曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

10 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 152 – 178
15 E 55S, 50S, 45S, ..., 45N, 50N, 55N 179 – 201
Band 5
20 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 1 – 27
25 E 55S, 50S, 45S, ..., 45N, 50N, 55N 28 – 50
Appendix B Annex 10 — Aeronautical Communications
APP B-43 23/11/06
IGP location
Transmission order in
IGP band mask
30 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 51 – 77
35 E 55S, 50S, 45S, ..., 45N, 50N, 55N 78 – 100
40 E 85S, 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 101 – 128
45 E 55S, 50S, 45S, ..., 45N, 50N, 55N 129 – 151
50 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 152 – 178
55 E 55S, 50S, 45S, ..., 45N, 50N, 55N 179 – 201
Band 6
60 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 1 – 27
65 E 55S, 50S, 45S, ..., 45N, 50N, 55N 28 – 50
70 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 51 – 77
75 E 55S, 50S, 45S, ..., 45N, 50N, 55N 78 – 100
80 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 101 – 127
85 E 55S, 50S, 45S, ..., 45N, 50N, 55N 128 – 150
90 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N, 85N 151 – 178
95 E 55S, 50S, 45S, ..., 45N, 50N, 55N 179 – 201
Band 7
100 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 1 – 27
105 E 55S, 50S, 45S, ..., 45N, 50N, 55N 28 – 50
110 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 51 – 77
115 E 55S, 50S, 45S, ..., 45N, 50N, 55N 78 – 100
120 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 101 – 127
125 E 55S, 50S, 45S, ..., 45N, 50N, 55N 128 – 150
130 E 85S, 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 151 – 178
135 E 55S, 50S, 45S, ..., 45N, 50N, 55N 179 – 201
Band 8
140 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 1 – 27
145 E 55S, 50S, 45S, ..., 45N, 50N, 55N 28 – 50
150 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 51 – 77
155 E 55S, 50S, 45S, ..., 45N, 50N, 55N 78 – 100
160 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 101 – 127
165 E 55S, 50S, 45S, ..., 45N, 50N, 55N 128 – 150
170 E 75S, 65S, 55S, 50S, 45S, ..., 45N, 50N, 55N, 65N, 75N 151 – 177
175 E 55S, 50S, 45S, ..., 45N, 50N, 55N 178 – 200
Band 9
60 N 180W, 175W, 170W, …, 165E, 170E, 175E 1 – 72
65 N 180W, 170W, 160W, …, 150E, 160E, 170E 73 – 108
70 N 180W, 170W, 160W, …, 150E, 160E, 170E 109 – 144
Annex 10 — Aeronautical Communications Volume I
23/11/06 APP B-44
IGP location
Transmission order in
IGP band mask
75 N 180W, 170W, 160W, …, 150E, 160E, 170E 145 – 180
85 N 180W, 150W, 120W, …, 90E, 120E, 150E 181 – 192
Band 10
60 S 180W, 175W, 170W, …, 165E, 170E, 175E 1 – 72
65 S 180W, 170W, 160W, …, 150E, 160E, 170E 73 – 108
70 S 180W, 170W, 160W, …, 150E, 160E, 170E 109 – 144
75 S 180W, 170W, 160W, …, 150E, 160E, 170E 145 – 180
85 S 170W, 140W, 110W, …, 100E, 130E, 160E 181 – 192
Table B-31. Validity interval
Data Bits used Range of values Resolution
Validity interval (V) 5 30 s to 960 s 30 s
Table B-32. Latency time
Data Bits used Range of values Resolution
Latency time (L) 3 0 s to 120 s 30 s
Table B-33. Evaluation of GIVEIi
GIVEIi σ2
i,GIVE
0 0.0084 m2
1 0.0333 m2
2 0.0749 m2
3 0.1331 m2
4 0.2079 m2
5 0.2994 m2
6 0.4075 m2
7 0.5322 m2
8 0.6735 m2
9 0.8315 m2
10 1.1974 m2
11 1.8709 m2
12 3.3260 m2
13 20.787 m2
14 187.0826 m2
15 “Not Monitored”
Appendix B Annex 10 — Aeronautical Communications
3.5.4.7 Degradation parameters. Degradation parameters, whenever used, shall be as follows:
ast correction degradation factor indicator (ai ): an indicator of the fast correction degradation factor (a ) for the ith satellite
Note.— The ai is also used to define the time-out interval for fast corrections, as described in 3.5.8.1.1.
System latency time (tlat): the time interval between the origin of the fast correction degradation and the user differential range
estimate indicator (UDREI) reference time.
rrc: a parameter that bounds the noise and round-off errors when computing the range rate correction degradation as in
ormation.
: the update interval for long-term corrections if velocity code = 1 (3.5.4.4.1).
ltc_v0: a parameter that bounds the difference between two consecutive long-term corrections for satellites with a velocity
　
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