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

All Implemented Interfaces:

Serializable, Comparable<ManeuverFieldType>
```
public enum ManeuverFieldType
extends Enum<ManeuverFieldType>
```
Maneuver field type used in CCSDS Orbit Comprehensive Messages.

Since:

11.0

Author:

Luc Maisonobe

Enum Constant Summary

Enum Constants
Enum Constant	Description
`ACC_DIR_SIGMA`	One σ off-nominal acceleration direction.
`ACC_INTERP`	Interpolation mode between current and next acceleration line.
`ACC_MAG_SIGMA`	One σ percent error on acceleration magnitude.
`ACC_X`	Acceleration along X axis.
`ACC_Y`	Acceleration along Y axis.
`ACC_Z`	Acceleration along Z axis.
`DELTA_MASS`	Mass change.
`DEPLOY_DIR_SIGMA`	One σ angular off-nominal deployment vector direction.
`DEPLOY_DV_CDA`	Typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
`DEPLOY_DV_RATIO`	Ratio of child-to-host ΔV vectors.
`DEPLOY_DV_SIGMA`	One σ percent error on deployment ΔV magnitude.
`DEPLOY_DV_X`	Velocity increment of deployed "child" object along X axis.
`DEPLOY_DV_Y`	Velocity increment of deployed "child" object along Y axis.
`DEPLOY_DV_Z`	Velocity increment of deployed "child" object along Z axis.
`DEPLOY_ID`	Identifier of resulting "child" object deployed from this host.
`DEPLOY_MASS`	Decrement in host mass as a result of deployment (shall be ≤ 0).
`DV_DIR_SIGMA`	One σ angular off-nominal ΔV direction.
`DV_MAG_SIGMA`	One σ percent error on ΔV magnitude.
`DV_X`	Velocity increment along X axis.
`DV_Y`	Velocity increment along Y axis.
`DV_Z`	Velocity increment along Z axis.
`MAN_DURA`	Maneuver duration.
`THR_DIR_SIGMA`	One σ angular off-nominal thrust direction.
`THR_EFFIC`	Thrust efficiency η typically between 0.0 and 1.0.
`THR_INTERP`	Interpolation mode between current and next acceleration line.
`THR_ISP`	Thrust specific impulse.
`THR_MAG_SIGMA`	One σ percent error on thrust magnitude.
`THR_X`	Thrust component along X axis.
`THR_Y`	Thrust component along Y axis.
`THR_Z`	Thrust component along Z axis.
`TIME_ABSOLUTE`	Absolute epoch time.
`TIME_RELATIVE`	Relative epoch time.

Method Summary

All Methods Static Methods Instance Methods Concrete Methods
Modifier and Type	Method	Description
`void`	`checkUnit(Unit parsedUnit)`	Check if parsed unit is compatible with field type.
`Unit`	`getUnit()`	Get the field unit.
`boolean`	`isTime()`	Check if a field is a time field.
`String`	`outputField(TimeConverter converter, OrbitManeuver maneuver)`	Output one maneuver field.
`void`	`process(String field, ContextBinding context, OrbitManeuver maneuver, int lineNumber, String fileName)`	Process one field.
`static ManeuverFieldType`	`valueOf(String name)`	Returns the enum constant of this type with the specified name.
`static ManeuverFieldType[]`	`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
  - TIME_ABSOLUTE
```
public static final ManeuverFieldType TIME_ABSOLUTE
```
    Absolute epoch time.
  - TIME_RELATIVE
```
public static final ManeuverFieldType TIME_RELATIVE
```
    Relative epoch time.
  - MAN_DURA
```
public static final ManeuverFieldType MAN_DURA
```
    Maneuver duration.
  - DELTA_MASS
```
public static final ManeuverFieldType DELTA_MASS
```
    Mass change.
  - ACC_X
```
public static final ManeuverFieldType ACC_X
```
    Acceleration along X axis.
  - ACC_Y
```
public static final ManeuverFieldType ACC_Y
```
    Acceleration along Y axis.
  - ACC_Z
```
public static final ManeuverFieldType ACC_Z
```
    Acceleration along Z axis.
  - ACC_INTERP
```
public static final ManeuverFieldType ACC_INTERP
```
    Interpolation mode between current and next acceleration line.
  - ACC_MAG_SIGMA
```
public static final ManeuverFieldType ACC_MAG_SIGMA
```
    One σ percent error on acceleration magnitude.
  - ACC_DIR_SIGMA
```
public static final ManeuverFieldType ACC_DIR_SIGMA
```
    One σ off-nominal acceleration direction.
  - DV_X
```
public static final ManeuverFieldType DV_X
```
    Velocity increment along X axis.
  - DV_Y
```
public static final ManeuverFieldType DV_Y
```
    Velocity increment along Y axis.
  - DV_Z
```
public static final ManeuverFieldType DV_Z
```
    Velocity increment along Z axis.
  - DV_MAG_SIGMA
```
public static final ManeuverFieldType DV_MAG_SIGMA
```
    One σ percent error on ΔV magnitude.
  - DV_DIR_SIGMA
```
public static final ManeuverFieldType DV_DIR_SIGMA
```
    One σ angular off-nominal ΔV direction.
  - THR_X
```
public static final ManeuverFieldType THR_X
```
    Thrust component along X axis.
  - THR_Y
```
public static final ManeuverFieldType THR_Y
```
    Thrust component along Y axis.
  - THR_Z
```
public static final ManeuverFieldType THR_Z
```
    Thrust component along Z axis.
  - THR_EFFIC
```
public static final ManeuverFieldType THR_EFFIC
```
    Thrust efficiency η typically between 0.0 and 1.0.
  - THR_INTERP
```
public static final ManeuverFieldType THR_INTERP
```
    Interpolation mode between current and next acceleration line.
  - THR_ISP
```
public static final ManeuverFieldType THR_ISP
```
    Thrust specific impulse.
  - THR_MAG_SIGMA
```
public static final ManeuverFieldType THR_MAG_SIGMA
```
    One σ percent error on thrust magnitude.
  - THR_DIR_SIGMA
```
public static final ManeuverFieldType THR_DIR_SIGMA
```
    One σ angular off-nominal thrust direction.
  - DEPLOY_ID
```
public static final ManeuverFieldType DEPLOY_ID
```
    Identifier of resulting "child" object deployed from this host.
  - DEPLOY_DV_X
```
public static final ManeuverFieldType DEPLOY_DV_X
```
    Velocity increment of deployed "child" object along X axis.
  - DEPLOY_DV_Y
```
public static final ManeuverFieldType DEPLOY_DV_Y
```
    Velocity increment of deployed "child" object along Y axis.
  - DEPLOY_DV_Z
```
public static final ManeuverFieldType DEPLOY_DV_Z
```
    Velocity increment of deployed "child" object along Z axis.
  - DEPLOY_MASS
```
public static final ManeuverFieldType DEPLOY_MASS
```
    Decrement in host mass as a result of deployment (shall be ≤ 0).
  - DEPLOY_DV_SIGMA
```
public static final ManeuverFieldType DEPLOY_DV_SIGMA
```
    One σ percent error on deployment ΔV magnitude.
  - DEPLOY_DIR_SIGMA
```
public static final ManeuverFieldType DEPLOY_DIR_SIGMA
```
    One σ angular off-nominal deployment vector direction.
  - DEPLOY_DV_RATIO
```
public static final ManeuverFieldType DEPLOY_DV_RATIO
```
    Ratio of child-to-host ΔV vectors.
  - DEPLOY_DV_CDA
```
public static final ManeuverFieldType DEPLOY_DV_CDA
```
    Typical (50th percentile) product of drag coefficient times cross-sectional area of deployed "child" object.
- Method Detail
  - values
```
public static ManeuverFieldType[] 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 (ManeuverFieldType c : ManeuverFieldType.values()) System.out.println(c);
    Returns:
    
    an array containing the constants of this enum type, in the order they are declared
  - valueOf
```
public static ManeuverFieldType 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
  - getUnit
```
public Unit getUnit()
```
    Get the field unit.
    
    Returns:
    
    field unit
  - checkUnit
```
public void checkUnit(Unit parsedUnit)
```
    Check if parsed unit is compatible with field type.
    
    Parameters:
    
    parsedUnit - unit to check
  - isTime
```
public boolean isTime()
```
    Check if a field is a time field.
    
    Returns:
    
    true if field is a time field
  - process
```
public void process(String field,
                    ContextBinding context,
                    OrbitManeuver maneuver,
                    int lineNumber,
                    String fileName)
```
    Process one field.
    
    Parameters:
    
    field - field to process
    
    context - context binding
    
    maneuver - maneuver to fill
    
    lineNumber - line number at which the field occurs
    
    fileName - name of the file in which the field occurs
  - outputField
```
public String outputField(TimeConverter converter,
                          OrbitManeuver maneuver)
```
    Output one maneuver field.
    
    Parameters:
    
    converter - converter for dates
    
    maneuver - maneuver containing the field to output
    
    Returns:
    
    output field

Enum ManeuverFieldType

Enum Constant Summary

Method Summary

Methods inherited from class java.lang.Enum

Methods inherited from class java.lang.Object

Enum Constant Detail

TIME_ABSOLUTE

TIME_RELATIVE

MAN_DURA

DELTA_MASS

ACC_X

ACC_Y

ACC_Z

ACC_INTERP

ACC_MAG_SIGMA

ACC_DIR_SIGMA

DV_X

DV_Y

DV_Z

DV_MAG_SIGMA

DV_DIR_SIGMA

THR_X

THR_Y

THR_Z

THR_EFFIC

THR_INTERP

THR_ISP

THR_MAG_SIGMA

THR_DIR_SIGMA

DEPLOY_ID

DEPLOY_DV_X

DEPLOY_DV_Y

DEPLOY_DV_Z

DEPLOY_MASS

DEPLOY_DV_SIGMA

DEPLOY_DIR_SIGMA

DEPLOY_DV_RATIO

DEPLOY_DV_CDA

Method Detail

values

valueOf

getUnit

checkUnit

isTime

process

outputField