HpeGnss.xid.xml
25.9 KB
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
353
354
355
356
357
358
359
360
361
362
363
364
365
366
367
368
369
370
371
372
373
374
375
376
377
378
379
380
381
382
383
384
385
386
387
388
389
390
391
392
393
394
395
396
397
398
399
400
401
402
403
404
405
406
407
408
409
410
411
412
413
414
415
416
417
418
419
420
421
422
423
424
425
426
427
428
429
430
431
432
433
434
435
436
437
438
439
440
441
442
443
444
445
446
447
448
449
450
451
452
453
454
455
456
457
458
459
460
461
462
463
464
465
466
467
468
469
470
<?xml version="1.0" encoding="UTF-8" ?>
<specification xmlns="https://xid.location.studio/schema/V1.0.0/XtensibleInterfaceDefinition.xsd"
xmlns:xid="https://xid.location.studio/schema/V1.0.0/XtensibleInterfaceDefinition.xsd"
xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance"
xsi:schemaLocation="https://xid.location.studio/schema/V1.0.0/XtensibleInterfaceDefinition.xsd https://xid.location.studio/schema/V1.0.0/XtensibleInterfaceDefinition.xsd"
identity="HpeGnss.xid.xml">
<title>HPE GNSS Data Definition</title>
<comment>File contains data definitions for GNSS HPE location related datatypes.</comment>
<import ref="https://xid.location.studio/Tensor/V1.0.0/Definitions.xid.xml" local="Definitions.xid.xml" />
<import ref="https://xid.location.studio/HPE/V1.2/HpeCore.xid.xml" local="HpeCore.xid.xml" />
<namespace name="HPE.Gnss">
<using namespace="Tensor"/>
<using namespace="HPE"/>
<enum name="Constellation" type="uint8" default="unspecified">
<comment>
GNSS constellation types.
</comment>
<literal name="unspecified" value="0x00"/>
<literal name="GPS" value="0x01"/>
<literal name="GLONASS" value="0x02"/>
<literal name="GALILEO" value="0x03"/>
<literal name="BEIDOU" value="0x04"/>
<literal name="QZSS" value="0x05"/>
<literal name="MBS_FLAG" value="0x20"/>
<literal name="RTLS_FLAG" value="0x40"/>
</enum>
<enum name="AssistanceType" type="uint8" default="unspecified">
<comment>
Enumeration literals defining the types of assistance data supported.
</comment>
<literal name="unspecified" value="0x00"/>
<literal name="GpsAlmanac" value="0x01"/>
<literal name="GpsEphemeris" value="0x02"/>
<literal name="GpsUtcParameters" value="0x03"/>
<literal name="GpsIonosphericCorrection" value="0x04"/>
<literal name="AcquisitionAssistance" value="0x05"/>
</enum>
<!-- Satellite ID -->
<struct name="SatelliteId" pack="true">
<comment>Satellite identifier specifies constellation and satellite identifier.</comment>
<elem name ="constellation" type="Constellation" multiplicity="1"/>
<elem name ="id" type="uint8" multiplicity="1">
<comment>Satellite identifier: range 0 to 63.</comment>
</elem>
</struct>
<!--
*******************************************************
Almanac Data Structures
*******************************************************
-->
<!-- Almanac -->
<struct name="Almanac" pack="true">
<comment>Generalized Almanac orbit in GPS reference frame. One record per satellite.</comment>
<elem name ="id" type="uint8" multiplicity="1">
<comment>Satellite identifier, valid range is 0-63.</comment>
</elem>
<elem name ="toa" type="uint8" multiplicity="1">
<comment>Time of almanac in seconds. Value is integer encoded with scale factor 2^12</comment>
<tag name="unit" value="2^12 seconds"/>
</elem>
<elem name ="deltai0" type="int16" multiplicity="1">
<comment>Relative inclination to i0 = 0.3 semi-circles at reference time. Value is integer encoded with scale factor 2^-19</comment>
<tag name="unit" value="2^-19 semi-circles"/>
</elem>
<elem name ="OmegaDot" type="int16" multiplicity="1">
<comment>Rate of Right Ascension in semi-circles/sec. Value is integer encoded with scale factor 2^-38</comment>
<tag name="unit" value="2^-38 seconds"/>
</elem>
<elem name ="af0" type="int16" multiplicity="1">
<comment>SV clock bias in seconds. Value is integer encoded with scale factor 2^-20</comment>
<tag name="unit" value="2^-20 seconds"/>
</elem>
<elem name ="af1" type="int16" multiplicity="1">
<comment>SV clock bias rate in seconds/second. Value is integer encoded with scale factor 2^-38</comment>
<tag name="unit" value="2^-38 seconds"/>
</elem>
<elem name ="eccentricity" type="uint16" multiplicity="1">
<comment>Eccentricity of the orbit. Value is integer encoded with scale factor 2^-21</comment>
<tag name="unit" value="2^-21"/>
</elem>
<elem name ="sqrtA" type="uint24" multiplicity="1">
<comment>Square root of Mean anomaly. Value is integer encoded with scale factor 2^-11</comment>
<tag name="unit" value="2^-11 meters^1/2"/>
</elem>
<elem name ="Omega0" type="int24" multiplicity="1">
<comment>Longitude of ascending node in semi-circles. Value is integer encoded with scale factor 2^-23</comment>
<tag name="unit" value="2^-23 semi-circles"/>
</elem>
<elem name ="omega" type="int24" multiplicity="1">
<comment>omega argument of perigee in semi-circles. Value is integer encoded with scale factor 2^-23</comment>
<tag name="unit" value="2^-23 semi-circles"/>
</elem>
<elem name ="M0" type="int24" multiplicity="1">
<comment>Mean anomaly at reference time in semi-circles. Value is integer encoded with scale factor 2^-23</comment>
<tag name="unit" value="2^-23 semi-circles"/>
</elem>
<elem name ="SvHealth" type="uint8" multiplicity="1">
<comment>Satellite health flags.</comment>
</elem>
</struct>
<!-- Ephemeris -->
<struct name="Ephemeris" pack="true">
<comment>Generalized GPS 15 element precision Keplerian orbit in GPS reference frame. One record per satellite.</comment>
<elem name ="id" type="uint8" multiplicity="1">
<comment>Satellite identifier, valid range is 0-63.</comment>
</elem>
<elem name ="toe" type="uint16" multiplicity="1">
<comment>Time of Ephemeris. Value is integer encoded with scale factor 2^4</comment>
<tag name="unit" value="2^4 seconds"/>
</elem>
<elem name ="iode" type="uint8" multiplicity="1">
<comment>Issue of data Ephemeris. The value for comparison with the 8 LSBs of the IODC</comment>
</elem>
<elem name ="eccentricity" type="uint32" multiplicity="1">
<comment>Eccentricity of the orbit. Value is integer encoded with scale factor 2^-33</comment>
<tag name="unit" value="2^-33"/>
</elem>
<elem name ="i0" type="int32" multiplicity="1">
<comment>Inclination at reference time in semi-circles. Value is integer encoded with scale factor 2^-31</comment>
<tag name="unit" value="2^-31 semi-circles"/>
</elem>
<elem name ="OmegaDot" type="int24" multiplicity="1">
<comment>Rate of Right Ascension in semi-circles/sec. Value is integer encoded with scale factor 2^-43</comment>
<tag name="unit" value="2^-43 seconds"/>
</elem>
<elem name ="sqrtA" type="uint32" multiplicity="1">
<comment>Square root of Mean anomaly. Value is integer encoded with scale factor 2^-19</comment>
<tag name="unit" value="2^-19 meters^1/2"/>
</elem>
<elem name ="Omega0" type="int32" multiplicity="1">
<comment>Longitude of ascending node in semi-circles. Value is integer encoded with scale factor 2^-31</comment>
<tag name="unit" value="2^-31 semi-circles"/>
</elem>
<elem name ="omega" type="int32" multiplicity="1">
<comment>omega argument of perigee in semi-circles. Value is integer encoded with scale factor 2^-31</comment>
<tag name="unit" value="2^-31 semi-circles"/>
</elem>
<elem name ="M0" type="int32" multiplicity="1">
<comment>Mean anomaly at reference time in semi-circles. Value is integer encoded with scale factor 2^-31</comment>
<tag name="unit" value="2^-31 semi-circles"/>
</elem>
<elem name ="deltan" type="int16" multiplicity="1">
<comment>Mean Motion Difference From Computed Value in semi-circles/sec. Value is integer encoded with scale factor 2^-43</comment>
<tag name="unit" value="2^-43 semi-circles"/>
</elem>
<elem name ="idot" type="int16" multiplicity="1">
<comment>Rate of Inclination in semi-circles/sec. Value is integer encoded with scale factor 2^-43</comment>
<tag name="unit" value="2^-43 semi-circles"/>
</elem>
<elem name ="Cis" type="int16" multiplicity="1">
<comment>Amp. Sin Correction of Inclination in radians. Value is integer encoded with scale factor 2^-29</comment>
<tag name="unit" value="2^-29 radians"/>
</elem>
<elem name ="Cic" type="int16" multiplicity="1">
<comment>Amp. Cosine Correction of Inclination in radians. Value is integer encoded with scale factor 2^-29</comment>
<tag name="unit" value="2^-29 radians"/>
</elem>
<elem name ="Crs" type="int16" multiplicity="1">
<comment>Amp. Sin Correction of orbit radius in meters. Value is integer encoded with scale factor 2^-5</comment>
<tag name="unit" value="2^-5 meters"/>
</elem>
<elem name ="Crc" type="int16" multiplicity="1">
<comment>Amp. Cosine Correction of orbit radius in meters. Value is integer encoded with scale factor 2^-5</comment>
<tag name="unit" value="2^-5 meters"/>
</elem>
<elem name ="Cus" type="int16" multiplicity="1">
<comment>Amp. Sin Correction of Latitude in radians. Value is integer encoded with scale factor 2^-29</comment>
<tag name="unit" value="2^-29 radians"/>
</elem>
<elem name ="Cuc" type="int16" multiplicity="1">
<comment>Amp. Cosine Correction of Latitude in radians. Value is integer encoded with scale factor 2^-29</comment>
<tag name="unit" value="2^-29 radians"/>
</elem>
<elem name ="toc" type="uint16" multiplicity="1">
<comment>Time of clock. Value is integer encoded with scale factor 2^4</comment>
<tag name="unit" value="2^4 seconds"/>
</elem>
<elem name ="iodc" type="uint16" multiplicity="1">
<comment>Issue of data Clock. </comment>
<tag name="unit" value="discretes"/>
</elem>
<elem name ="af0" type="int24" multiplicity="1">
<comment>SV clock bias in seconds. Value is integer encoded with scale factor 2^-31.</comment>
<tag name="unit" value="2^-31 seconds"/>
</elem>
<elem name ="af1" type="int16" multiplicity="1">
<comment>SV clock bias rate in seconds/second. Value is integer encoded with scale factor 2^-43.</comment>
<tag name="unit" value="2^-43 seconds"/>
</elem>
<elem name ="af2" type="int8" multiplicity="1">
<comment>SV clock bias rate in seconds/second^2. Value is integer encoded with scale factor 2^-55.</comment>
<tag name="unit" value="2^-55 seconds"/>
</elem>
<elem name ="TGD" type="int8" multiplicity="1">
<comment>L1-L2 group delay differential in seconds. Value is integer encoded with a scale factor 2^-31.</comment>
<tag name="unit" value="2^-31 seconds"/>
</elem>
<elem name ="SvHealth" type="uint8" multiplicity="1">
<comment>Satellite health flags.</comment>
</elem>
</struct>
<!-- UTC Parameters -->
<struct name="UtcParameters" pack="true">
<comment>Conversion data between GPS time and UTC.</comment>
<elem name ="a0" type="int32" multiplicity="1">
<comment>Constant term of the polynomial in seconds. Value is integer encoded with scale factor 2^-30.</comment>
<tag name="unit" value="2^-30 seconds"/>
</elem>
<elem name ="a1" type="int24" multiplicity="1">
<comment>First order term of the polynomial in seconds/second. Value is integer encoded with scale factor 2^-50.</comment>
<tag name="unit" value="2^-50 seconds"/>
</elem>
<elem name ="DeltaTls" type="int8" multiplicity="1">
<comment>Delta time due to Leap Seconds. </comment>
<tag name="unit" value="seconds"/>
</elem>
<elem name ="tot" type="uint8" multiplicity="1">
<comment>Time of Utc Data. Value is integer encoded with scale factor 2^12</comment>
<tag name="unit" value="2^12 seconds"/>
</elem>
<elem name ="WNt" type="uint8" multiplicity="1">
<comment>UTC Reference Week Number in weeks</comment>
<tag name="unit" value="weeks"/>
</elem>
<elem name ="WNlsf" type="uint8" multiplicity="1">
<comment>Week Number LeapSecond Future in weeks</comment>
<tag name="unit" value="weeks"/>
</elem>
<elem name ="DN" type="uint8" multiplicity="1">
<comment>Day number in days</comment>
<tag name="unit" value="days"/>
</elem>
<elem name ="DeltaTlsf" type="int8" multiplicity="1">
<comment>Delta time due to Leap Seconds Future</comment>
<tag name="unit" value="seconds"/>
</elem>
</struct>
<!-- Ionosperhic Correction -->
<struct name="IonosphericCorrection" pack="true">
<comment>Klobuchar Ionospheric Correction model parameters. See ICD200 para. 20.3.3.5.2.5</comment>
<elem name ="a0" type="int8" multiplicity="1">
<comment>alpha0 term of the polynomial in seconds. Value is integer encoded with scale factor 2^-30.</comment>
<tag name="unit" value="2^-30 seconds"/>
</elem>
<elem name ="a1" type="int8" multiplicity="1">
<comment>alpha1 term of the polynomial in seconds. Value is integer encoded with scale factor 2^-27.</comment>
<tag name="unit" value="2^-27 seconds"/>
</elem>
<elem name ="a2" type="int8" multiplicity="1">
<comment>alpha2 term of the polynomial in seconds. Value is integer encoded with scale factor 2^-24.</comment>
<tag name="unit" value="2^-24 seconds"/>
</elem>
<elem name ="a3" type="int8" multiplicity="1">
<comment>alpha3 term of the polynomial in seconds. Value is integer encoded with scale factor 2^-24.</comment>
<tag name="unit" value="2^-24 seconds"/>
</elem>
<elem name ="b0" type="int8" multiplicity="1">
<comment>beta0 term of the polynomial in seconds. Value is integer encoded with scale factor 2^11.</comment>
<tag name="unit" value="2^11 seconds"/>
</elem>
<elem name ="b1" type="int8" multiplicity="1">
<comment>beta1 term of the polynomial in seconds. Value is integer encoded with scale factor 2^14.</comment>
<tag name="unit" value="2^14 seconds"/>
</elem>
<elem name ="b2" type="int8" multiplicity="1">
<comment>beta2 term of the polynomial in seconds. Value is integer encoded with scale factor 2^16.</comment>
<tag name="unit" value="2^16 seconds"/>
</elem>
<elem name ="b3" type="int8" multiplicity="1">
<comment>beta3 term of the polynomial in seconds. Value is integer encoded with scale factor 2^16.</comment>
<tag name="unit" value="2^16 seconds"/>
</elem>
</struct>
<!-- ConstellationData -->
<struct name="ConstellationData">
<comment>Grouping of constellation data. Reference frame is GPS.</comment>
<comment>Will be extended to include other constellation data.</comment>
<!-- this has been embedded in a device, Only add. -->
<array name="AlmanacArray" type="Almanac"/>
<array name="EphemerisArray" type="Ephemeris" />
<elem name ="constellation" type="Constellation" multiplicity="1" ord="64"/>
<elem name ="week" type="uint16" multiplicity="1" ord="65"/>
<elem name ="almanacs" type="AlmanacArray" multiplicity="0..1" ord="66"/>
<!-- the following are are decoded in C decoding API yet -->
<elem name ="ephemeris" type="EphemerisArray" multiplicity="0..1" ord="67"/>
<elem name ="utc" type="UtcParameters" multiplicity="0..1" ord="68"/>
<elem name ="iono" type="IonosphericCorrection" multiplicity="0..1" ord="69" />
</struct>
<struct name="ConstellationSet">
<comment>Set of ConstellationData</comment>
<elem name ="constellationData" type="ConstellationData" multiplicity="0..*" ord="64"/>
</struct>
<!--
*******************************************************
Acquisistion Assistance Data
*******************************************************
-->
<!-- AcqAssistElem -->
<struct name="AcqAssistElem" pack="true">
<comment>Acquisistion assistance for a single satellite.</comment>
<elem name ="id" type="SatelliteId" multiplicity="1"/>
<elem name ="doppler0" type="int16" multiplicity="1">
<comment>Doppler 0th order term. Value is integer encoded with scale factor 2^-21</comment>
<tag name="unit" value="2^-21"/>
</elem>
<elem name ="doppler1" type="int16" multiplicity="1">
<comment>doppler first order term in Hz/sec. Value is integer encoded with scale factor 2^12</comment>
<tag name="unit" value="2^12 seconds"/>
</elem>
<elem name ="codephase" type="uint16" multiplicity="1">
<comment>code phase 0-1022 in 1/8 code chips. Value is integer encoded with scale factor 2^-3</comment>
<tag name="unit" value="2^-3 code chips"/>
</elem>
<elem name ="CodeCount" type="uint16" multiplicity="1">
<comment>Integer count of whole code epochs including the GPS bit number range 0 - 80 counts. </comment>
<tag name="unit" value="code epochs"/>
</elem>
<elem name ="searchWindow" type="uint8" multiplicity="1">
<comment>Rate of right ascension in semi-circles/sec. Value is integer encoded with scale factor 2^-38</comment>
<tag name="unit" value="2^-38 seconds"/>
</elem>
<elem name ="azimuth" type="int8" multiplicity="1">
<comment>Azimuth in degrees. Value is a scaled integer encoded with scale factor 2.5</comment>
<tag name="unit" value="2.5 degrees"/>
</elem>
<elem name ="elevation" type="int8" multiplicity="1">
<comment>Elevation in degrees.</comment>
<tag name="unit" value="degrees"/>
</elem>
</struct>
<!-- AcqAssistSet -->
<struct name="AcqAssistSet">
<comment>A set of doppler acquisition assistance elements</comment>
<elem name="data" type="AcqAssistElem" multiplicity="1..*" polymorphic="false"/>
</struct>
<!--
*******************************************************
GNSS Measurement data
*******************************************************
-->
<!-- CodephaseMeasurementMin-->
<struct name="CodephaseMeasurementMin" pack="true">
<comment>
Measurement of a single satellite codephase. This is a more compact version without RMS error and multipath indicator.
These will be encoded in cno in a future version.
</comment>
<elem name ="id" type="uint8" multiplicity="1">
<comment>
Satellite identifier: 0 - 63. If set to 255 (0xff), the measurement is considered invalid and ignored.
This marks the end of measurements in fixed array sets. See GpsCodePhaseObsMin6 for an example.
</comment>
</elem>
<elem name ="cn0" type="uint8" multiplicity="1">
<comment>Carrier noise ratio.</comment>
<tag name="unit" value="ratio"/>
</elem>
<elem name ="doppler" type="int16" multiplicity="1">
<comment>Measured Doppler shift in Hz. Value is integer encoded with scale factor 0.2</comment>
<tag name="unit" value="0.2 Hz"/>
</elem>
<elem name ="codephase" type="uint24" multiplicity="1">
<comment>Whole and fractional parts of code phase. Value is integer encoded with scale factor 2^-10</comment>
<tag name="unit" value="2^-10 code chips"/>
</elem>
</struct>
<!-- CodephaseMeasurement -->
<struct name="CodephaseMeasurement" type="CodephaseMeasurementMin" pack="true">
<comment>Measurement of a single satellite codephase including mpathIndicator and rmsErr.</comment>
<elem name ="mpathIndicator" type="uint8" multiplicity="1">
<comment>Multipath indicator. Default value is 0.</comment>
</elem>
<elem name ="rmsErr" type="uint8" multiplicity="1">
<comment>Pseudo range RMS Error value indexed 0..63, default is 0</comment>
<tag name="unit" value="2.5 degrees"/>
</elem>
</struct>
<!-- Observation Data types-->
<struct name="GpsCodePhaseObs8" type="ObservationEpoch" pack="true" rttkey="HPE.ObservationType.GPS_CODEPHASE_8">
<comment>
Eight standard GPS code phase measurements: 9 + (9 x 8) = 81 bytes. Mark
the end of the unused or invalid measurements with id=255 (0xFF). They will be ignored.
</comment>
<array name ="CodephaseMeasurement8" type="CodephaseMeasurement" size="8"/>
<elem name ="measurements" type="CodephaseMeasurement8" multiplicity="1">
</elem>
</struct>
<struct name="GpsCodePhaseObsMin6" type="ObservationEpoch" pack="true" rttkey="HPE.ObservationType.GPS_CODEPHASE_MIN6">
<comment>
Six minimum size GPS code phase measurements: 9 + (7 x 6) = 51 bytes.
Mark the end of the unused or invalid measurements with id=255 (0xFF). They will be ignored.
</comment>
<array name ="CodephaseMeasurementMin6" type="CodephaseMeasurementMin" size="6"/>
<elem name ="measurements" type="CodephaseMeasurementMin6" multiplicity="1">
</elem>
</struct>
<struct name="GpsCodePhaseObsMin8" type="ObservationEpoch" pack="true" rttkey="HPE.ObservationType.GPS_CODEPHASE_MIN8">
<comment>
Eight minimum size GPS code phase measurements: 9 + (7 x 8) = 65 bytes.
Mark the end of the unused or invalid measurements with id=255 (0xFF). They will be ignored.
</comment>
<array name ="CodephaseMeasurementMin8" type="CodephaseMeasurementMin" size="8"/>
<elem name ="measurements" type="CodephaseMeasurementMin8" multiplicity="1">
</elem>
</struct>
<struct name="PseudorangeObservation" type="ObservationEpoch" rttkey="HPE.ObservationType.GNSS_PSEUDORANGE">
<comment>GNSS observation data in generic format suited for variable sized input.</comment>
<elem name ="id" type="SatelliteId" multiplicity="1"/>
<elem name ="prr" type="float64" multiplicity="1">
<comment>Pseudorange rate measurement in meters per second.</comment>
<tag name="unit" value="meters per second"/>
</elem>
<elem name ="pr" type="float64" multiplicity="1">
<comment>Pseudorange measurement in meters.</comment>
<tag name="unit" value="meters"/>
</elem>
<elem name ="prrUncert" type="float32" multiplicity="1">
<comment>Pseudorange rate measurement uncertainty in meters per second. This is the one standard deviation confidence (68%) uncertainty.</comment>
<tag name="unit" value="meters per second"/>
</elem>
<elem name ="prUncert" type="float32" multiplicity="1">
<comment>Pseudorange measurement uncertainty in meters. This is the one standard deviation confidence (68%) uncertainty.</comment>
<tag name="unit" value="meters"/>
</elem>
<elem name ="cn0" type="uint8" multiplicity="1">
<comment>Carrier noise ratio.</comment>
<tag name="unit" value="ratio"/>
</elem>
<elem name ="mpathIndicator" type="uint8" multiplicity="1">
<comment>Multipath indicator. Default value is 0.</comment>
</elem>
</struct>
</namespace>
</specification>