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

Enum OrbitManeuverHistoryMetadataKey

java.lang.Object

java.lang.Enum<OrbitManeuverHistoryMetadataKey>

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

All Implemented Interfaces:

Serializable, Comparable<OrbitManeuverHistoryMetadataKey>

public enum OrbitManeuverHistoryMetadataKey
extends Enum<OrbitManeuverHistoryMetadataKey>

Keys for maneuver history container entries.

Since:

11.0

Author:

Luc Maisonobe

Enum Constant Summary

Enum Constants

Enum Constant	Description
COMMENT	Comment entry.
DC_BODY_FRAME	Spacecraft body frame in which DC_BODY_TRIGGER is specified.
DC_BODY_TRIGGER	Direction in body frame for triggering duty cycle.
DC_EXEC_START	Start time of initial duty cycle-based maneuver execution.
DC_EXEC_STOP	End time of final duty cycle-based maneuver execution.
DC_MAX_CYCLES	Maximum number of "ON" duty cycles.
DC_MIN_CYCLES	Minimum number of "ON" duty cycles.
DC_PA_START_ANGLE	Phase angle of pulse start.
DC_PA_STOP_ANGLE	Phase angle of pulse stop.
DC_REF_DIR	Reference direction for triggering duty cycle.
DC_REF_TIME	Duty cycle thrust reference time.
DC_TIME_PULSE_DURATION	Duty cycle pulse "ON" duration.
DC_TIME_PULSE_PERIOD	Duty cycle elapsed time between start of a pulse and start of next pulse.
DC_TYPE	Type of duty cycle.
DC_WIN_CLOSE	Start time of duty cycle-based maneuver window.
DC_WIN_OPEN	Start time of duty cycle-based maneuver window.
GRAV_ASSIST_NAME	Origin of maneuver gravitational assist body.
MAN_BASIS	Basis of this maneuver history data.
MAN_BASIS_ID	Identification number of the orbit determination or simulation upon which this maneuver is based.
MAN_COMPOSITION	Maneuver elements of information.
MAN_DEVICE_ID	Identifier of the device used for this maneuver.
MAN_FRAME_EPOCH	Epoch of the maneuver reference frame.
MAN_ID	Maneuver identification number.
MAN_NEXT_EPOCH	Start time of next maneuver.
MAN_NEXT_ID	Identification number of next maneuver.
MAN_PRED_SOURCE	Prediction source on which this maneuver is based.
MAN_PREV_EPOCH	Completion time of previous maneuver.
MAN_PREV_ID	Identification number of previous maneuver.
MAN_PURPOSE	Purposes of the maneuver.
MAN_REF_FRAME	Reference frame of the maneuver.
MAN_UNITS	SI units for each elements of the maneuver.

Method Summary

Modifier and Type	Method	Description
boolean	process(ParseToken token, ContextBinding context, OrbitManeuverHistoryMetadata container)	Process an token.
static OrbitManeuverHistoryMetadataKey	valueOf(String name)	Returns the enum constant of this type with the specified name.
static OrbitManeuverHistoryMetadataKey[]	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

COMMENT

public static final OrbitManeuverHistoryMetadataKey COMMENT

Comment entry.

MAN_ID

public static final OrbitManeuverHistoryMetadataKey MAN_ID

Maneuver identification number.

MAN_PREV_ID

public static final OrbitManeuverHistoryMetadataKey MAN_PREV_ID

Identification number of previous maneuver.

MAN_NEXT_ID

public static final OrbitManeuverHistoryMetadataKey MAN_NEXT_ID

Identification number of next maneuver.

MAN_BASIS

public static final OrbitManeuverHistoryMetadataKey MAN_BASIS

Basis of this maneuver history data.

MAN_BASIS_ID

public static final OrbitManeuverHistoryMetadataKey MAN_BASIS_ID

Identification number of the orbit determination or simulation upon which this maneuver is based.

MAN_DEVICE_ID

public static final OrbitManeuverHistoryMetadataKey MAN_DEVICE_ID

Identifier of the device used for this maneuver.

MAN_PREV_EPOCH

public static final OrbitManeuverHistoryMetadataKey MAN_PREV_EPOCH

Completion time of previous maneuver.

MAN_NEXT_EPOCH

public static final OrbitManeuverHistoryMetadataKey MAN_NEXT_EPOCH

Start time of next maneuver.

MAN_PURPOSE

public static final OrbitManeuverHistoryMetadataKey MAN_PURPOSE

Purposes of the maneuver.

MAN_PRED_SOURCE

public static final OrbitManeuverHistoryMetadataKey MAN_PRED_SOURCE

Prediction source on which this maneuver is based.

MAN_REF_FRAME

public static final OrbitManeuverHistoryMetadataKey MAN_REF_FRAME

Reference frame of the maneuver.

MAN_FRAME_EPOCH

public static final OrbitManeuverHistoryMetadataKey MAN_FRAME_EPOCH

Epoch of the maneuver reference frame.

GRAV_ASSIST_NAME

public static final OrbitManeuverHistoryMetadataKey GRAV_ASSIST_NAME

Origin of maneuver gravitational assist body.

DC_TYPE

public static final OrbitManeuverHistoryMetadataKey DC_TYPE

Type of duty cycle.

DC_WIN_OPEN

public static final OrbitManeuverHistoryMetadataKey DC_WIN_OPEN

Start time of duty cycle-based maneuver window.

DC_WIN_CLOSE

public static final OrbitManeuverHistoryMetadataKey DC_WIN_CLOSE

Start time of duty cycle-based maneuver window.

DC_MIN_CYCLES

public static final OrbitManeuverHistoryMetadataKey DC_MIN_CYCLES

Minimum number of "ON" duty cycles.

DC_MAX_CYCLES

public static final OrbitManeuverHistoryMetadataKey DC_MAX_CYCLES

Maximum number of "ON" duty cycles.

DC_EXEC_START

public static final OrbitManeuverHistoryMetadataKey DC_EXEC_START

Start time of initial duty cycle-based maneuver execution.

DC_EXEC_STOP

public static final OrbitManeuverHistoryMetadataKey DC_EXEC_STOP

End time of final duty cycle-based maneuver execution.

DC_REF_TIME

public static final OrbitManeuverHistoryMetadataKey DC_REF_TIME

Duty cycle thrust reference time.

DC_TIME_PULSE_DURATION

public static final OrbitManeuverHistoryMetadataKey DC_TIME_PULSE_DURATION

Duty cycle pulse "ON" duration.

DC_TIME_PULSE_PERIOD

public static final OrbitManeuverHistoryMetadataKey DC_TIME_PULSE_PERIOD

Duty cycle elapsed time between start of a pulse and start of next pulse.

DC_REF_DIR

public static final OrbitManeuverHistoryMetadataKey DC_REF_DIR

Reference direction for triggering duty cycle.

DC_BODY_FRAME

public static final OrbitManeuverHistoryMetadataKey DC_BODY_FRAME

Spacecraft body frame in which DC_BODY_TRIGGER is specified.

DC_BODY_TRIGGER

public static final OrbitManeuverHistoryMetadataKey DC_BODY_TRIGGER

Direction in body frame for triggering duty cycle.

DC_PA_START_ANGLE

public static final OrbitManeuverHistoryMetadataKey DC_PA_START_ANGLE

Phase angle of pulse start.

DC_PA_STOP_ANGLE

public static final OrbitManeuverHistoryMetadataKey DC_PA_STOP_ANGLE

Phase angle of pulse stop.

MAN_COMPOSITION

public static final OrbitManeuverHistoryMetadataKey MAN_COMPOSITION

Maneuver elements of information.

MAN_UNITS

public static final OrbitManeuverHistoryMetadataKey MAN_UNITS

SI units for each elements of the maneuver.

Method Detail

values

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

Returns:

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

valueOf

public static OrbitManeuverHistoryMetadataKey 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,
                       OrbitManeuverHistoryMetadata container)

Process an token.

Parameters:

token - token to process

context - context binding

container - container to fill

Returns:

true of token was accepted