OrekitMessages.java
/* Copyright 2002-2024 CS GROUP
* Licensed to CS GROUP (CS) under one or more
* contributor license agreements. See the NOTICE file distributed with
* this work for additional information regarding copyright ownership.
* CS licenses this file to You under the Apache License, Version 2.0
* (the "License"); you may not use this file except in compliance with
* the License. You may obtain a copy of the License at
*
* http://www.apache.org/licenses/LICENSE-2.0
*
* Unless required by applicable law or agreed to in writing, software
* distributed under the License is distributed on an "AS IS" BASIS,
* WITHOUT WARRANTIES OR CONDITIONS OF ANY KIND, either express or implied.
* See the License for the specific language governing permissions and
* limitations under the License.
*/
package org.orekit.errors;
import org.hipparchus.exception.Localizable;
import org.hipparchus.exception.UTF8Control;
import java.util.Locale;
import java.util.MissingResourceException;
import java.util.ResourceBundle;
/**
* Enumeration for localized messages formats.
* <p>
* The constants in this enumeration represent the available formats as
* localized strings. These formats are intended to be localized using simple
* properties files, using the constant name as the key and the property value
* as the message format. The source English format is provided in the constants
* themselves to serve both as a reminder for developers to understand the
* parameters needed by each format, as a basis for translators to create
* localized properties files, and as a default format if some translation is
* missing.
* </p>
* @since 2.1
*/
public enum OrekitMessages implements Localizable {
/** INTERNAL_ERROR. */
INTERNAL_ERROR("internal error, please notify development team by creating a new topic at {0}"),
/** ALTITUDE_BELOW_ALLOWED_THRESHOLD. */
ALTITUDE_BELOW_ALLOWED_THRESHOLD("altitude ({0} m) is below the {1} m allowed threshold"),
/** POINT_INSIDE_ELLIPSOID. */
POINT_INSIDE_ELLIPSOID("point is inside ellipsoid"),
/** TRAJECTORY_INSIDE_BRILLOUIN_SPHERE. */
TRAJECTORY_INSIDE_BRILLOUIN_SPHERE("trajectory inside the Brillouin sphere (r = {0})"),
/** ALMOST_EQUATORIAL_ORBIT. */
ALMOST_EQUATORIAL_ORBIT("almost equatorial orbit (i = {0} degrees)"),
/** ALMOST_CRITICALLY_INCLINED_ORBIT. */
ALMOST_CRITICALLY_INCLINED_ORBIT("almost critically inclined orbit (i = {0} degrees)"),
/** UNABLE_TO_COMPUTE_ECKSTEIN_HECHLER_MEAN_PARAMETERS. */
UNABLE_TO_COMPUTE_ECKSTEIN_HECHLER_MEAN_PARAMETERS("unable to compute Eckstein-Hechler mean parameters after {0} iterations"),
/** UNABLE_TO_COMPUTE_BROUWER_LYDDANE_MEAN_PARAMETERS. */
UNABLE_TO_COMPUTE_BROUWER_LYDDANE_MEAN_PARAMETERS("unable to compute Brouwer-Lyddane mean parameters after {0} iterations"),
/** UNABLE_TO_COMPUTE_TLE. */
UNABLE_TO_COMPUTE_TLE("unable to compute TLE after {0} iterations"),
/** NULL_PARENT_FOR_FRAME. */
NULL_PARENT_FOR_FRAME("null parent for frame {0}"),
/** FRAME_ALREADY_ATTACHED. */
FRAME_ALREADY_ATTACHED("frame {0} is already attached to frame {1}"),
/** FRAME_NOT_ATTACHED. */
FRAME_NOT_ATTACHED("frame {0} is not attached to the main frames tree"),
/** FRAME_ANCESTOR_OF_BOTH_FRAMES. */
FRAME_ANCESTOR_OF_BOTH_FRAMES("frame {0} is an ancestor of both frames {1} and {2}"),
/** FRAME_ANCESTOR_OF_NEITHER_FRAME. */
FRAME_ANCESTOR_OF_NEITHER_FRAME("frame {0} is an ancestor of neither frame {1} nor {2}"),
/** FRAME_NO_NTH_ANCESTOR. */
FRAME_NO_NTH_ANCESTOR("frame {0} has depth {1}, it cannot have an ancestor {2} levels above"),
/** NO_SUCH_ITRF_FRAME. */
NO_SUCH_ITRF_FRAME("ITRF frame {0} not found"),
/** UNSUPPORTED_LOCAL_ORBITAL_FRAME. */
UNSUPPORTED_LOCAL_ORBITAL_FRAME("unsupported local orbital frame {0}"),
/** NON_PSEUDO_INERTIAL_FRAME. */
NON_PSEUDO_INERTIAL_FRAME("non pseudo-inertial frame \"{0}\""),
/** DATA_ROOT_DIRECTORY_DOES_NOT_EXIST. */
DATA_ROOT_DIRECTORY_DOES_NOT_EXIST("data root directory {0} does not exist"),
/** NOT_A_DIRECTORY. */
NOT_A_DIRECTORY("{0} is not a directory"),
/** NEITHER_DIRECTORY_NOR_ZIP_OR_JAR. */
NEITHER_DIRECTORY_NOR_ZIP_OR_JAR("{0} is neither a directory nor a zip/jar archive file"),
/** UNABLE_TO_FIND_RESOURCE. */
UNABLE_TO_FIND_RESOURCE("unable to find resource {0} in classpath"),
/** NO_EARTH_ORIENTATION_PARAMETERS_LOADED. */
NO_EARTH_ORIENTATION_PARAMETERS_LOADED("no Earth Orientation Parameters loaded"),
/** MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES. */
MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES("missing Earth Orientation Parameters between {0} and {1}"),
/** MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES_GAP. */
MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES_GAP("missing Earth Orientation Parameters between {0} and {1}, gap is {2,number,0.0##############E0} s"),
/** NO_EARTH_ORIENTATION_PARAMETERS. */
NO_EARTH_ORIENTATION_PARAMETERS("missing Earth Orientation Parameters"),
/** NOT_A_SUPPORTED_IERS_DATA_FILE. */
NOT_A_SUPPORTED_IERS_DATA_FILE("file {0} is not a supported IERS data file"),
/** INCONSISTENT_DATES_IN_IERS_FILE. */
INCONSISTENT_DATES_IN_IERS_FILE("inconsistent dates in IERS file {0}: {1}-{2}-{3} and MJD {4}"),
/** UNEXPECTED_DATA_AFTER_LINE_IN_FILE. */
UNEXPECTED_DATA_AFTER_LINE_IN_FILE("unexpected data after line {0} in file {1}: {2}"),
/** UNEXPECTED_DATA_AT_LINE_IN_FILE. */
UNEXPECTED_DATA_AT_LINE_IN_FILE("unexpected data at line {0} in file {1}"),
/** NON_CHRONOLOGICAL_DATES_IN_FILE. */
NON_CHRONOLOGICAL_DATES_IN_FILE("non-chronological dates in file {0}, line {1}"),
/** NO_IERS_UTC_TAI_HISTORY_DATA_LOADED. */
NO_IERS_UTC_TAI_HISTORY_DATA_LOADED("no IERS UTC-TAI history data loaded"),
/** NO_ENTRIES_IN_IERS_UTC_TAI_HISTORY_FILE. */
NO_ENTRIES_IN_IERS_UTC_TAI_HISTORY_FILE("no entries found in IERS UTC-TAI history file {0}"),
/** MISSING_SERIE_J_IN_FILE. */
MISSING_SERIE_J_IN_FILE("missing serie j = {0} in file {1} (line {2})"),
/** CANNOT_PARSE_BOTH_TAU_AND_GAMMA. */
CANNOT_PARSE_BOTH_TAU_AND_GAMMA("cannot parse both τ and γ from the same Poissons series file"),
/** UNEXPECTED_END_OF_FILE_AFTER_LINE. */
UNEXPECTED_END_OF_FILE_AFTER_LINE("unexpected end of file {0} (after line {1})"),
/** UNABLE_TO_PARSE_LINE_IN_FILE. */
UNABLE_TO_PARSE_LINE_IN_FILE("unable to parse line {0} of file {1}:\n{2}"),
/** UNABLE_TO_PARSE_ELEMENT_IN_FILE. */
UNABLE_TO_PARSE_ELEMENT_IN_FILE("unable to parse element {0} at line {1}, file {2}"),
/** UNABLE_TO_FIND_FILE. */
UNABLE_TO_FIND_FILE("unable to find file {0}"),
/** POSITIVE_FLOW_RATE. */
POSITIVE_FLOW_RATE("positive flow rate (q: {0})"),
/** NO_GRAVITY_FIELD_DATA_LOADED. */
NO_GRAVITY_FIELD_DATA_LOADED("no gravity field data loaded"),
/** GRAVITY_FIELD_NORMALIZATION_UNDERFLOW. */
GRAVITY_FIELD_NORMALIZATION_UNDERFLOW("gravity field normalization underflow for degree {0} and order {1}"),
/** NO_OCEAN_TIDE_DATA_LOADED. */
NO_OCEAN_TIDE_DATA_LOADED("no ocean tide data loaded"),
/** OCEAN_TIDE_DATA_DEGREE_ORDER_LIMITS. */
OCEAN_TIDE_DATA_DEGREE_ORDER_LIMITS("ocean tide data file {0} limited to degree {1} and order {2}"),
/** OCEAN_TIDE_LOAD_DEFORMATION_LIMITS. */
OCEAN_TIDE_LOAD_DEFORMATION_LIMITS("load deformation coefficients limited to degree {0}, cannot parse degree {1} term from file {2}"),
/** POLAR_TRAJECTORY. */
POLAR_TRAJECTORY("polar trajectory (distance to polar axis: {0})"),
/** UNEXPECTED_FILE_FORMAT_ERROR_FOR_LOADER. */
UNEXPECTED_FILE_FORMAT_ERROR_FOR_LOADER("unexpected format error for file {0} with loader {1}"),
/** DUPLICATED_GRAVITY_FIELD_COEFFICIENT_IN_FILE. */
DUPLICATED_GRAVITY_FIELD_COEFFICIENT_IN_FILE("duplicated gravity field coefficient {0}({1}, {2}) in file {3}"),
/** MISSING_GRAVITY_FIELD_COEFFICIENT_IN_FILE. */
MISSING_GRAVITY_FIELD_COEFFICIENT_IN_FILE("missing gravity field coefficient {0}({1}, {2}) in file {3}"),
/** TOO_LARGE_DEGREE_FOR_GRAVITY_FIELD. */
TOO_LARGE_DEGREE_FOR_GRAVITY_FIELD("too large degree (n = {0}, potential maximal degree is {1})"),
/** TOO_LARGE_ORDER_FOR_GRAVITY_FIELD. */
TOO_LARGE_ORDER_FOR_GRAVITY_FIELD("too large order (m = {0}, potential maximal order is {1})"),
/** WRONG_DEGREE_OR_ORDER. */
WRONG_DEGREE_OR_ORDER("no term ({0}, {1}) in a {2}x{3} spherical harmonics decomposition"),
/** SEVERAL_REFERENCE_DATES_IN_GRAVITY_FIELD. */
SEVERAL_REFERENCE_DATES_IN_GRAVITY_FIELD("several reference dates ({0} and {1} differ by {3,number,0.0##############E0} s) found in gravity field file {2}"),
/** NO_TLE_FOR_OBJECT. */
NO_TLE_FOR_OBJECT("no TLE data available for object {0}"),
/** NO_TLE_FOR_LAUNCH_YEAR_NUMBER_PIECE. */
NO_TLE_FOR_LAUNCH_YEAR_NUMBER_PIECE("no TLE data available for launch year {0}, launch number {1}, launch piece {2}"),
/** NOT_TLE_LINES. */
NOT_TLE_LINES("lines {0} and {1} are not TLE lines:\n{0}: \"{2}\"\n{1}: \"{3}\""),
/** MISSING_SECOND_TLE_LINE. */
MISSING_SECOND_TLE_LINE("expected a second TLE line after line {0}:\n{0}: \"{1}\""),
/** TLE_LINES_DO_NOT_REFER_TO_SAME_OBJECT. */
TLE_LINES_DO_NOT_REFER_TO_SAME_OBJECT("TLE lines do not refer to the same object:\n{0}\n{1}"),
/** TLE_INVALID_PARAMETER. */
TLE_INVALID_PARAMETER("invalid TLE parameter for object {0}: {1} = {2}"),
/** TLE_CHECKSUM_ERROR. */
TLE_CHECKSUM_ERROR("wrong checksum of TLE line {0}, expected {1} but got {2} ({3})"),
/** NO_TLE_DATA_AVAILABLE. */
NO_TLE_DATA_AVAILABLE("no TLE data available"),
/** NOT_POSITIVE_SPACECRAFT_MASS. */
NOT_POSITIVE_SPACECRAFT_MASS("spacecraft mass is not positive: {0} kg"),
/** TOO_LARGE_ECCENTRICITY_FOR_PROPAGATION_MODEL. */
TOO_LARGE_ECCENTRICITY_FOR_PROPAGATION_MODEL("too large eccentricity for propagation model: e = {0}"),
/** NO_SOLAR_ACTIVITY_AT_DATE. */
NO_SOLAR_ACTIVITY_AT_DATE("no solar activity available at {0}, data available only in range [{1}, {2}]"),
/** NON_EXISTENT_MONTH. */
NON_EXISTENT_MONTH("non-existent month {0}"),
/** NON_EXISTENT_YEAR_MONTH_DAY. */
NON_EXISTENT_YEAR_MONTH_DAY("non-existent date {0}-{1}-{2}"),
/** NON_EXISTENT_WEEK_DATE. */
NON_EXISTENT_WEEK_DATE("non-existent week date {0}-W{1}-{2}"),
/** NON_EXISTENT_DATE. */
NON_EXISTENT_DATE("non-existent date {0}"),
/** NON_EXISTENT_DAY_NUMBER_IN_YEAR. */
NON_EXISTENT_DAY_NUMBER_IN_YEAR("no day number {0} in year {1}"),
/** NON_EXISTENT_HMS_TIME. */
NON_EXISTENT_HMS_TIME("non-existent time {0}:{1}:{2}"),
/** NON_EXISTENT_TIME. */
NON_EXISTENT_TIME("non-existent time {0}"),
/** OUT_OF_RANGE_SECONDS_NUMBER. */
OUT_OF_RANGE_SECONDS_NUMBER("out of range seconds number: {0}"),
/** OUT_OF_RANGE_SECONDS_NUMBER_DETAIL. */
OUT_OF_RANGE_SECONDS_NUMBER_DETAIL("out of range seconds number: {0} is not in [{1}, {2}]"),
/** ANGLE_TYPE_NOT_SUPPORTED. */
ANGLE_TYPE_NOT_SUPPORTED("angle type not supported, supported angles: {0}, {1} and {2}"),
/** SATELLITE_COLLIDED_WITH_TARGET. */
SATELLITE_COLLIDED_WITH_TARGET("satellite collided with target"),
/** ATTITUDE_POINTING_LAW_DOES_NOT_POINT_TO_GROUND. */
ATTITUDE_POINTING_LAW_DOES_NOT_POINT_TO_GROUND("attitude pointing law misses ground"),
/** TOO_SHORT_TRANSITION_TIME_FOR_ATTITUDES_SWITCH. */
TOO_SHORT_TRANSITION_TIME_FOR_ATTITUDES_SWITCH("{0} seconds transition time for attitudes switch is too short, should be longer than {1} seconds"),
/** ORBIT_AND_ATTITUDE_DATES_MISMATCH. */
ORBIT_AND_ATTITUDE_DATES_MISMATCH("orbit date ({0}) does not match attitude date ({1})"),
/** FRAMES_MISMATCH. */
FRAMES_MISMATCH("frame {0} does not match frame {1}"),
/** INITIAL_STATE_NOT_SPECIFIED_FOR_ORBIT_PROPAGATION. */
INITIAL_STATE_NOT_SPECIFIED_FOR_ORBIT_PROPAGATION("initial state not specified for orbit propagation"),
/** EVENT_DATE_TOO_CLOSE. */
EVENT_DATE_TOO_CLOSE("target event date must be before {1} by {3,number,0.0##############E0} seconds or after {2} by {3,number,0.0##############E0} seconds, but target event date {0} is {4,number,0.0##############E0} seconds before {1} and {5,number,0.0##############E0} seconds after {2} so it cannot be added"),
/** UNABLE_TO_READ_JPL_HEADER. */
UNABLE_TO_READ_JPL_HEADER("unable to read header record from JPL ephemerides binary file {0}"),
/** INCONSISTENT_ASTRONOMICAL_UNIT_IN_FILES. */
INCONSISTENT_ASTRONOMICAL_UNIT_IN_FILES("inconsistent values of astronomical unit in JPL ephemerides files: ({0} and {1})"),
/** INCONSISTENT_EARTH_MOON_RATIO_IN_FILES. */
INCONSISTENT_EARTH_MOON_RATIO_IN_FILES("inconsistent values of Earth/Moon mass ratio in JPL ephemerides files: ({0} and {1})"),
/** NO_DATA_LOADED_FOR_CELESTIAL_BODY. */
NO_DATA_LOADED_FOR_CELESTIAL_BODY("no data loaded for celestial body {0}"),
/** NOT_A_JPL_EPHEMERIDES_BINARY_FILE. */
NOT_A_JPL_EPHEMERIDES_BINARY_FILE("file {0} is not a JPL ephemerides binary file"),
/** NOT_A_MARSHALL_SOLAR_ACTIVITY_FUTURE_ESTIMATION_FILE. */
NOT_A_MARSHALL_SOLAR_ACTIVITY_FUTURE_ESTIMATION_FILE("file {0} is not a Marshall Solar Activity Future Estimation (MSAFE) file"),
/** NO_JPL_EPHEMERIDES_BINARY_FILES_FOUND. */
NO_JPL_EPHEMERIDES_BINARY_FILES_FOUND("no JPL ephemerides binary files found"),
/** OUT_OF_RANGE_BODY_EPHEMERIDES_DATE. */
OUT_OF_RANGE_BODY_EPHEMERIDES_DATE("out of range date for {0} ephemerides: {1}"),
/** OUT_OF_RANGE_DATE. */
OUT_OF_RANGE_DATE("out of range date: {0}, [{1}, {2}]"),
/** OUT_OF_RANGE_EPHEMERIDES_DATE_BEFORE. */
OUT_OF_RANGE_EPHEMERIDES_DATE_BEFORE("out of range date for ephemerides: {0} is {3,number,0.0##############E0} s before [{1}, {2}]"),
/** OUT_OF_RANGE_EPHEMERIDES_DATE_AFTER. */
OUT_OF_RANGE_EPHEMERIDES_DATE_AFTER("out of range date for ephemerides: {0} is {3,number,0.0##############E0} s after [{1}, {2}]"),
/** UNEXPECTED_TWO_ELEVATION_VALUES_FOR_ONE_AZIMUTH. */
UNEXPECTED_TWO_ELEVATION_VALUES_FOR_ONE_AZIMUTH("unexpected two elevation values: {0} and {1}, for one azimuth: {2}"),
/** UNSUPPORTED_PARAMETER_NAME. */
UNSUPPORTED_PARAMETER_NAME("unsupported parameter name {0}, supported names: {1}"),
/** PARAMETER_WITH_SEVERAL_ESTIMATED_VALUES. */
PARAMETER_WITH_SEVERAL_ESTIMATED_VALUES("{0} parameter contains several span in its value TimeSpanMap, the {1} method must be called"),
/** PARAMETER_PERIODS_HAS_ALREADY_BEEN_SET. */
PARAMETER_PERIODS_HAS_ALREADY_BEEN_SET("setPeriod was already called once on {0} parameter, another parameter should be created if the periods have to be changed"),
/** TOO_SMALL_SCALE_FOR_PARAMETER. */
TOO_SMALL_SCALE_FOR_PARAMETER("scale factor for parameter {0} is too small: {1}"),
/** UNKNOWN_ADDITIONAL_STATE. */
UNKNOWN_ADDITIONAL_STATE("unknown additional state \"{0}\""),
/** UNKNOWN_MONTH. */
UNKNOWN_MONTH("unknown month \"{0}\""),
/** SINGULAR_JACOBIAN_FOR_ORBIT_TYPE. */
SINGULAR_JACOBIAN_FOR_ORBIT_TYPE("Jacobian matrix for type {0} is singular with current orbit"),
/** STATE_JACOBIAN_NOT_INITIALIZED. */
STATE_JACOBIAN_NOT_INITIALIZED("state Jacobian has not been initialized yet"),
/** STATE_JACOBIAN_NOT_6X6. */
STATE_JACOBIAN_NOT_6X6("state Jacobian is a {0}x{1} matrix, it should be a 6x6 matrix"),
/** STATE_AND_PARAMETERS_JACOBIANS_ROWS_MISMATCH. */
STATE_AND_PARAMETERS_JACOBIANS_ROWS_MISMATCH("state Jacobian has {0} rows but parameters Jacobian has {1} rows"),
/** INITIAL_MATRIX_AND_PARAMETERS_NUMBER_MISMATCH. */
INITIAL_MATRIX_AND_PARAMETERS_NUMBER_MISMATCH("initial Jacobian matrix has {0} columns, but {1} parameters have been selected"),
/** ORBIT_A_E_MISMATCH_WITH_CONIC_TYPE. */
ORBIT_A_E_MISMATCH_WITH_CONIC_TYPE("orbit should be either elliptic with a > 0 and e < 1 or hyperbolic with a < 0 and e > 1, a = {0}, e = {1}"),
/** ORBIT_ANOMALY_OUT_OF_HYPERBOLIC_RANGE. */
ORBIT_ANOMALY_OUT_OF_HYPERBOLIC_RANGE("true anomaly {0} out of hyperbolic range (e = {1}, {2} < v < {3})"),
/** HYPERBOLIC_ORBIT_NOT_HANDLED_AS. */
HYPERBOLIC_ORBIT_NOT_HANDLED_AS("hyperbolic orbits cannot be handled as {0} instances"),
/** CCSDS_DATE_INVALID_PREAMBLE_FIELD. */
CCSDS_DATE_INVALID_PREAMBLE_FIELD("invalid preamble field in CCSDS date: {0}"),
/** CCSDS_DATE_INVALID_LENGTH_TIME_FIELD. */
CCSDS_DATE_INVALID_LENGTH_TIME_FIELD("invalid time field length in CCSDS date: {0}, expected {1}"),
/** CCSDS_DATE_MISSING_AGENCY_EPOCH. */
CCSDS_DATE_MISSING_AGENCY_EPOCH("missing agency epoch in CCSDS date"),
/** CCSDS_MISSING_KEYWORD. */
CCSDS_MISSING_KEYWORD("missing mandatory key {0} in CCSDS file {1}"),
/** CCSDS_KEYWORD_NOT_ALLOWED_IN_VERSION. */
CCSDS_KEYWORD_NOT_ALLOWED_IN_VERSION("key {0} is not allowed in format version {1}"),
/** CCSDS_UNEXPECTED_KEYWORD. */
CCSDS_UNEXPECTED_KEYWORD("unexpected keyword in CCSDS line number {0} of file {1}:\n{2}"),
/** CCSDS_UNKNOWN_GM. */
CCSDS_UNKNOWN_GM("the central body gravitational coefficient cannot be retrieved from the ODM"),
/** CCSDS_UNKNOWN_SPACECRAFT_MASS. */
CCSDS_UNKNOWN_SPACECRAFT_MASS("there is no spacecraft mass associated with this ODM file"),
/** CCSDS_UNKNOWN_CONVENTIONS. */
CCSDS_UNKNOWN_CONVENTIONS("no IERS conventions have been set before parsing"),
/** CCSDS_INVALID_FRAME. */
CCSDS_INVALID_FRAME("frame {0} is not valid in this CCSDS file context"),
/** CCSDS_DIFFERENT_LVLH_DEFINITION. */
CCSDS_DIFFERENT_LVLH_DEFINITION("this LVLH local orbital frame uses a different definition, please use LVLH_CCSDS instead"),
/** CCSDS_INCONSISTENT_TIME_SYSTEMS. */
CCSDS_INCONSISTENT_TIME_SYSTEMS("inconsistent time systems: {0} ≠ {1}"),
/** CCSDS_TIME_SYSTEM_NOT_IMPLEMENTED. */
CCSDS_TIME_SYSTEM_NOT_IMPLEMENTED("use of time system {0} in CCSDS files requires an additional ICD and is not implemented in Orekit"),
/** CCSDS_TDM_KEYWORD_NOT_FOUND. */
CCSDS_TDM_KEYWORD_NOT_FOUND("No CCSDS TDM keyword was found at line {0} of file {1}:\n{2}"),
/** CCSDS_TDM_MISSING_RANGE_UNITS_CONVERTER. */
CCSDS_TDM_MISSING_RANGE_UNITS_CONVERTER("no Range Units converter configured for parsing Tracking Data Message"),
/** CCSDS_TIME_SYSTEM_NOT_READ_YET. */
CCSDS_TIME_SYSTEM_NOT_READ_YET("Time system should have already been set before line {0} of file {1}"),
/** CCSDS_UNKNOWN_ATTITUDE_TYPE. */
CCSDS_UNKNOWN_ATTITUDE_TYPE("unknown attitude type {0}"),
/** CCSDS_INCOMPLETE_DATA. */
CCSDS_INCOMPLETE_DATA("incomplete data"),
/** CCSDS_INVALID_ROTATION_SEQUENCE. */
CCSDS_INVALID_ROTATION_SEQUENCE("invalid rotation sequence {0} at line {1} of file {2}"),
/** CCSDS_UNSUPPORTED_ELEMENT_SET_TYPE. */
CCSDS_UNSUPPORTED_ELEMENT_SET_TYPE("element set type {0} ({1}) is not supported yet"),
/** CCSDS_UNSUPPORTED_RETROGRADE_EQUINOCTIAL. */
CCSDS_UNSUPPORTED_RETROGRADE_EQUINOCTIAL("retrograde factor not supported in element set {0}"),
/** CCSDS_MANEUVER_UNITS_WRONG_NB_COMPONENTS. */
CCSDS_MANEUVER_UNITS_WRONG_NB_COMPONENTS("wrong number of units for maneuver {0}"),
/** CCSDS_MANEUVER_MISSING_TIME. */
CCSDS_MANEUVER_MISSING_TIME("missing time field for maneuver {0}"),
/** CCSDS_INCONSISTENT_NUMBER_OF_ATTITUDE_STATES. */
CCSDS_INCONSISTENT_NUMBER_OF_ATTITUDE_STATES("attitude type {0} and rate type {1} calls for {2} states, got {3}"),
/** CCSDS_INCOMPATIBLE_KEYS_BOTH_USED. */
CCSDS_INCOMPATIBLE_KEYS_BOTH_USED("incompatible keys {0} and {1} should not both be used"),
/** CCSDS_SENSOR_INDEX_ALREADY_USED. */
CCSDS_SENSOR_INDEX_ALREADY_USED("sensor index {0} is already used"),
/** CCSDS_MISSING_SENSOR_INDEX. */
CCSDS_MISSING_SENSOR_INDEX("missing sensor index {0}"),
/** INCONSISTENT_NUMBER_OF_ELEMENTS. */
INCONSISTENT_NUMBER_OF_ELEMENTS("inconsistent number of elements: expected {0}, got {1}"),
/** CANNOT_ESTIMATE_PRECESSION_WITHOUT_PROPER_DERIVATIVES. */
CANNOT_ESTIMATE_PRECESSION_WITHOUT_PROPER_DERIVATIVES("cannot estimate precession without proper derivatives"),
/** ADDITIONAL_STATE_NAME_ALREADY_IN_USE. */
ADDITIONAL_STATE_NAME_ALREADY_IN_USE("name \"{0}\" is already used for an additional state"),
/** NON_RESETABLE_STATE. */
NON_RESETABLE_STATE("reset state not allowed"),
/** DSST_NEWCOMB_OPERATORS_COMPUTATION. */
DSST_NEWCOMB_OPERATORS_COMPUTATION("Cannot compute Newcomb operators for sigma > rho ({0} > {1})"),
/** DSST_VMNS_COEFFICIENT_ERROR_MS. */
DSST_VMNS_COEFFICIENT_ERROR_MS("Cannot compute the Vmns coefficient with m > n ({0} > {1})"),
/** DSST_SPR_SHADOW_INCONSISTENT. */
DSST_SPR_SHADOW_INCONSISTENT("inconsistent shadow computation: entry = {0} whereas exit = {1}"),
/** DSST_ECC_NO_NUMERICAL_AVERAGING_METHOD. */
DSST_ECC_NO_NUMERICAL_AVERAGING_METHOD("The current orbit has an eccentricity ({0} > 0.5). DSST needs an unimplemented time dependent numerical method to compute the averaged rates"),
/** SP3_UNSUPPORTED_VERSION. */
SP3_UNSUPPORTED_VERSION("unsupported sp3 file version \"{0}\""),
/** SP3_INVALID_HEADER_ENTRY. */
SP3_INVALID_HEADER_ENTRY("invalid header entry {0} \"{1}\" in file {2} (format version {3})"),
/** SP3_TOO_MANY_SATELLITES_FOR_VERSION. */
SP3_TOO_MANY_SATELLITES_FOR_VERSION("version \"{0}\" supports only up to {1} satellites, found {2} in file {3}"),
/** SP3_NUMBER_OF_EPOCH_MISMATCH. */
SP3_NUMBER_OF_EPOCH_MISMATCH("found {0} epochs in file {1}, expected {2}"),
/** SP3_INCOMPATIBLE_FILE_METADATA. */
SP3_INCOMPATIBLE_FILE_METADATA("cannot splice sp3 files with incompatible metadata"),
/** SP3_INCOMPATIBLE_SATELLITE_MEDATADA. */
SP3_INCOMPATIBLE_SATELLITE_MEDATADA("cannot splice sp3 files with incompatible satellite metadata for satellite {0}"),
/** STK_INVALID_OR_UNSUPPORTED_COORDINATE_SYSTEM. */
STK_INVALID_OR_UNSUPPORTED_COORDINATE_SYSTEM("STK coordinate system \"{0}\" is invalid or not yet supported"),
/** STK_UNMAPPED_COORDINATE_SYSTEM. */
STK_UNMAPPED_COORDINATE_SYSTEM("STK coordinate system \"{0}\" has not been mapped to an Orekit frame"),
/** STK_UNEXPECTED_END_OF_FILE. */
STK_UNEXPECTED_END_OF_FILE("unexpected end of STK file (after line {0})"),
/** CLOCK_FILE_UNSUPPORTED_VERSION. */
CLOCK_FILE_UNSUPPORTED_VERSION("unsupported clock file version {0}"),
/** UNSUPPORTED_FILE_FORMAT_VERSION. */
UNSUPPORTED_FILE_FORMAT_VERSION("version {0} from file {1} is not supported, supported version: {2}"),
/** NON_EXISTENT_GEOMAGNETIC_MODEL. */
NON_EXISTENT_GEOMAGNETIC_MODEL("non-existent geomagnetic model {0} for year {1}"),
/** UNSUPPORTED_TIME_TRANSFORM. */
UNSUPPORTED_TIME_TRANSFORM("geomagnetic model {0} with epoch {1} does not support time transformation, no secular variation coefficients defined"),
/** OUT_OF_RANGE_TIME_TRANSFORM. */
OUT_OF_RANGE_TIME_TRANSFORM("time transformation of geomagnetic model {0} with epoch {1} is outside its validity range: {2} != [{3}, {4}]"),
/** NOT_ENOUGH_DATA. */
NOT_ENOUGH_DATA("not enough data (sample size = {0})"),
/** NOT_ENOUGH_CACHED_NEIGHBORS. */
NOT_ENOUGH_CACHED_NEIGHBORS("too small number of cached neighbors: {0} (must be at least {1})"),
/** NO_CACHED_ENTRIES. */
NO_CACHED_ENTRIES("no cached entries"),
/** NON_CHRONOLOGICALLY_SORTED_ENTRIES. */
NON_CHRONOLOGICALLY_SORTED_ENTRIES("generated entries not sorted: {0} > {1} by {2,number,0.0##############E0} s"),
/** NO_DATA_GENERATED. */
NO_DATA_GENERATED("no data generated around date: {0}"),
/** UNABLE_TO_GENERATE_NEW_DATA_BEFORE. */
UNABLE_TO_GENERATE_NEW_DATA_BEFORE("unable to generate new data before {0}, but data is requested for {1} which is {2,number,0.0##############E0} s before"),
/** UNABLE_TO_GENERATE_NEW_DATA_AFTER. */
UNABLE_TO_GENERATE_NEW_DATA_AFTER("unable to generate new data after {0}, but data is requested for {1} which is {2,number,0.0##############E0} s after"),
/** UNABLE_TO_COMPUTE_HYPERBOLIC_ECCENTRIC_ANOMALY. */
UNABLE_TO_COMPUTE_HYPERBOLIC_ECCENTRIC_ANOMALY("unable to compute hyperbolic eccentric anomaly from the mean anomaly after {0} iterations"),
/** UNABLE_TO_COMPUTE_ECCENTRIC_LONGITUDE_ARGUMENT. */
UNABLE_TO_COMPUTE_ECCENTRIC_LONGITUDE_ARGUMENT("unable to compute eccentric longitude argument from the mean one after {0} iterations"),
/** UNABLE_TO_COMPUTE_ECCENTRIC_LATITUDE_ARGUMENT. */
UNABLE_TO_COMPUTE_ECCENTRIC_LATITUDE_ARGUMENT("unable to compute eccentric latitude argument from the mean one after {0} iterations"),
/** UNABLE_TO_COMPUTE_DSST_MEAN_PARAMETERS. */
UNABLE_TO_COMPUTE_DSST_MEAN_PARAMETERS("unable to compute mean orbit from osculating orbit after {0} iterations"),
/** OUT_OF_RANGE_DERIVATION_ORDER. */
OUT_OF_RANGE_DERIVATION_ORDER("derivation order {0} is out of range"),
/** ORBIT_TYPE_NOT_ALLOWED. */
ORBIT_TYPE_NOT_ALLOWED("orbit type {0} not allowed here, allowed types: {1}"),
/** NON_PSEUDO_INERTIAL_FRAME_NOT_SUITABLE_AS_REFERENCE_FOR_INERTIAL_FORCES. */
NON_PSEUDO_INERTIAL_FRAME_NOT_SUITABLE_AS_REFERENCE_FOR_INERTIAL_FORCES("non pseudo-inertial frame {0} is not suitable as reference for inertial forces"),
/** METHOD_NOT_AVAILABLE_WITHOUT_CENTRAL_BODY. */
METHOD_NOT_AVAILABLE_WITHOUT_CENTRAL_BODY("method not available in the absence of a central body"),
/** INCOMPATIBLE_FRAMES. */
INCOMPATIBLE_FRAMES("operation not available between frames {0} and {1}"),
/** UNDEFINED_ORBIT. */
UNDEFINED_ORBIT("orbit not defined, state rather contains an absolute position-velocity-acceleration"),
/** UNDEFINED_ABSOLUTE_PVCOORDINATES. */
UNDEFINED_ABSOLUTE_PVCOORDINATES("absolute position-velocity-acceleration not defined, state rather contains an orbit"),
/** INERTIAL_FORCE_MODEL_MISSING. */
INERTIAL_FORCE_MODEL_MISSING("an inertial force model has to be used when propagating in non-inertial frame {0}"),
/** NO_SEM_ALMANAC_AVAILABLE. */
NO_SEM_ALMANAC_AVAILABLE("no SEM almanac file found"),
/** NOT_A_SUPPORTED_SEM_ALMANAC_FILE. */
NOT_A_SUPPORTED_SEM_ALMANAC_FILE("file {0} is not a supported SEM almanac file"),
/** NO_YUMA_ALMANAC_AVAILABLE. */
NO_YUMA_ALMANAC_AVAILABLE("no Yuma almanac file found"),
/** NOT_A_SUPPORTED_YUMA_ALMANAC_FILE. */
NOT_A_SUPPORTED_YUMA_ALMANAC_FILE("file {0} is not a supported Yuma almanac file"),
/** NOT_ENOUGH_GNSS_FOR_DOP. */
NOT_ENOUGH_GNSS_FOR_DOP("only {0} GNSS orbits are provided while {1} are needed to compute the DOP"),
/** NOT_ENOUGH_PROPAGATORS. */
NOT_ENOUGH_PROPAGATORS("Creating an aggregate propagator requires at least one constituent propagator, but none were provided."),
/** NOT_ENOUGH_ATTITUDE_PROVIDERS. */
NOT_ENOUGH_ATTITUDE_PROVIDERS("Creating an aggregate attitude provider requires at least one constituent attitude provider, but none were provided."),
/** NULL_ARGUMENT. */
NULL_ARGUMENT("argument {0} cannot be null"),
/** VALUE_NOT_FOUND. */
VALUE_NOT_FOUND("value {0} not found in {1}"),
/** KLOBUCHAR_ALPHA_BETA_NOT_LOADED. */
KLOBUCHAR_ALPHA_BETA_NOT_LOADED("Klobuchar coefficients α or β could not be loaded from {0}"),
/** KLOBUCHAR_ALPHA_BETA_NOT_AVAILABLE_FOR_DATE. */
KLOBUCHAR_ALPHA_BETA_NOT_AVAILABLE_FOR_DATE("Klobuchar coefficients α or β not available for date {0}"),
/** NO_KLOBUCHAR_ALPHA_BETA_IN_FILE. */
NO_KLOBUCHAR_ALPHA_BETA_IN_FILE("file {0} does not contain Klobuchar coefficients α or β"),
/** NO_REFERENCE_DATE_FOR_PARAMETER. */
NO_REFERENCE_DATE_FOR_PARAMETER("no reference date set for parameter {0}"),
/** STATION_NOT_FOUND. */
STATION_NOT_FOUND("station {0} not found, known stations: {1}"),
/** UNKNOWN_SATELLITE_SYSTEM. */
UNKNOWN_SATELLITE_SYSTEM("unknown satellite system {0}"),
/** UNKNOWN_TIME_SYSTEM. */
UNKNOWN_TIME_SYSTEM("unknown time system {0}"),
/** UNKNOWN_UTC_ID. */
UNKNOWN_UTC_ID("unknown UTC Id {0}"),
/** UNKNOWN_CLOCK_DATA_TYPE. */
UNKNOWN_CLOCK_DATA_TYPE("unknown clock data type {0}"),
/** UNKNOWN_SATELLITE_ANTENNA_CODE. */
UNKNOWN_SATELLITE_ANTENNA_CODE("unknown satellite antenna code {0}"),
/** UNSUPPORTED_FREQUENCY_FOR_ANTENNA. */
UNSUPPORTED_FREQUENCY_FOR_ANTENNA("frequency {0} is not supported by antenna {1}"),
/** CANNOT_FIND_SATELLITE_IN_SYSTEM. */
CANNOT_FIND_SATELLITE_IN_SYSTEM("cannot find satellite {0} in satellite system {1}"),
/** UNKNOWN_RINEX_FREQUENCY. */
UNKNOWN_RINEX_FREQUENCY("unknown RINEX frequency {0} in file {1}, line {2}"),
/** MISMATCHED_FREQUENCIES. */
MISMATCHED_FREQUENCIES("mismatched frequencies in file {0}, line {1} (expected {2}, got {3})"),
/** WRONG_PARSING_TYPE. */
WRONG_PARSING_TYPE("wrong parsing type for file {0}"),
/** WRONG_COLUMNS_NUMBER. */
WRONG_COLUMNS_NUMBER("wrong number of columns in file {0}, line {1} (expected {2} columns, got {3} columns)"),
/** UNSUPPORTED_FILE_FORMAT. */
UNSUPPORTED_FILE_FORMAT("unsupported format for file {0}"),
/** INCOMPLETE_HEADER. */
INCOMPLETE_HEADER("incomplete header in file {0}"),
/** INCONSISTENT_NUMBER_OF_SATS. */
INCONSISTENT_NUMBER_OF_SATS("inconsistent number of satellites in line {0}, file {1}: observation with {2} satellites and number of max satellites is {3}"),
/** INCONSISTENT_SATELLITE_SYSTEM. */
INCONSISTENT_SATELLITE_SYSTEM("the satellite system {3} from line {0}, file {1} is not consistent with the Rinex Satellite System {2} in header"),
/** NO_PROPAGATOR_CONFIGURED. */
NO_PROPAGATOR_CONFIGURED("no propagator configured"),
/** DIMENSION_INCONSISTENT_WITH_PARAMETERS. */
DIMENSION_INCONSISTENT_WITH_PARAMETERS("dimension {0} is inconsistent with parameters list: {1}"),
/** NOT_A_SUPPORTED_UNIX_COMPRESSED_FILE. */
NOT_A_SUPPORTED_UNIX_COMPRESSED_FILE("file {0} is not a supported Unix-compressed file"),
/** UNEXPECTED_END_OF_FILE. */
UNEXPECTED_END_OF_FILE("unexpected end of file {0}"),
/** CORRUPTED_FILE. */
CORRUPTED_FILE("file {0} is corrupted"),
/** VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_LOADED. */
VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_LOADED("Vienna coefficients ah or aw or zh or zw could not be loaded from {0}"),
/** VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_AVAILABLE_FOR_DATE. */
VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_AVAILABLE_FOR_DATE("Vienna coefficients ah or aw or zh or zw not available for date {0}"),
/** NO_VIENNA_ACOEF_OR_ZENITH_DELAY_IN_FILE. */
NO_VIENNA_ACOEF_OR_ZENITH_DELAY_IN_FILE("file {0} does not contain Vienna coefficients ah, aw, zh or zw"),
/** IRREGULAR_OR_INCOMPLETE_GRID. */
IRREGULAR_OR_INCOMPLETE_GRID("irregular or incomplete grid in file {0}"),
/** INVALID_SATELLITE_SYSTEM. */
INVALID_SATELLITE_SYSTEM("invalid satellite system {0}"),
/** NO_TEC_DATA_IN_FILES_FOR_DATE. */
NO_TEC_DATA_IN_FILES_FOR_DATE("IONEX files {0} does not contain TEC data for date {1}"),
/** INCONSISTENT_NUMBER_OF_TEC_MAPS_IN_FILE. */
INCONSISTENT_NUMBER_OF_TEC_MAPS_IN_FILE("number of maps {0} is inconsistent with header specification: {1}"),
/** NO_LATITUDE_LONGITUDE_BONDARIES_IN_IONEX_HEADER. */
NO_LATITUDE_LONGITUDE_BONDARIES_IN_IONEX_HEADER("file {0} does not contain latitude or longitude bondaries in its header section"),
/** NO_EPOCH_IN_IONEX_HEADER. */
NO_EPOCH_IN_IONEX_HEADER("file {0} does not contain epoch of first or last map in its header section"),
/** ITRF_VERSIONS_PREFIX_ONLY. */
ITRF_VERSIONS_PREFIX_ONLY("The first column of itrf-versions.conf is a plain prefix that is matched against the name of each loaded file. It should not contain any regular expression syntax or directory components, i.e. \"/\" or \"\\\". Actual value: \"{0}\"."),
/** CANNOT_COMPUTE_AIMING_AT_SINGULAR_POINT. */
CANNOT_COMPUTE_AIMING_AT_SINGULAR_POINT("cannot compute aiming direction at singular point: latitude = {0}, longitude = {1}"),
/** STEC_INTEGRATION_DID_NOT_CONVERGE. */
STEC_INTEGRATION_DID_NOT_CONVERGE("STEC integration did not converge"),
/** MODIP_GRID_NOT_LOADED. */
MODIP_GRID_NOT_LOADED("MODIP grid not be loaded from {0}"),
/** NEQUICK_F2_FM3_NOT_LOADED. */
NEQUICK_F2_FM3_NOT_LOADED("NeQuick coefficient f2 or fm3 not be loaded from {0}"),
/** NOT_A_SUPPORTED_HATANAKA_COMPRESSED_FILE. */
NOT_A_SUPPORTED_HATANAKA_COMPRESSED_FILE("file {0} is not a supported Hatanaka-compressed file"),
/** CANNOT_COMPUTE_LAGRANGIAN. */
CANNOT_COMPUTE_LAGRANGIAN("Cannot compute around {0}"),
/** TRAJECTORY_NOT_CROSSING_XZPLANE. */
TRAJECTORY_NOT_CROSSING_XZPLANE("The trajectory does not cross XZ Plane, it will not result in a Halo Orbit"),
/** MULTIPLE_SHOOTING_UNDERCONSTRAINED. */
MULTIPLE_SHOOTING_UNDERCONSTRAINED("The multiple shooting problem is underconstrained : {0} free variables, {1} constraints"),
/** INVALID_MEASUREMENT_TYPES_FOR_COMBINATION_OF_MEASUREMENTS. */
INVALID_MEASUREMENT_TYPES_FOR_COMBINATION_OF_MEASUREMENTS("invalid measurement types {0} and {1} for the combination of measurements {2}"),
/** INCOMPATIBLE_FREQUENCIES_FOR_COMBINATION_OF_MEASUREMENTS. */
INCOMPATIBLE_FREQUENCIES_FOR_COMBINATION_OF_MEASUREMENTS("frequencies {0} and {1} are incompatibles for the {2} combination"),
/** NON_CHRONOLOGICAL_DATES_FOR_OBSERVATIONS. */
NON_CHRONOLOGICAL_DATES_FOR_OBSERVATIONS("observations are not in chronological order: {0} is {2,number,0.0##############E0} s after {1}"),
/** INCONSISTENT_SAMPLING_DATE. */
INCONSISTENT_SAMPLING_DATE("inconsistent sampling date: expected {0} but got {1}"),
/** EXCEPTIONAL_DATA_CONTEXT. */
EXCEPTIONAL_DATA_CONTEXT("Use of the ExceptionalDataContext detected. This is typically used to detect developer errors."),
/** NON_DIFFERENT_DATES_FOR_OBSERVATIONS. */
NON_DIFFERENT_DATES_FOR_OBSERVATIONS("Observations must have different dates: {0}, {1} ({3,number,0.0##############E0} s from first observation), and {2} ({4,number,0.0##############E0} s from first observation, {5,number,0.0##############E0} s from second observation)"),
/** NON_COPLANAR_POINTS. */
NON_COPLANAR_POINTS("observations are not in the same plane"),
/** INVALID_PARAMETER_RANGE. */
INVALID_PARAMETER_RANGE("invalid parameter {0}: {1} not in range [{2}, {3}]"),
/** PARAMETER_NOT_SET. */
PARAMETER_NOT_SET("The parameter {0} should not be null in {1}"),
/** FUNCTION_NOT_IMPLEMENTED. */
FUNCTION_NOT_IMPLEMENTED("{0} is not implemented"),
/** INVALID_TYPE_FOR_FUNCTION. */
INVALID_TYPE_FOR_FUNCTION("Impossible to execute {0} with {1} set to {2}"),
/** NO_DATA_IN_FILE. */
NO_DATA_IN_FILE("No data could be parsed from file {0}"),
/** CPF_UNEXPECTED_END_OF_FILE. */
CPF_UNEXPECTED_END_OF_FILE("Unexpected end of CPF file (after line {0})"),
/** UNEXPECTED_FORMAT_FOR_ILRS_FILE. */
UNEXPECTED_FORMAT_FOR_ILRS_FILE("Unexpected file format. Must be {0} but is {1}"),
/** CRD_UNEXPECTED_END_OF_FILE. */
CRD_UNEXPECTED_END_OF_FILE("Unexpected end of CRD file (after line {0})"),
/** INVALID_RANGE_INDICATOR_IN_CRD_FILE. */
INVALID_RANGE_INDICATOR_IN_CRD_FILE("Invalid range indicator {0} in CRD file header"),
/** END_OF_ENCODED_MESSAGE. */
END_OF_ENCODED_MESSAGE("end of encoded message reached"),
/** TOO_LARGE_DATA_TYPE. */
TOO_LARGE_DATA_TYPE("too large data type ({0} bits)"),
/** UNKNOWN_ENCODED_MESSAGE_NUMBER. */
UNKNOWN_ENCODED_MESSAGE_NUMBER("unknown encoded message number {0}"),
/** UNKNOWN_AUTHENTICATION_METHOD. */
UNKNOWN_AUTHENTICATION_METHOD("unknown authentication method: {0}"),
/** UNKNOWN_CARRIER_PHASE_CODE. */
UNKNOWN_CARRIER_PHASE_CODE("unknown carrier phase code: {0}"),
/** UNKNOWN_DATA_FORMAT. */
UNKNOWN_DATA_FORMAT("unknown data format: {0}"),
/** UNKNOWN_NAVIGATION_SYSTEM. */
UNKNOWN_NAVIGATION_SYSTEM("unknown navigation system: {0}"),
/** STREAM_REQUIRES_NMEA_FIX. */
STREAM_REQUIRES_NMEA_FIX("data stream {0} requires a NMEA fix data"),
/** FAILED_AUTHENTICATION. */
FAILED_AUTHENTICATION("failed authentication for mountpoint {0}"),
/** CONNECTION_ERROR. */
CONNECTION_ERROR("error connecting to {0}: {1}"),
/** UNEXPECTED_CONTENT_TYPE. */
UNEXPECTED_CONTENT_TYPE("unexpected content type {0}"),
/** CANNOT_PARSE_GNSS_DATA. */
CANNOT_PARSE_GNSS_DATA("cannot parse GNSS data from {0}"),
/** INVALID_GNSS_DATA. */
INVALID_GNSS_DATA("invalid GNSS data: {0}"),
/** GNSS_PARITY_ERROR. */
GNSS_PARITY_ERROR("GNSS parity error on word {0}"),
/** UNKNOWN_HOST. */
UNKNOWN_HOST("unknown host {0}"),
/** SOURCETABLE_PARSE_ERROR. */
SOURCETABLE_PARSE_ERROR("error parsing sourcetable line {0} from {1}: {2}"),
/** CANNOT_PARSE_SOURCETABLE. */
CANNOT_PARSE_SOURCETABLE("cannot parse sourcetable from {0}"),
/** MOUNPOINT_ALREADY_CONNECTED. */
MOUNPOINT_ALREADY_CONNECTED("mount point {0} is already connected"),
/** MISSING_HEADER. */
MISSING_HEADER("missing header from {0}: {1}"),
/** NOT_VALID_INTERNATIONAL_DESIGNATOR. */
NOT_VALID_INTERNATIONAL_DESIGNATOR("{0} is not a valid international designator"),
/** UNINITIALIZED_VALUE_FOR_KEY. */
UNINITIALIZED_VALUE_FOR_KEY("value for key {0} has not been initialized"),
/** UNKNOWN_UNIT. */
UNKNOWN_UNIT("unknown unit {0}"),
/** INCOMPATIBLE_UNITS. */
INCOMPATIBLE_UNITS("units {0} and {1} are not compatible"),
/** MISSING_VELOCITY. */
MISSING_VELOCITY("missing velocity data"),
/** ATTEMPT_TO_GENERATE_MALFORMED_FILE. */
ATTEMPT_TO_GENERATE_MALFORMED_FILE("attempt to generate file {0} with a formatting error"),
/** FIND_ROOT. */
FIND_ROOT("{0} failed to find root between {1} (g={2,number,0.0##############E0}) and {3} (g={4,number,0.0##############E0})\nLast iteration at {5} (g={6,number,0.0##############E0})"),
/** MISSING_STATION_DATA_FOR_EPOCH. */
MISSING_STATION_DATA_FOR_EPOCH("missing station data for epoch {0}"),
/** INCONSISTENT_SELECTION. */
INCONSISTENT_SELECTION("inconsistent parameters selection between pairs {0}/{1} and {2}/{3}"),
/** NO_UNSCENTED_TRANSFORM_CONFIGURED. */
NO_UNSCENTED_TRANSFORM_CONFIGURED("no unscented transform configured"),
/** NOT_STRICTLY_POSITIVE. */
NOT_STRICTLY_POSITIVE("value is not strictly positive: {0}"),
/** UNSUPPORTED_TRANSFORM. */
UNSUPPORTED_TRANSFORM("transform from {0} to {1} is not implemented"),
/** WRONG_ORBIT_PARAMETERS_TYPE. */
WRONG_ORBIT_PARAMETERS_TYPE("orbital parameters type: {0} is different from expected orbital type : {1}"),
/** WRONG_NB_COMPONENTS. */
WRONG_NB_COMPONENTS("{0} expects {1} elements, got {2}"),
/** CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_LOF. */
CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_LOF("cannot change covariance type if defined in a local orbital frame"),
/** CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_NON_INERTIAL_FRAME. */
CANNOT_CHANGE_COVARIANCE_TYPE_IF_DEFINED_IN_NON_INERTIAL_FRAME("cannot change covariance type if defined in a non pseudo-inertial reference frame"),
/** DIFFERENT_TIME_OF_CLOSEST_APPROACH. */
DIFFERENT_TIME_OF_CLOSEST_APPROACH("primary collision object time of closest approach is different from the secondary collision object's one"),
/** DATES_MISMATCH. */
DATES_MISMATCH("first date {0} does not match second date {1}"),
/** WRONG ELEMENTS FOR AVERAGING THEORY. */
WRONG_ELEMENTS_FOR_AVERAGING_THEORY("unexpected type of orbital elements for required averaging theory"),
/** ORBITS_MUS_MISMATCH. */
ORBITS_MUS_MISMATCH("first orbit mu {0} does not match second orbit mu {1}"),
/** DIFFERENT_STATE_DEFINITION. */
DIFFERENT_STATE_DEFINITION("one state is defined using an orbit while the other is defined using an absolute position-velocity-acceleration"),
/** STATE_AND_COVARIANCE_DATES_MISMATCH. */
STATE_AND_COVARIANCE_DATES_MISMATCH("state date {0} does not match its covariance date {1}"),
/** NO_INTERPOLATOR_FOR_STATE_DEFINITION. */
NO_INTERPOLATOR_FOR_STATE_DEFINITION("creating a spacecraft state interpolator requires at least one orbit interpolator or an absolute position-velocity-acceleration interpolator"),
/** WRONG_INTERPOLATOR_DEFINED_FOR_STATE_INTERPOLATION. */
WRONG_INTERPOLATOR_DEFINED_FOR_STATE_INTERPOLATION("wrong interpolator defined for this spacecraft state type (orbit or absolute PV)"),
/** MULTIPLE_INTERPOLATOR_USED. */
MULTIPLE_INTERPOLATOR_USED("multiple interpolators are used so they may use different numbers of interpolation points"),
/** HEADER_NOT_WRITTEN. */
HEADER_NOT_WRITTEN("header for file {0} has not been written yet"),
/** HEADER_ALREADY_WRITTEN. */
HEADER_ALREADY_WRITTEN("header for file {0} has already been written"),
/** CANNOT_START_PROPAGATION_FROM_INFINITY. */
CANNOT_START_PROPAGATION_FROM_INFINITY("Cannot start the propagation from an infinitely far date"),
/** TOO_LONG_TIME_GAP_BETWEEN_DATA_POINTS. */
TOO_LONG_TIME_GAP_BETWEEN_DATA_POINTS("Too long time gap between data points: {0} s"),
/** INVALID_SATELLITE_ID. */
INVALID_SATELLITE_ID("invalid satellite id {0}"),
/** WRONG_EOP_INTERPOLATION_DEGREE. */
WRONG_EOP_INTERPOLATION_DEGREE("EOP interpolation degree must be of the form 4k-1, got {0}"),
/** WALKER_INCONSISTENT_PLANES. */
WALKER_INCONSISTENT_PLANES("number of planes {0} is inconsistent with number of satellites {1} in Walker constellation");
/** Base name of the resource bundle in classpath. */
private static final String RESOURCE_BASE_NAME = "assets/org/orekit/localization/OrekitMessages";
/** Source English format. */
private final String sourceFormat;
/**
* Simple constructor.
* @param sourceFormat source English format to use when no localized version is
* available
*/
OrekitMessages(final String sourceFormat) {
this.sourceFormat = sourceFormat;
}
/** {@inheritDoc} */
public String getSourceString() {
return sourceFormat;
}
/** {@inheritDoc} */
public String getLocalizedString(final Locale locale) {
try {
final ResourceBundle bundle = ResourceBundle.getBundle(RESOURCE_BASE_NAME, locale, new UTF8Control());
if (bundle.getLocale().getLanguage().equals(locale.getLanguage())) {
final String translated = bundle.getString(name());
if (!(translated.isEmpty() || translated.toLowerCase().contains("missing translation"))) {
// the value of the resource is the translated format
return translated;
}
}
} catch (MissingResourceException mre) {
// do nothing here
}
// either the locale is not supported or the resource is not translated or
// it is unknown: don't translate and fall back to using the source format
return sourceFormat;
}
}