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17 package org.orekit.errors;
18
19 import java.io.IOException;
20 import java.io.InputStream;
21 import java.io.InputStreamReader;
22 import java.net.URL;
23 import java.net.URLConnection;
24 import java.nio.charset.StandardCharsets;
25 import java.util.Locale;
26 import java.util.MissingResourceException;
27 import java.util.PropertyResourceBundle;
28 import java.util.ResourceBundle;
29
30 import org.hipparchus.exception.Localizable;
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46 public enum OrekitMessages implements Localizable {
47
48
49
50 INTERNAL_ERROR("internal error, please notify development team by creating a new topic at {0}"),
51 ALTITUDE_BELOW_ALLOWED_THRESHOLD("altitude ({0} m) is below the {1} m allowed threshold"),
52 POINT_INSIDE_ELLIPSOID("point is inside ellipsoid"),
53 TRAJECTORY_INSIDE_BRILLOUIN_SPHERE("trajectory inside the Brillouin sphere (r = {0})"),
54 ALMOST_EQUATORIAL_ORBIT("almost equatorial orbit (i = {0} degrees)"),
55 ALMOST_CRITICALLY_INCLINED_ORBIT("almost critically inclined orbit (i = {0} degrees)"),
56 UNABLE_TO_COMPUTE_ECKSTEIN_HECHLER_MEAN_PARAMETERS(
57 "unable to compute Eckstein-Hechler mean parameters after {0} iterations"),
58 UNABLE_TO_COMPUTE_BROUWER_LYDDANE_MEAN_PARAMETERS(
59 "unable to compute Brouwer-Lyddane mean parameters after {0} iterations"),
60 UNABLE_TO_COMPUTE_TLE(
61 "unable to compute TLE after {0} iterations"),
62 NULL_PARENT_FOR_FRAME("null parent for frame {0}"),
63 FRAME_ALREADY_ATTACHED("frame {0} is already attached to frame {1}"),
64 FRAME_NOT_ATTACHED("frame {0} is not attached to the main frames tree"),
65 FRAME_ANCESTOR_OF_BOTH_FRAMES("frame {0} is an ancestor of both frames {1} and {2}"),
66 FRAME_ANCESTOR_OF_NEITHER_FRAME("frame {0} is an ancestor of neither frame {1} nor {2}"),
67 FRAME_NO_NTH_ANCESTOR("frame {0} has depth {1}, it cannot have an ancestor {2} levels above"),
68 NO_SUCH_ITRF_FRAME("ITRF frame {0} not found"),
69 UNSUPPORTED_LOCAL_ORBITAL_FRAME("unsupported local orbital frame {0}"),
70 NON_PSEUDO_INERTIAL_FRAME("non pseudo-inertial frame \"{0}\""),
71 DATA_ROOT_DIRECTORY_DOES_NOT_EXIST("data root directory {0} does not exist"),
72 NOT_A_DIRECTORY("{0} is not a directory"),
73 NEITHER_DIRECTORY_NOR_ZIP_OR_JAR("{0} is neither a directory nor a zip/jar archive file"),
74 UNABLE_TO_FIND_RESOURCE("unable to find resource {0} in classpath"),
75 NO_EARTH_ORIENTATION_PARAMETERS_LOADED("no Earth Orientation Parameters loaded"),
76 MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES("missing Earth Orientation Parameters between {0} and {1}"),
77 MISSING_EARTH_ORIENTATION_PARAMETERS_BETWEEN_DATES_GAP("missing Earth Orientation Parameters between {0} and {1}, gap is {2,number,0.0##############E0} s"),
78 NO_EARTH_ORIENTATION_PARAMETERS("missing Earth Orientation Parameters"),
79 NOT_A_SUPPORTED_IERS_DATA_FILE("file {0} is not a supported IERS data file"),
80 INCONSISTENT_DATES_IN_IERS_FILE("inconsistent dates in IERS file {0}: {1}-{2}-{3} and MJD {4}"),
81 UNEXPECTED_DATA_AFTER_LINE_IN_FILE("unexpected data after line {0} in file {1}: {2}"),
82 UNEXPECTED_DATA_AT_LINE_IN_FILE("unexpected data at line {0} in file {1}"),
83 NON_CHRONOLOGICAL_DATES_IN_FILE("non-chronological dates in file {0}, line {1}"),
84 NO_IERS_UTC_TAI_HISTORY_DATA_LOADED("no IERS UTC-TAI history data loaded"),
85 NO_ENTRIES_IN_IERS_UTC_TAI_HISTORY_FILE("no entries found in IERS UTC-TAI history file {0}"),
86 MISSING_SERIE_J_IN_FILE("missing serie j = {0} in file {1} (line {2})"),
87 CANNOT_PARSE_BOTH_TAU_AND_GAMMA("cannot parse both τ and γ from the same Poissons series file"),
88 UNEXPECTED_END_OF_FILE_AFTER_LINE("unexpected end of file {0} (after line {1})"),
89 UNABLE_TO_PARSE_LINE_IN_FILE("unable to parse line {0} of file {1}:\n{2}"),
90 UNABLE_TO_PARSE_ELEMENT_IN_FILE("unable to parse element {0} at line {1}, file {2}"),
91 UNABLE_TO_FIND_FILE("unable to find file {0}"),
92 SPACECRAFT_MASS_BECOMES_NEGATIVE("spacecraft mass becomes negative: {0} kg"),
93 POSITIVE_FLOW_RATE("positive flow rate (q: {0})"),
94 NO_GRAVITY_FIELD_DATA_LOADED("no gravity field data loaded"),
95 GRAVITY_FIELD_NORMALIZATION_UNDERFLOW("gravity field normalization underflow for degree {0} and order {1}"),
96 NO_OCEAN_TIDE_DATA_LOADED("no ocean tide data loaded"),
97 OCEAN_TIDE_DATA_DEGREE_ORDER_LIMITS("ocean tide data file {0} limited to degree {1} and order {2}"),
98 OCEAN_TIDE_LOAD_DEFORMATION_LIMITS(
99 "load deformation coefficients limited to degree {0}, cannot parse degree {1} term from file {2}"),
100 POLAR_TRAJECTORY("polar trajectory (distance to polar axis: {0})"),
101 UNEXPECTED_FILE_FORMAT_ERROR_FOR_LOADER("unexpected format error for file {0} with loader {1}"),
102 DUPLICATED_GRAVITY_FIELD_COEFFICIENT_IN_FILE("duplicated gravity field coefficient {0}({1}, {2}) in file {3}"),
103 MISSING_GRAVITY_FIELD_COEFFICIENT_IN_FILE("missing gravity field coefficient {0}({1}, {2}) in file {3}"),
104 TOO_LARGE_DEGREE_FOR_GRAVITY_FIELD("too large degree (n = {0}, potential maximal degree is {1})"),
105 TOO_LARGE_ORDER_FOR_GRAVITY_FIELD("too large order (m = {0}, potential maximal order is {1})"),
106 WRONG_DEGREE_OR_ORDER("no term ({0}, {1}) in a {2}x{3} spherical harmonics decomposition"),
107 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}"),
108 NO_TLE_FOR_OBJECT("no TLE data available for object {0}"),
109 NO_TLE_FOR_LAUNCH_YEAR_NUMBER_PIECE(
110 "no TLE data available for launch year {0}, launch number {1}, launch piece {2}"),
111 NOT_TLE_LINES("lines {0} and {1} are not TLE lines:\n{0}: \"{2}\"\n{1}: \"{3}\""),
112 MISSING_SECOND_TLE_LINE("expected a second TLE line after line {0}:\n{0}: \"{1}\""),
113 TLE_LINES_DO_NOT_REFER_TO_SAME_OBJECT("TLE lines do not refer to the same object:\n{0}\n{1}"),
114 TLE_INVALID_PARAMETER("invalid TLE parameter for object {0}: {1} = {2}"),
115 TLE_CHECKSUM_ERROR("wrong checksum of TLE line {0}, expected {1} but got {2} ({3})"),
116 NO_TLE_DATA_AVAILABLE("no TLE data available"),
117 NOT_POSITIVE_SPACECRAFT_MASS("spacecraft mass is not positive: {0} kg"),
118 TOO_LARGE_ECCENTRICITY_FOR_PROPAGATION_MODEL("too large eccentricity for propagation model: e = {0}"),
119 NO_SOLAR_ACTIVITY_AT_DATE("no solar activity available at {0}, data available only in range [{1}, {2}]"),
120 NON_EXISTENT_MONTH("non-existent month {0}"),
121 NON_EXISTENT_YEAR_MONTH_DAY("non-existent date {0}-{1}-{2}"),
122 NON_EXISTENT_WEEK_DATE("non-existent week date {0}-W{1}-{2}"),
123 NON_EXISTENT_DATE("non-existent date {0}"),
124 NON_EXISTENT_DAY_NUMBER_IN_YEAR("no day number {0} in year {1}"),
125 NON_EXISTENT_HMS_TIME("non-existent time {0}:{1}:{2}"),
126 NON_EXISTENT_TIME("non-existent time {0}"),
127 OUT_OF_RANGE_SECONDS_NUMBER("out of range seconds number: {0}"),
128 OUT_OF_RANGE_SECONDS_NUMBER_DETAIL("out of range seconds number: {0} is not in [{1}, {2}]"),
129 ANGLE_TYPE_NOT_SUPPORTED("angle type not supported, supported angles: {0}, {1} and {2}"),
130 SATELLITE_COLLIDED_WITH_TARGET("satellite collided with target"),
131 ATTITUDE_POINTING_LAW_DOES_NOT_POINT_TO_GROUND("attitude pointing law misses ground"),
132 TOO_SHORT_TRANSITION_TIME_FOR_ATTITUDES_SWITCH(
133 "{0} seconds transition time for attitudes switch is too short, should be longer than {1} seconds"),
134 ORBIT_AND_ATTITUDE_DATES_MISMATCH("orbit date ({0}) does not match attitude date ({1})"),
135 FRAMES_MISMATCH("frame {0} does not match frame {1}"),
136 INITIAL_STATE_NOT_SPECIFIED_FOR_ORBIT_PROPAGATION("initial state not specified for orbit propagation"),
137 EVENT_DATE_TOO_CLOSE(
138 "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"),
139 UNABLE_TO_READ_JPL_HEADER("unable to read header record from JPL ephemerides binary file {0}"),
140 INCONSISTENT_ASTRONOMICAL_UNIT_IN_FILES(
141 "inconsistent values of astronomical unit in JPL ephemerides files: ({0} and {1})"),
142 INCONSISTENT_EARTH_MOON_RATIO_IN_FILES(
143 "inconsistent values of Earth/Moon mass ratio in JPL ephemerides files: ({0} and {1})"),
144 NO_DATA_LOADED_FOR_CELESTIAL_BODY("no data loaded for celestial body {0}"),
145 NOT_A_JPL_EPHEMERIDES_BINARY_FILE("file {0} is not a JPL ephemerides binary file"),
146 NOT_A_MARSHALL_SOLAR_ACTIVITY_FUTURE_ESTIMATION_FILE(
147 "file {0} is not a Marshall Solar Activity Future Estimation (MSAFE) file"),
148 NO_JPL_EPHEMERIDES_BINARY_FILES_FOUND("no JPL ephemerides binary files found"),
149 OUT_OF_RANGE_BODY_EPHEMERIDES_DATE("out of range date for {0} ephemerides: {1}"),
150 OUT_OF_RANGE_EPHEMERIDES_DATE("out of range date for ephemerides: {0}, [{1}, {2}]"),
151 OUT_OF_RANGE_EPHEMERIDES_DATE_BEFORE("out of range date for ephemerides: {0} is {3,number,0.0##############E0} s before [{1}, {2}]"),
152 OUT_OF_RANGE_EPHEMERIDES_DATE_AFTER("out of range date for ephemerides: {0} is {3,number,0.0##############E0} s after [{1}, {2}]"),
153 UNEXPECTED_TWO_ELEVATION_VALUES_FOR_ONE_AZIMUTH(
154 "unexpected two elevation values: {0} and {1}, for one azimuth: {2}"),
155 UNSUPPORTED_PARAMETER_NAME("unsupported parameter name {0}, supported names: {1}"),
156 TOO_SMALL_SCALE_FOR_PARAMETER("scale factor for parameter {0} is too small: {1}"),
157 UNKNOWN_ADDITIONAL_STATE("unknown additional state \"{0}\""),
158 UNKNOWN_MONTH("unknown month \"{0}\""),
159 SINGULAR_JACOBIAN_FOR_ORBIT_TYPE("Jacobian matrix for type {0} is singular with current orbit"),
160 STATE_JACOBIAN_NOT_INITIALIZED("state Jacobian has not been initialized yet"),
161 STATE_JACOBIAN_NOT_6X6("state Jacobian is a {0}x{1} matrix, it should be a 6x6 matrix"),
162 STATE_AND_PARAMETERS_JACOBIANS_ROWS_MISMATCH("state Jacobian has {0} rows but parameters Jacobian has {1} rows"),
163 INITIAL_MATRIX_AND_PARAMETERS_NUMBER_MISMATCH(
164 "initial Jacobian matrix has {0} columns, but {1} parameters have been selected"),
165 ORBIT_A_E_MISMATCH_WITH_CONIC_TYPE(
166 "orbit should be either elliptic with a > 0 and e < 1 or hyperbolic with a < 0 and e > 1, a = {0}, e = {1}"),
167 ORBIT_ANOMALY_OUT_OF_HYPERBOLIC_RANGE("true anomaly {0} out of hyperbolic range (e = {1}, {2} < v < {3})"),
168 HYPERBOLIC_ORBIT_NOT_HANDLED_AS("hyperbolic orbits cannot be handled as {0} instances"),
169 CCSDS_DATE_INVALID_PREAMBLE_FIELD("invalid preamble field in CCSDS date: {0}"),
170 CCSDS_DATE_INVALID_LENGTH_TIME_FIELD("invalid time field length in CCSDS date: {0}, expected {1}"),
171 CCSDS_DATE_MISSING_AGENCY_EPOCH("missing agency epoch in CCSDS date"),
172 CCSDS_MISSING_KEYWORD("missing mandatory key {0} in CCSDS file {1}"),
173 CCSDS_KEYWORD_NOT_ALLOWED_IN_VERSION("key {0} is not allowed in format version {1}"),
174 CCSDS_UNEXPECTED_KEYWORD("unexpected keyword in CCSDS line number {0} of file {1}:\n{2}"),
175 CCSDS_UNKNOWN_GM("the central body gravitational coefficient cannot be retrieved from the ODM"),
176 CCSDS_UNKNOWN_SPACECRAFT_MASS("there is no spacecraft mass associated with this ODM file"),
177 CCSDS_UNKNOWN_CONVENTIONS("no IERS conventions have been set before parsing"),
178 CCSDS_INVALID_FRAME("frame {0} is not valid in this CCSDS file context"),
179 CCSDS_INCONSISTENT_TIME_SYSTEMS("inconsistent time systems: {0} ≠ {1}"),
180 CCSDS_TIME_SYSTEM_NOT_IMPLEMENTED(
181 "use of time system {0} in CCSDS files requires an additional ICD and is not implemented in Orekit"),
182 CCSDS_TDM_KEYWORD_NOT_FOUND("No CCSDS TDM keyword was found at line {0} of file {1}:\n{2}"),
183 CCSDS_TDM_MISSING_RANGE_UNITS_CONVERTER("no Range Units converter configured for parsing Tracking Data Message"),
184 CCSDS_TIME_SYSTEM_NOT_READ_YET("Time system should have already been set before line {0} of file {1}"),
185 CCSDS_AEM_INCONSISTENT_TIME_SYSTEMS("inconsistent time systems in the attitude blocks: {0} ≠ {1}"),
186 CCSDS_AEM_ATTITUDE_TYPE_NOT_IMPLEMENTED("attitude type {0} in CCSDS AEM files is not implemented in Orekit"),
187 CCSDS_INVALID_ROTATION_SEQUENCE("invalid rotation sequence {0} at line {1} of file {2}"),
188 CCSDS_UNSUPPORTED_ELEMENT_SET_TYPE("element set type {0} ({1}) is not supported yet"),
189 CCSDS_UNSUPPORTED_RETROGRADE_EQUINOCTIAL("retrograde factor not supported in element set {0}"),
190 CCSDS_ELEMENT_SET_WRONG_NB_COMPONENTS("element set type {0} ({1}) expects {2} elements"),
191 CCSDS_MANEUVER_UNITS_WRONG_NB_COMPONENTS("wrong number of units for maneuver {0}"),
192 CCSDS_MANEUVER_MISSING_TIME("missing time field for maneuver {0}"),
193 ADDITIONAL_STATE_NAME_ALREADY_IN_USE("name \"{0}\" is already used for an additional state"),
194 NON_RESETABLE_STATE("reset state not allowed"),
195 DSST_NEWCOMB_OPERATORS_COMPUTATION("Cannot compute Newcomb operators for sigma > rho ({0} > {1})"),
196 DSST_VMNS_COEFFICIENT_ERROR_MS("Cannot compute the Vmns coefficient with m > n ({0} > {1})"),
197 DSST_SPR_SHADOW_INCONSISTENT("inconsistent shadow computation: entry = {0} whereas exit = {1}"),
198 DSST_ECC_NO_NUMERICAL_AVERAGING_METHOD(
199 "The current orbit has an eccentricity ({0} > 0.5). DSST needs an unimplemented time dependent numerical method to compute the averaged rates"),
200 SP3_UNSUPPORTED_VERSION("unsupported sp3 file version {0}"),
201 SP3_NUMBER_OF_EPOCH_MISMATCH("found {0} epochs in file {1}, expected {2}"),
202 SP3_UNEXPECTED_END_OF_FILE("unexpected end of sp3 file (after line {0})"),
203 CLOCK_FILE_UNSUPPORTED_VERSION("unsupported clock file version {0}"),
204 NAVIGATION_FILE_UNSUPPORTED_VERSION("unsupported navigation messages file version {0}"),
205 NON_EXISTENT_GEOMAGNETIC_MODEL("non-existent geomagnetic model {0} for year {1}"),
206 UNSUPPORTED_TIME_TRANSFORM(
207 "geomagnetic model {0} with epoch {1} does not support time transformation, no secular variation coefficients defined"),
208 OUT_OF_RANGE_TIME_TRANSFORM(
209 "time transformation of geomagnetic model {0} with epoch {1} is outside its validity range: {2} != [{3}, {4}]"),
210 NOT_ENOUGH_DATA_FOR_INTERPOLATION("not enough data for interpolation (sample size = {0})"),
211 NOT_ENOUGH_CACHED_NEIGHBORS("too small number of cached neighbors: {0} (must be at least {1})"),
212 NO_CACHED_ENTRIES("no cached entries"),
213 NON_CHRONOLOGICALLY_SORTED_ENTRIES("generated entries not sorted: {0} > {1} by {2,number,0.0##############E0} s"),
214 NO_DATA_GENERATED("no data generated around date: {0}"),
215 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"),
216 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"),
217 UNABLE_TO_COMPUTE_HYPERBOLIC_ECCENTRIC_ANOMALY(
218 "unable to compute hyperbolic eccentric anomaly from the mean anomaly after {0} iterations"),
219 UNABLE_TO_COMPUTE_DSST_MEAN_PARAMETERS("unable to compute mean orbit from osculating orbit after {0} iterations"),
220 OUT_OF_RANGE_DERIVATION_ORDER("derivation order {0} is out of range"),
221 ORBIT_TYPE_NOT_ALLOWED("orbit type {0} not allowed here, allowed types: {1}"),
222 NON_PSEUDO_INERTIAL_FRAME_NOT_SUITABLE_AS_REFERENCE_FOR_INERTIAL_FORCES(
223 "non pseudo-inertial frame {0} is not suitable as reference for inertial forces"),
224 METHOD_NOT_AVAILABLE_WITHOUT_CENTRAL_BODY("method not available in the absence of a central body"),
225 INCOMPATIBLE_FRAMES("operation not available between frames {0} and {1}"),
226 UNDEFINED_ORBIT("orbit not defined, state rather contains an absolute position-velocity-acceleration"),
227 UNDEFINED_ABSOLUTE_PVCOORDINATES(
228 "absolute position-velocity-acceleration not defined, state rather contains an orbit"),
229 INERTIAL_FORCE_MODEL_MISSING("an inertial force model has to be used when propagating in non-inertial frame {0}"),
230 NO_SEM_ALMANAC_AVAILABLE("no SEM almanac file found"),
231 NOT_A_SUPPORTED_SEM_ALMANAC_FILE("file {0} is not a supported SEM almanac file"),
232 NO_YUMA_ALMANAC_AVAILABLE("no Yuma almanac file found"),
233 NOT_A_SUPPORTED_YUMA_ALMANAC_FILE("file {0} is not a supported Yuma almanac file"),
234 NOT_ENOUGH_GNSS_FOR_DOP("only {0} GNSS orbits are provided while {1} are needed to compute the DOP"),
235 NOT_ENOUGH_PROPAGATORS(
236 "Creating an aggregate propagator requires at least one constituent propagator, but none were provided."),
237 NOT_ENOUGH_ATTITUDE_PROVIDERS(
238 "Creating an aggregate attitude provider requires at least one constituent attitude provider, but none were provided."),
239 NULL_ARGUMENT("argument {0} cannot be null"),
240 VALUE_NOT_FOUND("value {0} not found in {1}"),
241 KLOBUCHAR_ALPHA_BETA_NOT_LOADED("Klobuchar coefficients α or β could not be loaded from {0}"),
242 KLOBUCHAR_ALPHA_BETA_NOT_AVAILABLE_FOR_DATE("Klobuchar coefficients α or β not available for date {0}"),
243 NO_KLOBUCHAR_ALPHA_BETA_IN_FILE("file {0} does not contain Klobuchar coefficients α or β"),
244 NO_REFERENCE_DATE_FOR_PARAMETER("no reference date set for parameter {0}"),
245 STATION_NOT_FOUND("station {0} not found, known stations: {1}"),
246 UNKNOWN_SATELLITE_SYSTEM("unknown satellite system {0}"),
247 UNKNOWN_TIME_SYSTEM("unknown time system {0}"),
248 UNKNOWN_CLOCK_DATA_TYPE("unknown clock data type {0}"),
249 UNKNOWN_SATELLITE_ANTENNA_CODE("unknown satellite antenna code {0}"),
250 UNSUPPORTED_FREQUENCY_FOR_ANTENNA("frequency {0} is not supported by antenna {1}"),
251 CANNOT_FIND_SATELLITE_IN_SYSTEM("cannot find satellite {0} in satellite system {1}"),
252 UNKNOWN_RINEX_FREQUENCY("unknown RINEX frequency {0} in file {1}, line {2}"),
253 MISMATCHED_FREQUENCIES("mismatched frequencies in file {0}, line {1} (expected {2}, got {3})"),
254 WRONG_COLUMNS_NUMBER("wrong number of columns in file {0}, line {1} (expected {2} columns, got {3} columns)"),
255 UNSUPPORTED_FILE_FORMAT("unsupported format for file {0}"),
256 INCOMPLETE_HEADER("incomplete header in file {0}"),
257 INCONSISTENT_NUMBER_OF_SATS(
258 "inconsistent number of satellites in line {0}, file {1}: observation with {2} satellites and number of max satellites is {3}"),
259 INCONSISTENT_SATELLITE_SYSTEM(
260 "the satellite system {3} from line {0}, file {1} is not consistent with the Rinex Satellite System {2} in header"),
261 NO_PROPAGATOR_CONFIGURED("no propagator configured"),
262 DIMENSION_INCONSISTENT_WITH_PARAMETERS("dimension {0} is inconsistent with parameters list: {1}"),
263 NOT_A_SUPPORTED_UNIX_COMPRESSED_FILE("file {0} is not a supported Unix-compressed file"),
264 UNEXPECTED_END_OF_FILE("unexpected end of file {0}"),
265 CORRUPTED_FILE("file {0} is corrupted"),
266 VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_LOADED("Vienna coefficients ah or aw or zh or zw could not be loaded from {0}"),
267 VIENNA_ACOEF_OR_ZENITH_DELAY_NOT_AVAILABLE_FOR_DATE(
268 "Vienna coefficients ah or aw or zh or zw not available for date {0}"),
269 NO_VIENNA_ACOEF_OR_ZENITH_DELAY_IN_FILE("file {0} does not contain Vienna coefficients ah, aw, zh or zw"),
270 IRREGULAR_OR_INCOMPLETE_GRID("irregular or incomplete grid in file {0}"),
271 INVALID_SATELLITE_SYSTEM("invalid satellite system {0}"),
272 NO_TEC_DATA_IN_FILE_FOR_DATE("IONEX file {0} does not contain TEC data for date {1}"),
273 INCONSISTENT_NUMBER_OF_TEC_MAPS_IN_FILE("number of maps {0} is inconsistent with header specification: {1}"),
274 NO_LATITUDE_LONGITUDE_BONDARIES_IN_IONEX_HEADER(
275 "file {0} does not contain latitude or longitude bondaries in its header section"),
276 NO_EPOCH_IN_IONEX_HEADER("file {0} does not contain epoch of first or last map in its header section"),
277 ITRF_VERSIONS_PREFIX_ONLY("The first column of itrf-versions.conf is a plain " +
278 "prefix that is matched against the name of each loaded file. It should " +
279 "not contain any regular expression syntax or directory components, i.e. " +
280 "\"/\" or \"\\\". Actual value: \"{0}\"."),
281 CANNOT_COMPUTE_AIMING_AT_SINGULAR_POINT(
282 "cannot compute aiming direction at singular point: latitude = {0}, longitude = {1}"),
283 STEC_INTEGRATION_DID_NOT_CONVERGE("STEC integration did not converge"),
284 MODIP_GRID_NOT_LOADED("MODIP grid not be loaded from {0}"),
285 NEQUICK_F2_FM3_NOT_LOADED("NeQuick coefficient f2 or fm3 not be loaded from {0}"),
286 NOT_A_SUPPORTED_HATANAKA_COMPRESSED_FILE("file {0} is not a supported Hatanaka-compressed file"),
287 CANNOT_COMPUTE_LAGRANGIAN("Cannot compute around {0}"),
288 TRAJECTORY_NOT_CROSSING_XZPLANE("The trajectory does not cross XZ Plane, it will not result in a Halo Orbit"),
289 MULTIPLE_SHOOTING_UNDERCONSTRAINED(
290 "The multiple shooting problem is underconstrained : {0} free variables, {1} constraints"),
291 INVALID_MEASUREMENT_TYPES_FOR_COMBINATION_OF_MEASUREMENTS(
292 "invalid measurement types {0} and {1} for the combination of measurements {2}"),
293 INCOMPATIBLE_FREQUENCIES_FOR_COMBINATION_OF_MEASUREMENTS(
294 "frequencies {0} and {1} are incompatibles for the {2} combination"),
295 NON_CHRONOLOGICAL_DATES_FOR_OBSERVATIONS("observations are not in chronological order: {0} is {2,number,0.0##############E0} s after {1}"),
296 EXCEPTIONAL_DATA_CONTEXT(
297 "Use of the ExceptionalDataContext detected. This is typically used to detect developer errors."),
298 NON_DIFFERENT_DATES_FOR_OBSERVATIONS(
299 "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)"),
300 NON_COPLANAR_POINTS("observations are not in the same plane"),
301 INVALID_PARAMETER_RANGE("invalid parameter {0}: {1} not in range [{2}, {3}]"),
302 PARAMETER_NOT_SET("The parameter {0} should not be null in {1}"),
303 FUNCTION_NOT_IMPLEMENTED("{0} is not implemented"),
304 INVALID_TYPE_FOR_FUNCTION("Impossible to execute {0} with {1} set to {2}"),
305 NO_DATA_IN_FILE("No data could be parsed from file {0}"),
306 CPF_UNEXPECTED_END_OF_FILE("Unexpected end of CPF file (after line {0})"),
307 UNEXPECTED_FORMAT_FOR_ILRS_FILE("Unexpected file format. Must be {0} but is {1}"),
308 CRD_UNEXPECTED_END_OF_FILE("Unexpected end of CRD file (after line {0})"),
309 INVALID_RANGE_INDICATOR_IN_CRD_FILE("Invalid range indicator {0} in CRD file header"),
310 END_OF_ENCODED_MESSAGE("end of encoded message reached"),
311 TOO_LARGE_DATA_TYPE("too large data type ({0} bits)"),
312 UNKNOWN_ENCODED_MESSAGE_NUMBER("unknown encoded message number {0}"),
313 UNKNOWN_AUTHENTICATION_METHOD("unknown authentication method: {0}"),
314 UNKNOWN_CARRIER_PHASE_CODE("unknown carrier phase code: {0}"),
315 UNKNOWN_DATA_FORMAT("unknown data format: {0}"),
316 UNKNOWN_NAVIGATION_SYSTEM("unknown navigation system: {0}"),
317 STREAM_REQUIRES_NMEA_FIX("data stream {0} requires a NMEA fix data"),
318 FAILED_AUTHENTICATION("failed authentication for mountpoint {0}"),
319 CONNECTION_ERROR("error connecting to {0}: {1}"),
320 UNEXPECTED_CONTENT_TYPE("unexpected content type {0}"),
321 CANNOT_PARSE_GNSS_DATA("cannot parse GNSS data from {0}"),
322 UNKNOWN_HOST("unknown host {0}"),
323 SOURCETABLE_PARSE_ERROR("error parsing sourcetable line {0} from {1}: {2}"),
324 CANNOT_PARSE_SOURCETABLE("cannot parse sourcetable from {0}"),
325 MOUNPOINT_ALREADY_CONNECTED("mount point {0} is already connected"),
326 MISSING_HEADER("missing header from {0}: {1}"),
327 NOT_VALID_INTERNATIONAL_DESIGNATOR("{0} is not a valid international designator"),
328 UNINITIALIZED_VALUE_FOR_KEY("value for key {0} has not been initialized"),
329 UNKNOWN_UNIT("unknown unit {0}"),
330 INCOMPATIBLE_UNITS("units {0} and {1} are not compatible"),
331 MISSING_VELOCITY("missing velocity data"),
332 ATTEMPT_TO_GENERATE_MALFORMED_FILE("attempt to generate file {0} with a formatting error"),
333 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})"),
334 BACKWARD_PROPAGATION_NOT_ALLOWED("backward propagation not allowed here"),
335 NO_STATION_ECCENTRICITY_FOR_EPOCH("no station eccentricity values for the given epoch {0}, validity interval is between {1} and {2}"),
336 INCONSISTENT_SELECTION("inconsistent parameters selection between pairs {0}/{1} and {2}/{3}");
337
338
339
340
341 private static final String RESOURCE_BASE_NAME = "assets/org/orekit/localization/OrekitMessages";
342
343
344 private final String sourceFormat;
345
346
347
348
349
350
351 OrekitMessages(final String sourceFormat) {
352 this.sourceFormat = sourceFormat;
353 }
354
355
356 public String getSourceString() {
357 return sourceFormat;
358 }
359
360
361 public String getLocalizedString(final Locale locale) {
362 try {
363 final ResourceBundle bundle = ResourceBundle.getBundle(RESOURCE_BASE_NAME, locale, new UTF8Control());
364 if (bundle.getLocale().getLanguage().equals(locale.getLanguage())) {
365 final String translated = bundle.getString(name());
366 if (translated != null && translated.length() > 0 &&
367 !translated.toLowerCase().contains("missing translation")) {
368
369 return translated;
370 }
371 }
372
373 } catch (MissingResourceException mre) {
374
375 }
376
377
378
379 return sourceFormat;
380
381 }
382
383
384
385
386
387
388
389
390
391
392
393 public static class UTF8Control extends ResourceBundle.Control {
394
395
396 @Override
397 public ResourceBundle newBundle(final String baseName, final Locale locale, final String format,
398 final ClassLoader loader, final boolean reload)
399 throws IllegalAccessException, InstantiationException, IOException {
400
401 final String bundleName = toBundleName(baseName, locale);
402 final String resourceName = toResourceName(bundleName, "utf8");
403 ResourceBundle bundle = null;
404 InputStream stream = null;
405 if (reload) {
406 final URL url = loader.getResource(resourceName);
407 if (url != null) {
408 final URLConnection connection = url.openConnection();
409 if (connection != null) {
410 connection.setUseCaches(false);
411 stream = connection.getInputStream();
412 }
413 }
414 } else {
415 stream = loader.getResourceAsStream(resourceName);
416 }
417 if (stream != null) {
418 try (InputStreamReader inputStreamReader = new InputStreamReader(stream, StandardCharsets.UTF_8)) {
419
420 bundle = new PropertyResourceBundle(inputStreamReader);
421 }
422 }
423 return bundle;
424 }
425 }
426 }