion first vectorial component.
`Q1_DOT` Quaternion first vectorial component.
`Q2` Quaternion second vectorial component.
`Q2_DOT` Quaternion second vectorial component.
`Q3` Quaternion third vectorial component.
`Q3_DOT` Quaternion third vectorial component.
`QC` Quaternion scalar component.
`QC_DOT` Quaternion scalar component.
`quaternion` Quaternion sub-sub-section.
`quaternionDerivative` Quaternion/derivative sub-section.
`quaternionEulerRate` Quaternion/rate sub-section.
`quaternionRate` Quaternion rate sub-sub-section.
`quaternionState` Quaternion state sub-section.
`rotationAngles` Rotation angles sub-sub-section.
`rotationRates` Rotation rates sub-sub-section.
`spin` Spin sub-section.
`SPIN_ALPHA` Right ascension of spin axis vector.
`SPIN_ANGLE` Phase of satellite about spin axis.
`SPIN_ANGLE_VEL` angular velocity of satellite around spin axis.
`SPIN_DELTA` Declination of spin axis vector.
`spinNutation` Spin/nutation sub-section.
`X_ANGLE` Rotation about X axis.
`X_RATE` Rotation about X axis.
`Y_ANGLE` Rotation about Y axis.
`Y_RATE` Rotation about Y axis.
`Z_ANGLE` Rotation about Z axis.
`Z_RATE` Rotation about Z axis.

Method Summary

All Methods Static Methods Instance Methods Concrete Methods
Modifier and Type	Method and Description
`boolean`	`process(ParseToken token, ContextBinding context, org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntry container)` Process an token.
`static AttitudeEntryKey`	`valueOf(String name)` Returns the enum constant of this type with the specified name.
`static AttitudeEntryKey[]`	`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
  - quaternionState
```
public static final AttitudeEntryKey quaternionState
```
    Quaternion state sub-section.
  - quaternionDerivative
```
public static final AttitudeEntryKey quaternionDerivative
```
    Quaternion/derivative sub-section.
  - quaternionEulerRate
```
public static final AttitudeEntryKey quaternionEulerRate
```
    Quaternion/rate sub-section.
  - eulerAngle
```
public static final AttitudeEntryKey eulerAngle
```
    Euler angle sub-section.
  - eulerAngleRate
```
public static final AttitudeEntryKey eulerAngleRate
```
    Euler angle/rate sub-section.
  - spin
```
public static final AttitudeEntryKey spin
```
    Spin sub-section.
  - spinNutation
```
public static final AttitudeEntryKey spinNutation
```
    Spin/nutation sub-section.
  - quaternion
```
public static final AttitudeEntryKey quaternion
```
    Quaternion sub-sub-section.
  - quaternionRate
```
public static final AttitudeEntryKey quaternionRate
```
    Quaternion rate sub-sub-section.
  - rotationAngles
```
public static final AttitudeEntryKey rotationAngles
```
    Rotation angles sub-sub-section.
  - rotationRates
```
public static final AttitudeEntryKey rotationRates
```
    Rotation rates sub-sub-section.
  - EPOCH
```
public static final AttitudeEntryKey EPOCH
```
    Entry epoch.
  - Q1
```
public static final AttitudeEntryKey Q1
```
    Quaternion first vectorial component.
  - Q2
```
public static final AttitudeEntryKey Q2
```
    Quaternion second vectorial component.
  - Q3
```
public static final AttitudeEntryKey Q3
```
    Quaternion third vectorial component.
  - QC
```
public static final AttitudeEntryKey QC
```
    Quaternion scalar component.
  - Q1_DOT
```
public static final AttitudeEntryKey Q1_DOT
```
    Quaternion first vectorial component.
  - Q2_DOT
```
public static final AttitudeEntryKey Q2_DOT
```
    Quaternion second vectorial component.
  - Q3_DOT
```
public static final AttitudeEntryKey Q3_DOT
```
    Quaternion third vectorial component.
  - QC_DOT
```
public static final AttitudeEntryKey QC_DOT
```
    Quaternion scalar component.
  - X_ANGLE
```
public static final AttitudeEntryKey X_ANGLE
```
    Rotation about X axis.
  - Y_ANGLE
```
public static final AttitudeEntryKey Y_ANGLE
```
    Rotation about Y axis.
  - Z_ANGLE
```
public static final AttitudeEntryKey Z_ANGLE
```
    Rotation about Z axis.
  - X_RATE
```
public static final AttitudeEntryKey X_RATE
```
    Rotation about X axis.
  - Y_RATE
```
public static final AttitudeEntryKey Y_RATE
```
    Rotation about Y axis.
  - Z_RATE
```
public static final AttitudeEntryKey Z_RATE
```
    Rotation about Z axis.
  - SPIN_ALPHA
```
public static final AttitudeEntryKey SPIN_ALPHA
```
    Right ascension of spin axis vector.
  - SPIN_DELTA
```
public static final AttitudeEntryKey SPIN_DELTA
```
    Declination of spin axis vector.
  - SPIN_ANGLE
```
public static final AttitudeEntryKey SPIN_ANGLE
```
    Phase of satellite about spin axis.
  - SPIN_ANGLE_VEL
```
public static final AttitudeEntryKey SPIN_ANGLE_VEL
```
    angular velocity of satellite around spin axis.
  - NUTATION
```
public static final AttitudeEntryKey NUTATION
```
    Nutation angle entry.
  - NUTATION_PER
```
public static final AttitudeEntryKey NUTATION_PER
```
    Nutation period entry.
  - NUTATION_PHASE
```
public static final AttitudeEntryKey NUTATION_PHASE
```
    Nutation phase entry.
- Method Detail
  - values
```
public static AttitudeEntryKey[] 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 (AttitudeEntryKey c : AttitudeEntryKey.values())
    System.out.println(c);
```
    Returns:
    
    an array containing the constants of this enum type, in the order they are declared
  - valueOf
```
public static AttitudeEntryKey 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,
                       org.orekit.files.ccsds.ndm.adm.aem.AttitudeEntry container)
```
    Process an token.
    
    Parameters:
    
    token - token to process
    
    context - context binding
    
    container - container to fill
    
    Returns:
    
    true of token was accepted

Enum AttitudeEntryKey

Enum Constant Summary

Method Summary

Methods inherited from class java.lang.Enum

Methods inherited from class java.lang.Object

Enum Constant Detail

quaternionState

quaternionDerivative

quaternionEulerRate

eulerAngle

eulerAngleRate

spin

spinNutation

quaternion

quaternionRate

rotationAngles

rotationRates

EPOCH

Q1

Q2

Q3

QC

Q1_DOT

Q2_DOT

Q3_DOT

QC_DOT

X_ANGLE

Y_ANGLE

Z_ANGLE

X_RATE

Y_RATE

Z_RATE

SPIN_ALPHA

SPIN_DELTA

SPIN_ANGLE

SPIN_ANGLE_VEL

NUTATION

NUTATION_PER

NUTATION_PHASE

Method Detail

values

valueOf

process