Japan Radio NKE2632 Solid State S-Band Marine Radar User Manual Installation Manual Part 11

Japan Radio Co Ltd. Solid State S-Band Marine Radar Installation Manual Part 11

Installation Manual Part 11

Download: Japan Radio NKE2632 Solid State S-Band Marine Radar User Manual Installation Manual Part 11
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Document DescriptionInstallation Manual Part 11
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Date Submitted2015-10-22 00:00:00
Date Available2015-10-22 00:00:00
Creation Date2015-10-15 15:12:08
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Document TitleInstallation Manual Part 11
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6-176
U1
V1
UTH
U1
V1
UTH
WHT.T
RED.T
W401
7ZCRD1682*
P5201
P5105
J5105
S2B-XH-A
1.+12V
2.RTN
P5301
J5201
B2PS-VH
1. +3.3V
2. GND
1.VD+
2.VD3.GND
4.BP
5.BZ
6.GND
7.TIY
8.MTR_TRX9.TIY_RTN
10.MTR_TRX+
11.GND
12.GND
13.MNT_TX+
14.GND
15.MNT_TX16.PHZ
17.GND
18.PHA
19.MNT_RX20.PHB
21.MNT_RX+
22.GND
23.GND
24.MOT_TRX25.C2
26.MOT_TRX+
27.GND
28.GND
29.FAN_CNT0
30.PS_STATUS
J5203
DF20F-30DP-1H(59)
W302
7ZCRD1693*
BLK.T
BLK.T
W301
7ZCRD1692*
RED.T
6 RED.T
W303
7ZCRD1694*
RED.T
WHT.T
TB102
OGM-300NE-6P-04C
J5901
DF3A- 5P-2DSA
1.MNT-RX-P
2.MNT-TX-P
3.MNT-RX-N
4.MNT-TX-N
5.MNTE
TB101
231-344/001-000 [WAGO]
1.VD+
2.VD3.TRIG+
4.TRIG5.BP+
6.BP7.BZ+
8.BZ9.MTR+
10.MTR11.MTRG
12. NC
13. DC48V+
14. DC48VG
J5301
SC02B-J42SK-GHXPR
1.+32V
2.GND
P3505
J2503
DF20F-30DP
-1H(59)
1.VD
2.GND
3.GND
4.BP
5.BZ
6.GND
7.TIY
8.MTR_TRX9.TIY_RTN
10.MTR_TRX+
11.GND
12.GND
13.MNT_TX+
14.GND
15.MNT_TX16.PHZ
17.GND
18.PHA
19.MNT_RX20.PHB
21.MNT_RX+
22.GND
23.GND
24.MOT_TRX25.C2
26.MOT_TRX+
27.GND
28.GND
29.FAN_CNT0
30.PS_STATUS
W203
7ZCRD1675
J3505
SC02B-J42SK
-GHXPR
1. +32V
2. GND
W104
7ZCRD1671*
FAN
W204 P2502 J2502
7ZCRD1669* PV-3-T
GND
J2501
P2501 PV-3-T
+3.3V
W103
7ZCRD1668*
W102
7ZCRD1667*
1.+12V
2.GND
3.MOT_TRX+
4.MOT_TRX5.GND
J1501
P1501 B4P-VH(LF,SN)
1.MU
2.NC
3.MV
4.NC
P1505
J1505
53426-0510(L angle)
P1504
J1504
B3P-VH(LF,SN)
W1
7ZCRD1680*
J2902
J1502
1.M1
2.NC
3.M2
4.NC
5.M3
J1503
B06BOXASK-1(LF,SN)
1.S1
2.S2
3.S3
4.S4
5.S5
6.S6
B3P5-VH(LF,SN)
DATA I/F
J2903
FPGA JTAG
P3104
P3102
W201
7ZCRD1676*
J2901
CPU JTAG
W202
7ZCRD1677*
J3104
P0B-R-35
PM_OUT
J3102
P0B-R-35
RF_ANT
MOTOR
B101
P4301
J4301
PERFORMANCE
MONITOR ANTENNA
(N type connector)
P1301
(TRANSDUCER)
(ROTARY JOINT)
“*” means revision of the specfication document.
W501
7ZCRD1674*
W101
7ZCRD1673*
J1301
6. Appendix > 6.6 Scanner Unit Interconnection Unit
6.6.13 NKE-1632
U1
V1
UTH
U1
V1
UTH
WHT.T
RED.T
W401
7ZCRD1682*
P5201
P5105
J5201
B2PS-VH
1. +3.3V
2. GND
J5105
S2B-XH-A
1.+12V
2.RTN
J5203
DF20F-30DP-1H(59)
1.VD+
2.VD3.GND
4.BP
5.BZ
6.GND
7.TIY
8.MTR_TRX9.TIY_RTN
10.MTR_TRX+
11.GND
12.GND
13.MNT_TX+
14.GND
15.MNT_TX16.PHZ
17.GND
18.PHA
19.MNT_RX20.PHB
21.MNT_RX+
22.GND
23.GND
24.MOT_TRX25.C2
26.MOT_TRX+
27.GND
28.GND
29.FAN_CNT0
30.PS_STATUS
P5203
P5301
W103
7ZCRD1668*
P3505
J2503
DF20F-30DP
-1H(59)
1.VD
2.GND
3.GND
4.BP
5.BZ
6.GND
7.TIY
8.MTR_TRX9.TIY_RTN
10.MTR_TRX+
11.GND
12.GND
13.MNT_TX+
14.GND
15.MNT_TX16.PHZ
17.GND
18.PHA
19.MNT_RX20.PHB
21.MNT_RX+
22.GND
23.GND
24.MOT_TRX25.C2
26.MOT_TRX+
27.GND
28.GND
29.FAN_CNT0
30.PS_STATUS
W203
7ZCRD1675
J3505
SC02B-J42SK
-GHXPR
1. +32V
2. GND
W104
7ZCRD1671*
FAN
J2501
P2501 PV-3-T
+3.3V
GND
W204 P2502 J2502
PV-3-T
7ZCRD1669*
P2503
J3206
DF20F-10DP-1H(59)
P3206
J5301
SC02B-J42SK-GHXPR
1.+32V
2.GND
W302
Normal:7ZCRD1679*
HS
:7ZCRD1706*
BLK.T
W301
7ZCRD1678*
BLK.T
RED.T
6 RED.T
W303
7ZCRD1670*
J5102
P5102 53426-0210
1.+12V
2.C2
RED.T
WHT.T
TB102
OGM-300NE-6P-04C
J5901
DF3A- 5P-2DSA
1.MNT-RX-P
2.MNT-TX-P
3.MNT-RX-N
4.MNT-TX-N
5.MNTE
TB101
231-344/001-000 [WAGO]
1.VD+
2.VD3.TRIG+
4.TRIG5.BP+
6.BP7.BZ+
8.BZ9.MTR+
10.MTR11.MTRG
12. NC
13. DC48V+
14. DC48VG
REDP5101
BLK
BLU
WHT
YEL
J5101
DF3A-6P-2DS(01)
1.+12V
2.RTN
3.PHA
4.PHB
5.PHZ
6.GND
BLK(SHIELD)
6-177
J5103
P5103 53426-0510
1.+12V
2.RTN
3.MOT_TRX+
4.MOT_TRX5.GND
1.+12V
2.GND
3.MOT_TRX+
4.MOT_TRX5.GND
J1501
P1501 B4P-VH(LF,SN)
1.MU
2.NC
3.MV
4.NC
P1505
J1505
53426-0510(L angle)
P1504
J1504
B3P-VH(LF,SN)
W1
7ZCRD1680*
P3104
J3104
P0B-R-35
PM_OUT
W202
7ZCRD1677*
J1502
J1503
B06BOXASK-1(LF,SN)
1.S1
2.S2
3.S3
4.S4
5.S5
6.S6
1.M1
2.NC
3.M2
4.NC
5.M3
B3P5-VH(LF,SN)
DATA I/F
J2903
FPGA JTAG
J2902
CPU JTAG
J2901
W201
7ZCRD1676*
P3102
J3102
P0B-R-35
RF_ANT
IF_IN(Tx)
W102
7ZCRD1667*
1.R1
2.NC
3.R2
1.GND
2.RF_STC
3.NC
4.LO_MODE
5.GND
6.RF_GATE
7.GND
8.PM_MODE
9.GND
10.TX_MONI
J2303
DF20F-10DP-1H(59) P2303
1.GND
2.RF_STC
3.NC
4.LO_MODE
5.GND
6.RF_GATE
7.GND
8.PM_MODE
9.GND
10.TX_MONI
J3203
27DP-LR-PS-1
IF_OUT(Rx)
P3203
P2302
J2302
27DP-LR-PS-1
IF_IN(Rx)
J3201
27DP-LR-PS-1
P3201
P2301
J2301
27DP-LR-PS-1
IF_OUT(Tx)
J4301
PERFORMANCE
MONITOR ANTENNA
MOTOR
B101
P4301
(N type connector)
P1301
(TRANSDUCER)
(ROTARY JOINT)
“*” means revision of the specfication document.
W501
7ZCRD1674*
W101
7ZCRD1673*
J1301
6. Appendix > 6.6 Scanner Unit Interconnection Unit
6.6.14 NKE-2632/2632-H
6. Appendix > 6.7 External input/output sentence format
6.7
External input/output sentence format
Note: Use external input/output sentence data after NMEA version 2.1
6.7.1
Receivable signals
6.7.1.1 Ship Heading
$--THS,x.x,a*hh
2 34
1.THS
Header
2.x.x
Heading, degrees true
3.a
Mode indicator: A = Autonomous, E = Estimated (dead reckoning)
M = Manual input, S = Simulator mode ,V = Data not valid (including standby)
4.hh
Checksum
$--HDT, x.x, T*hh
2 3
1.HDT
Header
2.x.x
Heading
3.T
Degrees true
6.7.1.2 Course
$--GGA,hhmmss.ss,llll.ll,a,yyyyy.yy,a,x,xx,x.x,x.x,M,x.x,M,x.x,xxxx*hh
34
67
8 9 10 11 12 13 14 15
16
1. GGA
Header
2. hhmmss.ss
UTC of position
3. llll.ll
Latitude
4. a
N/S
5. yyyyy.yy
Longitude
6. a
E/W
7. x
GPS Quality indicator
8. xx
Number of satellites in use, 00-12, may be different from the number in view
9. x.x
Horizontal dilution of precision
10. x.x
Antenna altitude from mean-sea-level (geoid) (m)
11. M
Antenna altitude unit; M=meters
12. x.x
Height difference from WGS-84 earth ellipsoid surface to mean-sea-level
surface (m) = Geoidal separation
13. M
Unit for the height difference from WGS-84 earth ellipsoid surface to
mean-sea-level; M=meters
14. x.x
Age of Differential GPS data (seconds)
15. xxxx
Differential GPS reference station ID (0000 – 1023)
6-178
6. Appendix > 6.7 External input/output sentence format
16. hh
Checksum
$--RMC,hhmmss.ss,A,llll.ll,a,yyyyy.yy,a,x.x,x.x,xxxxxx,x.x,a,a*hh
3 4
8 9
10
11 12 13 14
1. RMC
Header
2. hhmmss.ss
UTC of position fix
3. A
Status; A = Data valid, V = Navigation receiver warning
4. llll.ll
Latitude
5. a
N/S
6. yyyyy.yy
Longitude
7. a
E/W
8. x.x
Speed over ground (knots)
9. x.x
Course Over Ground (degrees, true north)
10. xxxxxx
Date (UTC): ddmmyy
11. x.x
Magnetic variation (degrees)
12. a
Magnetic variation direction E/W
13. a
Mode Indicator; A = Autonomous mode, D = Differential mode, N = Data not valid,
E = Estimated (dead reckoning) mode, M = Manual input mode, S = Simulator mode
14. hh
Checksum
$--RMA, A, llll.ll, a, yyyyy.yy, a, x.x, x.x, x.x, x.x, x.x,a,a*hh
3 4
6 7
9 10 11 12 13 14
1. RMA
Heading
2. A
Status : A = data valid, V = blink, cycle or SNR warning
3. llll.ll
Latitude
4. a
Degrees N/S
5. yyyyy.yy
Longitude
6. a
Degrees E/W
7. x.x
Time difference A, μs
8. x.x
Time difference B, μs
9. x.x
Speed over ground, knots
10. x.x
Course over ground, degrees true
11. x.x
Magnetic variation, degrees E/W
12. a
Degrees E/W
13. a
Mode indicator: A = Autonomous mode; D = Differential mode; E = Estimated (dead reckoning)
mode; M = Manual input mode; S = Simulator mode;N = Data not valid.
14.
hh
Checksum
6-179
6. Appendix > 6.7 External input/output sentence format
$-- GNS, hhmmss.ss, llll.ll, a, yyyyy.yy, a, c--c,xx,x.x,x.x,x.x,x.x,x.x,a *hh
6 7 8 9
10 11 12 13 14 15
1.
GNS
Heading
2.
hhmmss.ss UTC of position
3.
llll.ll
Latitude
4.
N/S
5.
yyyyy.yy
Longitude
6.
Degrees E/W
7.
c—c
Mode indicator
8.
xx
Total number of satellites in use, 00-99
9.
x.x
HDOP
10.
x.x
Antenna altitude, m
11.
x.x
Geoidal separation, m
12.
x.x
Age of differential data
13.
x.x
Differential reference station ID
14.
Navigational status indicator
15.
hh
Checksum
$--GLL,llll.ll,a,yyyyy.yy,a,hhmmss.ss,A,a*hh
23
789
1.GLL
Header
2. llll.ll
Latitude
3. a
N/S
4. yyyyy.yy
Longitude
5. a
E/W
6. hhmmss.ss
UTC of position
7. A
Status; A = Data valid, V = Data not valid
8. a
Mode Indicator; A = Autonomous mode, D = Differential mode, N = Data not valid,
E = Estimated (dead reckoning) mode, M = Manual input mode, S = Simulator
mode
9. hh Checksum
6-180
6. Appendix > 6.7 External input/output sentence format
6.7.1.3 Geodetic positioning system
$--DTM,ccc,a,x.x,a,x.x,a,x.x,ccc*hh
34 56 78 9
1. DTM
10
Header (Datum Reference)
2. ccc
Local (geodetic reference) datum code; W84 = WGS84, W72 = WGS72,S85
=SGS85, P90 = PE90, 999 = User defined, IHO datum code
3. a
Local datum subdivision code
4. x.x
Latitude offset (minutes)
5. a
N/S
6. x.x
Longitude offset (minutes)
7. a
E/W
8. x.x
Altitude offset (meters)
9. ccc
Reference
datum
code
(Geodetic
reference
system
to
which
conformed);W84 = WGS84, W72 = WGS72, S85 = SGS85, P90 = PE90
10. hh
Checksum
6.7.1.4 Date information
$--ZDA,hhmmss.ss,xx,xx,xxxx,xx,xx*hh
5 6 7
1. ZDA
Header (Time & Date)
2. hhmmss.ss
UTC
3. xx
Day (UTC)
4. xx
Month (UTC)
5. xxxx
Year (UTC)
6. xx
Local zone hours, 00 to +13 hrs
7. xx
Local zone minutes, 00 to +59
8. hh
Checksum
6-181
being
6. Appendix > 6.7 External input/output sentence format
6.7.1.5 COG/SOG
$--RMC,hhmmss.ss,A,llll.ll,a,yyyyy.yy,a,x.x,x.x,xxxxxx,x.x,a,a*hh
3 4
5 6
8 9
10
11 12 13 14
1. RMC
Header
2. hhmmss.ss
UTC of position fix
3. A
Status; A = Data valid, V = Navigation receiver warning
4. llll.ll
Latitude
5. a
N/S
6. yyyyy.yy
Longitude
7. a
E/W
8. x.x
Speed over ground (knots)
9. x.x
Course Over Ground (degrees, true north)
10. xxxxxx
Date (UTC): ddmmyy
11. x.x
Magnetic variation (degrees)
12. a
Magnetic variation direction E/W
13. a
Mode Indicator; A = Autonomous mode, D = Differential mode, N = Data not
valid, E = Estimated (dead reckoning) mode, M = Manual input mode, S =
Simulator mode
14. hh
Checksum
$--RMA, A, llll.ll, a, yyyyy.yy, a, x.x, x.x, x.x, x.x, x.x,a,a*hh
2 3
6 7
9 10
11 12 13 14
1. RMA
Heading
2. A
Status : A = data valid, V = blink, cycle or SNR warning
3. llll.ll
Latitude
4. a
Degrees N/S
5. yyyyy.yy
Longitude
6. a
Degrees E/W
7. x.x
Time difference A, μs
8. x.x
Time difference B, μs
9. x.x
Speed over ground, knots
10. x.x
Course over ground, degrees true
11. x.x
Magnetic variation, degrees E/W
12. a
Degrees E/W
13. a
Mode indicator: D = Differential mode; E = Estimated (dead reckoning) mode;
M = Manual input mode; S = Simulator mode;N = Data not valid.
14.
hh
Checksum
6-182
6. Appendix > 6.7 External input/output sentence format
$--VTG,x.x,T,x.x,M,x.x,N,x.x,K,a*hh
2 3
4 5 6
8 9 10 11
1. VTG
Header
2. x.x
Course over ground based on true north (degrees)
3. T
Unit of course over ground; T = True
4. x.x
Course over ground based on magnetic north (degrees)
5. M
Unit of course over ground; M = Magnetic
6. x.x
Speed over ground (knots)
7. N
Speed over ground unit; N = knots
8. x.x
Speed over ground (km/h)
9. K
Speed over ground unit; K = km/hr
10. a
Mode Indicator; A = Autonomous mode, D = Differential mode, N = Data not valid,
E = Estimated (dead reckoning) mode, M = Manual input mode, S = Simulator
mode
11. hh
Checksum
6.7.1.6 Ship speed through water
$--VBW,x.x,x.x,A,x.x,x.x,A,x.x,A,x.x,A*hh
3 4 5 6 7 8 9 10 11 12
1. VBW
Header
2. x.x
Longitudinal water speed (knots)
3. x.x
Transverse water speed (knots)
4. A
Status of water speed; A = Data valid
5. x.x
Longitudinal ground speed (knots)
6. x.x
Transverse ground speed (knots)
7. A
Status of ground speed; A = Data valid
8. x.x
Stern transverse water speed (knots)
9. A
Status of stern transverse water speed; A = Data valid
10. x.x
Stern transverse ground speed (knots)
11. A
Status of stern transverse ground speed; A = Data valid, V = Invalid
12. hh
Checksum
6.7.1.7 Turning speed
$--ROT, x.x, A*hh
3 4
1. ROT
Header
2. x.x
Rate of turn, °/min, "-" = bow turns to port
3. A
Status: A = data valid, V = data invalid
4.hh
Checksum
6-183
6. Appendix > 6.7 External input/output sentence format
6.7.1.8 Water depth
$--DPT,x.x,x.x,x.x*hh
3 4 5
1. DPT
Header
2. x.x
Water depth relative to the transducer (meters)
3. x.x
Offset from transducer (meters)
4. x.x
Maximum range scale in use
5. hh
Checksum
$--DBS,x.x,f,x.x,M,x.x,F*hh
34 5 6
78
1. SDDBS
Header
2. x.x
Water depth from ship’s bottom (feet)
3. f
Units (feet)
4. x.x
Water depth from ship’s bottom (meters)
5. M
Units (meters)
6. x.x
Water depth from ship’s bottom (fathoms)
7. F
Units (fathoms)
8. hh
Checksum
$--DBT,x.x,f,x.x,M,x.x,F*hh
23
4 5 6
1. DBT
Header
2. x.x
Water depth from ship’s bottom (feet)
3. f
Units (feet)
4. x.x
Water depth from ship’s bottom (meters)
5. M
Units (meters)
6. x.x
Water depth from ship’s bottom (fathoms)
7. F
Units (fathoms)
8. hh
Checksum
$--DBK,x.x,f,x.x,M,x.x,F*hh
23
4 5 67
1. DBK
Header
2. x.x
Water depth from ship’s bottom (feet)
3. f
Units (feet)
4. x.x
Water depth from ship’s bottom (meters)
5. M
Units (meters)
6. x.x
Water depth from ship’s bottom (fathoms)
7. F
Units (fathoms)
8. hh
Checksum
6-184
6. Appendix > 6.7 External input/output sentence format
6.7.1.9 Wind direction/wind speed
$--MWV, x.x, a, x.x, a, A *hh
3 4 5
6 7
1.MWV
Heading
2.x.x
Wind angle, 0° to 359°
3.a
Reference, R = relative, T=true
4.x.x
Wind speed
5.a
Wind speed units, K = km/h, M = m/s, N = knots
6.A
Status, A = data valid V= data invalid
7.hh
Checksum
$--MWD, x.x,T,x.x,M,x.x,N,x.x,M*hh
1.MWD
Heading
2.x.x,T
Wind direction, 0° to 359° true
3.x.x,M
Wind direction, 0° to 359° magnetic
4.x.x,N
Wind speed, knots
5.x.x.M
Wind speed, m/s
6.7.1.10 Air temperature
$--XDR, a, x.x, a, c--c,................ a, x.x, a, c--c*hh
4 5
1.XDR
Heading
2.a
Transducer type, transducer No. 1
3.x.x
Measurement data, transducer No. 1
4.a
Units of measure, transducer No. 1
5. c--c
Transducer No. 1 ID
6. ................
a Data, variable number of transducers
7. a, x.x, a, c--c
Transducer "n"
8.hh
Checksum
$--MTA,x.x,C*hh
1.--MTA
Header
2. x.x,C
Temperature, degrees C
3.hh
Checksum
6-185
6. Appendix > 6.7 External input/output sentence format
$--MDA,x.x,I,x.x,B,x.x,C,x.x,C,x.x,x.x,x.x,C,x.x,T,x.x,M,x.x,N,x.x,M*hh
10
11
12
13
1.--MDA
Header
2. x.x,I
Barometric pressure, inches of mercury
3. x.x,B
Barometric pressure, bars
4. x.x,C
Air temperature, degrees C
5. x.x,C
Water temperature, degrees C
6. x.x
Relative humidity, percent
7. x.x
Absolute humidity, percent
8. x.x.C
Dew point, degrees C
9.x.x.T
Wind direction, degrees True
10. x.x.M
Wind direction, degrees Magnetic
11. x.x.N
Wind speed, knots
12. x.x.M
Wind speed, meters/second
13. hh
Checksum
6.7.1.11 Water temperature
$-- MTW, x.x, C*hh
1.MTW
Heading
2.x.x, C
Temperature, degrees C
3.hh
Checksum
$--MDA,x.x,I,x.x,B,x.x,C,x.x,C,x.x,x.x,x.x,C,x.x,T,x.x,M,x.x,N,x.x,M*hh
10
11
12
13
1.MDA
Header
2. x.x,I
Barometric pressure, inches of mercury
3. x.x,B
Barometric pressure, bars
4. x.x,C
Air temperature, degrees C
5. x.x,C
Water temperature, degrees C
6. x.x
Relative humidity, percent
7. x.x
Absolute humidity, percent
8. x.x.C
Dew point, degrees C
9.x.x.T
Wind direction, degrees True
10. x.x.M
Wind direction, degrees Magnetic
11. x.x.N
Wind speed, knots
12. x.x.M
Wind speed, meters/second
13. hh
Checksum
6-186
6. Appendix > 6.7 External input/output sentence format
6.7.1.12 Atmospheric pressure
$--XDR, a, x.x, a, c--c,................ a, x.x, a, c--c*hh
4 5
1.XDR
Heading
2.a
Transducer type, transducer No. 1
3.x.x
Measurement data, transducer No. 1
4.a
Units of measure, transducer No. 1
5. c--c
Transducer No. 1 ID
6. ................
a Data, variable number of transducers
7. a, x.x, a, c--c
Transducer "n"
8.hh
Checksum
$--MMB,x.x,I,x.x,B*hh
1.MMB
Header
2. x.x,I
Barometric pressure, bars
3. x.x,B
Barometric pressure, inches of mercury
4.hh
Checksum
$--MDA,x.x,I,x.x,B,x.x,C,x.x,C,x.x,x.x,x.x,C,x.x,T,x.x,M,x.x,N,x.x,M*hh
10
11
12
13
1.MDA
Header
2. x.x,I
Barometric pressure, inches of mercury
3. x.x,B
Barometric pressure, bars
4. x.x,C
Air temperature, degrees C
5. x.x,C
Water temperature, degrees C
6. x.x
Relative humidity, percent
7. x.x
Absolute humidity, percent
8. x.x.C
Dew point, degrees C
9.x.x.T
Wind direction, degrees True
10. x.x.M
Wind direction, degrees Magnetic
11. x.x.N
Wind speed, knots
12. x.x.M
Wind speed, meters/second
13. hh
Checksum
6-187
6. Appendix > 6.7 External input/output sentence format
6.7.1.13 Humidity
$--XDR, a, x.x, a, c--c,................ a, x.x, a, c--c*hh
4 5
1.XDR
Heading
2.a
Transducer type, transducer No. 1
3.x.x
Measurement data, transducer No. 1
4.a
Units of measure, transducer No. 1
5. c--c
Transducer No. 1 ID
6. ................
a Data, variable number of transducers
7. a, x.x, a, c--c
Transducer "n"
8.hh
Checksum
$--MHU,x.x,x.x,x.x,C*hh
1.MHU
Header
2.x.x
Relative humidity, percent
3.x.x
Absolute humidity, percent
4.x.x,C
Dew point, degrees C
5.hh
Checksum
$--MDA,x.x,I,x.x,B,x.x,C,x.x,C,x.x,x.x,x.x,C,x.x,T,x.x,M,x.x,N,x.x,M*hh
10
11
12
13
1.MDA
Header
2. x.x,I
Barometric pressure, inches of mercury
3. x.x,B
Barometric pressure, bars
4. x.x,C
Air temperature, degrees C
5. x.x,C
Water temperature, degrees C
6. x.x
Relative humidity, percent
7. x.x
Absolute humidity, percent
8. x.x.C
Dew point, degrees C
9.x.x.T
Wind direction, degrees True
10. x.x.M
Wind direction, degrees Magnetic
11. x.x.N
Wind speed, knots
12. x.x.M
Wind speed, meters/second
13. hh
Checksum
6-188
6. Appendix > 6.7 External input/output sentence format
6.7.1.14 AIS
!--VDM,x,x,x,a,s—s,x*hh
1 2345
6 78
1.VDM
Header
2.x
Total number of sentences needed to transfer the message,1 to 9
3.x
Sentence number, 1 to 9
4.x
Sequential message identifier, 0 to 9
5.a
AIS channel
6.s—s
Encapsulated ITU-R M.1371 radio message
7. x
Number of fill-bits, 0 to 5
8.hh
Checksum
!--VDO,x,x,x,a,s—s,x*hh
2345
6 7 8
1.VDO
Header
2.x
Total number of sentences needed to transfer the message, 1 to 9
3.x
Sentence number, 1 to 9
4.x
Sequential message identifier, 0 to 9
5.a
AIS Channel
6.s—s
Encapsulated ITU-R M.1371 radio message
7.x
Number of fill-bits, 0 to 5
8.hh
Checksum
6.7.1.15 Alert
$--ACK,xxx*hh
2 3
1.ACK
Header
2.xxx
Unique alarm number (identifier) at alarm source
3.hh
Checksum
$--ALR,hhmmss.ss,xxx,A, A,c--c*hh
3 4
5 6 7
1.ALR
Header
2. hhmmss.ss
Time of alarm condition change, UTC
3. xxx
Unique alarm number (identifier) at alarm source
4.A
Alarm condition (A = threshold exceeded, V = not exceeded)
5.A
Alarm’s acknowledge state, A = acknowledged,V = unacknowledged
6. c—c
Alarm’s description text
7.hh
Checksum
6-189
6. Appendix > 6.7 External input/output sentence format
6.7.2
Transmittable signals
6.7.2.1 RADAR system data
$--RSD, x.x, x.x,x.x, x.x,x.x, x.x,x.x, x.x,x.x, x.x, x.x, a, a*hh
3 4
7 8
10 11
12 13 14 15
1. RSD
Header
2. x.x
Origin 1 range (see Note 2), from own ship
3. x.x
Origin 1 bearing (see Note 2) degrees from 0°
4. x.x
Variable range marker 1 (VRM1), range
5. x.x
Bearing line 1 (EBL1), degrees from 0°
6. x.x
Origin 2 range (see Note 2)
7. x.x
Origin 2 bearing (see Note 2)
8. x.x
VRM 2, range
9. x.x
EBL 2, degrees
10. x.x
Cursor range, from own ship
11. x.x
Cursor bearing, degrees clockwise from 0°
12. x.x
Range scale in use
13. x.x
Range units, K = km,N = nautical miles, S = statute miles
14.a,a
Display rotation
15.hh
Checksum
6.7.2.2 Own ship data
$--OSD, x.x,A,x.x, a,x.x,a,x.x,x.x,a*hh
34
5 6 7 8 9 10 11
1.OSD
Header
2.x.x
Heading, degrees true
3.A
Heading status: A = data valid, V = data invalid
4.x.x
Vessel course, degrees true
5.a
Course reference,
B = bottom tracking log, M = manually entered, W = water referenced,
R = radar tracking (of fixed target), P = positioning system ground reference.
6.x.x
Vessel speed
7.x.x
Speed reference,
B = bottom tracking log, M = manually entered, W = water referenced,
R = radar tracking (of fixed target), P = positioning system ground reference.
8.x.x
Vessel set, degrees true
9.x.x
Vessel drift (speed)
10.x.x
Speed units, K = km/h; N = knots; S = statute miles/h
11.hh
Checksum
6-190
6. Appendix > 6.7 External input/output sentence format
6.7.2.3 Watch timer reset
$--EVE,hhmmss.ss,c--c,c--c*hh
1.EVE
Header
2.hhmmss.ss
Event time
3.c—c
Tag code used for identification of source of event
4.c—c
Event description
5.hh
Checksum
6.7.2.4 TT data, AIS target data
$--TTM,xx,x.x,x.x,a,x.x,x.x,a,x.x,x.x,a,c--c,a,a,hhmmss.ss,a*hh
2 3
4 5 6
78
9 10 11 12 13 14
15
1617 18
1. TTM
Header (Track Target Message)
2. xx
Target number (00-99)
3. x.x
Target distance from own ship
4. x.x
Target bearing from own ship (degrees)
5. a
Reference of target bearing from own ship; T = True, R = Relative
6. x.x
Target speed
7. x.x
Target course (degrees)
8. a
Reference of target course; T = True, R = Relative
9. x.x
Distance of closest-point-of-approach
10. x.x
Time to CPA (minutes), “-“ = increasing
11. a
Speed/distance units (K/N/S)
12. c—c
Target name
13. a
Target status; L = Lost (tracked target has been lost),
Q = Query (target in the process of acquisition), T = Tracking
14. a
Reference target; R = Reference (target is a reference used to determined
own-ship position or velocity), null = other than reference
15. hhmmss.ss
UTC of data
16. a
Type of acquisition; A = Auto, M = Manual, R = Reported
17. hh
Checksum
6-191
6. Appendix > 6.7 External input/output sentence format
$--TLL, xx, llll.ll, a, yyyyy.yy, a, c--c, hhmmss.ss, a, a*hh
78
1.TLL
Header
2.xx
Target number 00 – 99
3. llll.ll, NS
Target latitude, N/S
4. yyyyy.yy,a
Target longitude, E/W
5. c—c
Target name
6. hhmmss.ss
UTC of data
7. a
Target status
8. a
Reference target = R, null otherwise
9.hh
Checksum
!--TTD,hh,hh,x,s—s,x*hh
2 34 5
6 7
1.TTD
Header
2.hh
Total hex number of sentences needed to transfer the message, 01 to FF
3.hh
Hex sentence number, 01 to FF
4.x
Sequential message identifier, 0 to 9
5.s--s
Encapsulated tracked target data
6.x
Number of fill-bits, 0 to 5
7.hh
Checksum
$--TLB,x.x,c--c,x.x,c--c,...x.x,c--c*hh
2 3
1.TLB
Header
2.x.x
Target number ‘n’ reported by the device.
3.c—c
Label assigned to target ‘n’
4.x.x,c—c
Additional label pairs
5.hh
Checksum
6-192
6. Appendix > 6.7 External input/output sentence format
6.7.2.5 AIS remote control data
$--VSD,x.x,x.x,x.x,c—c,hhmmss.ss,xx,xx,x.x,x.x*hh
2 3
7 8
9 10
11
1.VSD
Header
2.x.x
Type of ship and cargo category, 0 to 255
3.x.x
Maximum present static draught, 0 to 25,5 m
4.x.x
Persons on-board, 0 to 8 191
5.c—c
Destination, 1-20 characters
6. hhmmss.ss
Estimated UTC of arrival at destination
7.xx
Estimated day of arrival at destination, 00 to 31 (UTC)
8.xx
Estimated month of arrival at destination, 00 to 12 (UTC)
9.x.x
Navigational status, 0 to 15
10.x.x
Regional application flags
11.hh
Checksum
$--AIR,xxxxxxxxx,x.x,x,x.x,x,xxxxxxxxx,x.x,x,a,x.x,x.x,x.x*hh
3 4 56
8 9 10 11 12
13 14
1.AIR
Header
2. xxxxxxxxx
MMSI of interrogated station-1
3.x.x
First message number requested from station-1
4.x
Message sub-section
5.x.x
Second message number requested from station-1
6.x
Message sub-section
7. xxxxxxxxx
MMSI of interrogated station-2
8.x.x
Message Number requested from station-2
9.x
Message sub-section
10.a
Channel of interrogation
11.x.x
Message ID1.1, station-1 reply slot
12.x.x
Message ID1.2, station-1 reply slot
13.x.x
Message ID2.1, station-2 reply slot
14.hh
Checksum
$--AIQ,xxx.*hh
1—AIQ
Header
2.xxx
request of static information (VSD, ACA, etc.)
3.hh
Checksum
6-193
6. Appendix > 6.7 External input/output sentence format
!--ABM,x,x,x,xxxxxxxxx,x,xx,s—s,x*hh
1 234
7 8 9 10
1.AMB
Header
2. x
Total number of sentences needed to transfer the message,1 to 9
3. x
Sentence number, 1 to 9
4. x
Sequential message identifier
5. xxxxxxxxx
The MMSI of the destination AIS unit for the ITU-R M.1371 Message 6 or 12
6. x
AIS channel for broadcast of the radio message
7. xx
ITU-R M.1371 Message ID
8. s—s
Encapsulated data
9. x
Number of fill-bits, 0 to 5
10. hh
Checksum
!--BBM,x,x,x,x,xx,s—s,x*hh
234 56
89
1.--BBM
Header
2.x
Total number of sentences needed to transfer the message,1 to 9
3.x
Sentence number, 1 to 9
4.x
Sequential message identifier, 0 to 9
5.x
AIS channel for broadcast of the radio message
6.xx
ITU-R M.1371 Message ID
7.s—s
Encapsulated data
8.x
Number of fill-bits, 0 to 5
9.hh
Checksum
6.7.2.6 Remote control data
JRC format
$PJRC,s—s*hh
2 3
1.PJRC
Header
2.s—s
Data field
3.hh
Checksum
6-194
6. Appendix > 6.7 External input/output sentence format
6.7.2.7 Alert
$--ACK,xxx*hh
2 3
1.ACK
Header
2.xxx
Unique alarm number (identifier) at alarm source
3.hh
Checksum
$--ALR,hhmmss.ss,xxx,A, A,c--c*hh
3 4
5 6 7
1.ALR
Header
2. hhmmss.ss
Time of alarm condition change, UTC
3. xxx
Unique alarm number (identifier) at alarm source
4.A
Alarm condition (A = threshold exceeded, V = not exceeded)
5.A
Alarm’s acknowledge state, A = acknowledged,
V =unacknowledged
6. c—c
Alarm’s description text
7.hh
Checksum
6-195
6. Appendix > 6.8 Setting for the route transfer by LAN connection with the GPS
6.8
Setting for the route transfer by LAN connection
with the GPS
6.8.1
How to set the IP address of GPS
1. Refer to "4.20 Equipment Configuration" and display the equipment configuration menu.
2. Press
"IP".
(1) IP ADDRESS Configuration
3. Press
4. Press
"IP ADDR".
to select "INPUT", and press
5. Enter the IP address with the numeric keypad, and press
To return the value to the default value, select "DEFAULT" and press
(2) SUBNET MASK Configuration
6. Press
7. Press
"SUBNET MASK".
to select "INPUT", and press
8. Enter the subnet mask with the numeric keypad, and press
To return the value to the default value, select "DEFAULT" and press
(3) DEFAULT GATEWAY Configuration
9. Press
10. Press
"DEFAULT GATEWAY".
to select "INPUT", and press
11. Enter the default gateway with the numeric keypad, and press
To return the value to the default value, select "DEFAULT" and press
6-196
6. Appendix > 6.8 Setting for the route transfer by LAN connection with the GPS
6.8.2
Setting of the LAN for GPS
· LAN configuration can be performed for active route sharing, data route sharing, data output,
mutual monitoring, and remote maintenance output.
· In data output, the output NMEA sentence can be selected.
· To share active or data routes, sharing route configuration must be performed.
Set the route sharing setting to "SHARE" for data routes.
When set to "SHARE", data route reception will occur automatically.
For active routes, set the route sharing setting to "SHARE 1", "SHARE 2", "SHARE 3",
"SHARE 4" or "SHARE 5".
(1) SHARE1:
If the active route is switched on the unit, the route will automatically be sent
out to connected equipment.
When a shared route is received, the route is automatically switched.
(2) SHARE2:
If the active route is switched on the unit, a request is made to the user of
the unit before the route is sent. Transmission of the route to the connected
equipment is dependant on the permission of the user.
If the user has not authorized sending, the active route will only be executed
on the local unit.
When a shared route is received, the route is automatically switched.
(3) SHARE3:
If the active route is switched on the unit, the route will automatically be sent
out to connected equipment.
When a shared route is received, the user is asked whether or not they want
to switch routes.
If the user does not authorize route switching, the route will not be switched.
(4) SHARE4:
If the active route is switched on the unit, a request is made to the user of
the unit before the route is sent. Transmission of the route to the connected
equipment is dependant on the permission of the user.
If the user has not authorized sending, the active route will only be executed
on the local unit.
When a shared route is received, the user is asked whether or not they want
to switch routes.
If the user does not authorize route switching, the route will not be switched.
(5) SHARE5:
The active route cannot be sent
When a shared route is received, the route is automatically switched.
The following icon is displayed when active routes are shared.
SHARE1 Icon:
SHARE2 Icon:
SHARE3 Icon:
SHARE5 Icon:
6-197
SHARE4 Icon:
6. Appendix > 6.8 Setting for the route transfer by LAN connection with the GPS
· To perform mutual monitoring, mutual monitoring mode must be configured. With mutual
monitoring mode, when GPS positioning is not being performed, the GPS positioning
information from other units can be displayed.
· Remote maintenance output configuration can be used to regularly output data for use in
remote maintenance
LAN 設定プルダウン
Data output setting
ACTIVE route sharing setting
DATA route sharing setting
Mutual monitoring mode setting
Remote maintenance output setting
LAN Selection Screen
1. Refer to "4.20 Equipment Configuration" and display the equipment configuration menu.
2. Press
, then
, and select "LAN".
3. Press
to select "ACTIVE ROUTE", and press
4. Press
to select "SHARE1", "SHARE2", "SHARE3", "SHARE4", or "SHARE5", and
press
to display the connection destination screen.
Select "OFF" to disable sharing.
5. Press
"CONNECT", select the destination, and press
Normally, "MULTICAST" should be selected for the destination.
To send to a specific unit, select "UNICAST".
6. When "UNICAST" is selected, press
and
and "3.PORT No.".
6-198
to select the destination IP "2.TO IP"
6. Appendix > 6.9 Specification of alert communication with BNWAS
6.9
Specification of alert communication with BNWAS
6.9.1
System Block Diagram
6.9.1.1 Connection Diagram
6.9.1.2 Function Diagram
(1).
INS Alert and Back-up navigator call
6-199
6. Appendix > 6.9 Specification of alert communication with BNWAS
(2).
BNWAS alert
(3).
Watch Timer Reset
(4).
Connection supervision
6-200
6. Appendix > 6.9 Specification of alert communication with BNWAS
6.9.2
Mechanism
6.9.2.1 BNWAS status
6-201
6. Appendix > 6.9 Specification of alert communication with BNWAS
6.9.2.2 Watch alarm
6-202
6. Appendix > 6.9 Specification of alert communication with BNWAS
6.9.2.3 Alarm transfer
(1).
Alarm transfer
6-203
6. Appendix > 6.9 Specification of alert communication with BNWAS
(2).
Acknowledge to alert
6-204
6. Appendix > 6.9 Specification of alert communication with BNWAS
(3).
Acknowledge to 2nd/3rd stage remote audible alert
6-205
6. Appendix > 6.9 Specification of alert communication with BNWAS
(4).
Rectified
6-206
6. Appendix > 6.9 Specification of alert communication with BNWAS
6.9.3
No
Sentences
mnemonic
Meaning
Remarks
ACK
Acknowledge alert
This
sentence
is
used
to
acknowledge
an
Category-B alert condition reported by a device.
ALR
Set alert state
This sentence is used to report an alert condition on
a device and its current state of acknowledgement.
EVE
Watch Timer reset
JRC-INS to BNWAS for timer-reset.
(IEC 62616/7.4.6)
HBT
Heartbeat supervision sentence
This sentence is intended to be used to indicate that
equipment is operating normally, or for supervision of
a connection between JRC-INS and BNWAS.
6.9.3.1 Talker ID
No.
Source
Talker ID
Remark
BNWAS
BN
IEC 61162/Table 4
RADAR
RA
IEC 61162/Table 4
ECDIS
EI
IEC 61162/Table 4
INS/ CONNING/ AMS
IN
IEC 61162/Table 4
6.9.3.2 ACK sentence
$INALR,xxx*hh
(INS -> BMWAS)
$BNALR,xxx*hh
(BNWAS -> INS)
Alert number
See. Alert number table(Described later)
6-207
6. Appendix > 6.9 Specification of alert communication with BNWAS
6.9.3.3 ALR sentence
Transmit : interval from 1sec to 15sec for BNWAS, from 1 sec to 3 sec for AMS.
$INALR,hhmmss.ss,xxx,A,A,c--c*hh
(INS -> BMWAS)
$BNALR,hhmmss.ss,xxx,A,A,c--c*hh
(BNWAS -> INS)
Alert’s description text
If unnecessary, null is OK.
Alert’s acknowledge state
Acknowledged
Unacknowledged
Alert condition
Threshold exceeded
Not exceeded
Alert number
See Alert number table(Described later)
Time of alert condition change. UTC
UTC
or if time cannot be inserted, null is OK.
6-208
6. Appendix > 6.9 Specification of alert communication with BNWAS
Alert number (sample)
alert number
(none)
000
source
mean
remark
JRC-INS, BNWAS
no-alerts message
IEC 61924-2/L.1.3
BNWAS
Dormant period report
Category-B
IEC 62616 Ed1.0/6.2
001
BNWAS
System fail
Category-B
002
BNWAS
Power fail
Category-B
260
AMS
Emergency call (Back-up Navigator Call)
IEC 61924-2/J.2
300
No.1 RADAR
ARPA(CPA/TCPA) alert
Category-A
301
No.1 RADAR
Power & System fail
Category-B
302
No.2 RADAR
ARPA(CPA/TCPA) alert
Category-A
303
No.2 RADAR
Power & System fail
Category-B
304
No.3 RADAR
ARPA(CPA/TCPA) alert
Category-A
305
No.3 RADAR
Power & System fail
Category-B
310
ECDIS
Cross-Track (Off-Track)
Category-A
311
ECDIS
Course Difference (Off course)
Category-A
312
ECDIS
Wheel Over Line (ACCA)
Category-A
313
ECDIS
End Of Track
Category-A
314
ECDIS
Depth below keel
Category-A
315
ECDIS
Power & System fail
Category-B
320
Backup-ECDIS
Cross-Track (Off-Track)
Category-A
321
Backup-ECDIS
Course Difference (Off course)
Category-A
322
Backup-ECDIS
Wheel Over Line (ACCA)
Category-A
323
Backup-ECDIS
End Of Track
Category-A
324
Backup-ECDIS
Depth below keel
Category-A
325
Backup-ECDIS
Power & System fail
Category-B
350
CONNING
Power & System fail
Category-B
360
No.1 DGPS
Power & System fail
Category-B/Warning
361
No.2 DGPS
Power & System fail
Category-B/Warning
362
No.1 Gyro Compass
Power & System fail
Category-B/Warning
363
No.2 Gyro Compass
Power & System fail
Category-B/Warning
364
No.1 Speed Log
Power & System fail
Category-B/Warning
365
No.2 Speed Log
Power & System fail
Category-B/Warning
366
Echo Sounder
Power & System fail
Category-B/Warning
367
AIS
Power & System fail
Category-B/Warning
368
Auto Pilot
Power & System fail
Category-B/Warning
369
NAVTEX
Power & System fail
Category-B/Warning
370
VDR
Power & System fail
Category-B/Warning
371
Clock
Power & System fail
Category-B/Warning
6-209
6. Appendix > 6.9 Specification of alert communication with BNWAS
372
GMDSS
Power & System fail
Category-B/Warning
373
No.1 Main SLC
Power & System fail
Category-B/Warning
374
No.2 Main SLC
Power & System fail
Category-B/Warning
375
No.3 Main SLC
Power & System fail
Category-B/Warning
376
No.1 Sub SLC
Power & System fail
Category-B/Warning
377
No.2 Sub SLC
Power & System fail
Category-B/Warning
378
No.3 Sub SLC
Power & System fail
Category-B/Warning
379
No.1 ALC
Power & System fail
Category-B/Warning
380
No.2 ALC
Power & System fail
Category-B/Warning
381
No.3 ALC
Power & System fail
Category-B/Warning
999
JRC-INS, BNWAS
Buzzer off request
original
6.9.3.4 No-alert message
When there is no alarm, this message will be sent from BNWAS or INS to the another.
$INALR,,,V,V,*hh
(INS -> BNWAS)
$BNALR,,,V,V,*hh
(BNWAS -> INS)
Note) see IEC 61924-2/L1.3
6.9.3.5 Back-up navigator call
For Back-up navigator call, emergency message sentence will be sent from AMS to BNWAS:
$INALR,,260,A,V,Emergency Call*hh
For removing Back up navigator call:
$INALR,,260,A,A,Emergency Call*hh
Note) see IEC 61924-2/J.2
6.9.3.6 Buzzer off request
For request buzzer off, this message will be used.
Transmit : 1 time
$INALR,,999,A,A,BZ off*hh
(INS -> BNWAS)
$BNALR,,999,A,A,BZ off*hh
(BNWAS -> INS)
6-210
6. Appendix > 6.9 Specification of alert communication with BNWAS
6.9.3.7 Dormant period report
The ALR sentence is used for dormant period report from BNWAS to AMS.
$BNALR, hhmmss.ss, 000, A, A, c1;c2;c3*hh
Alarm stage
1,2 or 3
Dormant period in min
03 - 12
AUT or MAN or OFF
Alarm’s acknowledge state
A = Acknowledged
V = Unacknowledged
Dormant period condition
A = Threshold exceeded
V = Not exceeded
Alert number = 000
Time of alert condition change.
UTC or if time cannot be inserted, null is OK.
Example:
$BNALR,,000,A,V,C1=AUT;C2=03;C3=1*hh
The alarm message shall be sent with any change of the BNWAS settings for mode or dormant period, and
with any activated and reset alarm.
2nd and 3rd alarm should be acknowledged by “$INACK,,000*hhLF>” from AMS.
Note) see IEC 62616 Ed1.0/6.2
6.9.3.8 EVE sentence
For reset of the Watch Timer, EVE sentence will be sent from individual equipment in INS except ALC to
BNWAS.
Transmit : minimum interval is 1 sec per equipment.
$EIEVE,,BNWAS,Operator activity*hh
(ECDIS -> BNWAS)
$RAEVE,,BNWAS,Operator activity*hh
(RADAR -> BNWAS)
$INEVE,,BNWAS,Operator activity*hh
(CONNING/AMS -> BNWAS)
Event description
Fixed string “Operator activity”
Tag code
Fixed string “BNWAS”
Event time
Null
6-211
6. Appendix > 6.9 Specification of alert communication with BNWAS
see IEC 62616/7.4.6.
6.9.3.9 HBT sentence
This sentence is intended to be used for supervision of a connection between AMS and BNWAS.
Transmit : interval from 1 sec to 3 sec.
$INHBT,x.x,A,x*hh
(INS -> BNWAS)
$BNHBT,x.x,A,x*hh
(BNWAS -> INS)
Sequential sentence identifier
Changing sentence counter. Number from 0
to 9.
Equipment status
Fix
Configured repeat interval
1.0
6-212
Fix
6. Appendix > 6.10 Troubleshooting
6.10
Troubleshooting
When this equipment does not operate correctly, check the following points before asking for repairs.
Consult with your nearest subsidiary company, branch office, or sales office if the problem does not get solved
even after checking and correcting these points, or if there are any abnormally locations other than the
following items.
Symptom
The power is not
supplied.
Alternatively, the
equipment does not start
even if the Power button
of the operation unit is
pressed.
The power is not
supplied to the monitor.
Although the power is
supplied to the monitor,
the screen is not
displayed.
The brightness of the
monitor cannot be
adjusted.
Cause
Action
The AC or DC power supply is not
connected.
Connect the AC or DC power supply.
The circuit breaker at the front of
the PSU (NBD-913) is not set to
ON.
Set the breaker to ON by pushing up
the lever of the breaker.
The AC or DC power supply is not
input within the specified voltage
range.
Connect the AC or DC power supply
within the specified voltage range.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The PSU (NBD-913) is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
The CCU (NCE-5605) is faulty.
Make a request to the distributor for
repair.
The display unit is not activated.
Activate the display unit.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The MNU (NWZ-208/NWZ-207) is
faulty.
Make a request to the distributor for
repair.
The brightness of the monitor is set Adjust the brightness of the monitor
to the minimum level.
to the appropriate level.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The MNU (NWZ-208/NWZ-207) is
faulty.
Make a request to the distributor for
repair.
The MNU (NWZ-208/NWZ-207) is
faulty.
Make a request to the distributor for
repair.
The internal wiring is faulty.
The trackball or the
option keyboard cannot
be operated.
The display unit
(NCE-5605/NCE5625) is faulty.
6-213
Make a request to the distributor for
repair.
Make a request to the distributor for
repair.
6. Appendix > 6.10 Troubleshooting
Symptom
The trackball does
cannot be moved
smoothly.
Cause
Action
The trackball is dirty.
Clean the trackball.
Although the power is The CCU (NDC-1590) is abnormal. Make a request to the distributor for
supplied and the screen
repair.
is displayed, the display
is frozen, disabling
processing to advance
up to display of the task
menu.
Some task menus
cannot be selected.
The device license has not been
installed.
Install the license of the device to be
used.
The cursor is not
displayed correctly.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
Characters/symbols are The CCU (NDC-1590) is faulty.
not displayed correctly.
Make a request to the distributor for
repair.
Position information
The communication is not set
(GPS) is not displayed. correctly.
Set the communication correctly.
The power supply for the GPS unit Turn on the power supply for the
is not turned on.
GPS unit.
The GPS unit does not perform
positioning.
Check the state of the GPS unit.
The connection with the GPS unit is Check the connection with the GPS
abnormal.
unit.
If a GPS unit is connected to the
SLC, check that the LED of the
corresponding port is lit during data
reception.
The power supply for the SLC
(CMH-2370) is not turned on.
(Case where the GPS unit is
connected to the SLC)
Turn on the power supply for the
SLC.
The SLC (CMH-2370) is faulty.
(Case where the GPS unit is
connected to the SLC)
Make a request to the distributor for
repair.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
6-214
6. Appendix > 6.10 Troubleshooting
Symptom
AIS information is not
displayed.
Cause
Action
The communication is not set
correctly.
Set the communication correctly.
The power supply for the AIS unit is Turn on the power supply for the AIS
not turned on.
unit.
The AIS unit does not perform
receiving.
Check the state of the AIS unit.
The connection with the AIS unit is Check the connection with the AIS
abnormal.
unit.
If an AIS unit is connected to the
SLC, check that the LED of the
corresponding port is lit during data
reception.
The power supply for the SLC
(CMH-2370) is not turned on.
(Case where the AIS unit is
connected to the SLC)
Turn on the power supply for the
SLC.
The SLC (CMH-2370) is faulty.
(Case where the AIS unit is
connected to the SLC)
Make a request to the distributor for
repair.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
6-215
6. Appendix > 6.10 Troubleshooting
Symptom
The azimuth of the Gyro
compass is not
displayed.
Alternatively, the
azimuth rotation
direction is not
displayed correctly.
Cause
Action
The communication is not set
correctly.
Set the communication correctly.
The power supply for the gyro
compass is not turned on.
Turn on the power supply for the gyro
compass.
The connection with the gyro
compass is abnormal.
Check the connection with the gyro
compass.
If the gyro compass is connected to
the SLC or GIF, check that the
corresponding LED is lit during signal
reception.
The power supply for the SLC
Turn on the power supply for the
(CMH-2370) is not turned on.
SLC.
(Case where the gyro compass is
connected to the SLC)
The SLC (CMH-2370) is faulty.
Make a request to the distributor for
(Case where the gyro compass is repair.
connected to the SLC)
Set the GIF correctly according to the
The GIF (CMJ-554) is not set
gyro compass.
correctly
(Case where the gyro compass is
connected to the GIF)
The fuse of the GIF (CMJ-554) has Replace the fuse of the GIF.
blown.
(Case where the gyro compass is
connected to the GIF)
Make a request to the distributor for
The GIF (CMJ-554)is faulty.
(Case where the gyro compass is repair.
connected to the GIF)
The internal wiring is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
6-216
6. Appendix > 6.10 Troubleshooting
Symptom
Cause
Action
Vessel speed is not
The communication is not set
Set the communication correctly.
displayed or the values correctly.
are not displayed
The power supply for the speed log Turn on the power supply for the
correctly.
is not turned on.
speed log.
The connection with the speed log Check the connection with the speed
is abnormal.
log.
If the speed log is connected to the
SLC or GIF, check that the
corresponding LED is lit during signal
reception.
The power supply for the SLC
(CMH-2370) is not turned on.
(Case where the speed log is
connected to the SLC).
Turn on the power supply for the
SLC.
The SLC (CMH-2370) is faulty.
(Case where the speed log is
connected to the SLC).
Make a request to the distributor for
repair.
The GIF (CMJ-554) is not set
correctly.
(Case where the speed log is
connected to the GIF).
Set the GIF correctly according to the
speed log.
The GIF (CMJ-554) is faulty.
(Case where the speed log is
connected to the GIF).
Make a request to the distributor for
repair.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
6-217
6. Appendix > 6.10 Troubleshooting
Symptom
Rudder angles are not
displayed.
Alternatively, the values
are not displayed
correctly.
Cause
Action
The communication is not set
correctly.
Set the communication correctly.
The power supply for the rudder
angle indicator is not turned on.
Turn on the power supply for the
rudder angle indicator.
The connection with the rudder
angle indicator is abnormal.
Check the connection with the rudder
angle indicator.
If the rudder angle indicator is
connected to the SLC, check that the
LED of the corresponding port is lit
during data reception.
The power supply for the SLC
Turn on the power supply for the
(CMH-2370) is not turned on.
SLC.
(Case where the rudder angle
indicator is connected to the SLC or
the rudder angle indicator is
connected to the AOC)
The SLC (CMH-2370) is faulty.
Make a request to the distributor for
(Case where the rudder angle
repair.
indicator is connected to the SLC or
the rudder angle indicator is
connected to the AOC)
The AOC (CMJ-560) is not set
Set the AOC correctly according to
correctly.
the rudder angle indicator.
(Case where the rudder angle
indicator is connected to the AOC)
The AOC (CMJ-560) is faulty.
Make a request to the distributor for
(Case where the rudder angle
repair.
indicator is connected to the AOC)
The internal wiring is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
6-218
6. Appendix > 6.10 Troubleshooting
Symptom
Cause
Action
The digital anemometer The communication is not set
values (wind direction correctly.
and speed) are not
The power supply for the
displayed.
anemometer is not turned on.
The connection with the
anemometer is abnormal
Set the communication correctly.
Turn on the power supply for the
anemometer.
Check the connection with the
anemometer.
Check that the LED of the
corresponding port in the SLC is lit
during data reception.
The power supply for the SLC
(CMH-2370) is not turned on.
Turn on the power supply for the
SLC.
The SLC (CMH-2370) is faulty.
Make a request to the distributor for
repair.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
Water depth values are The communication is not set
not displayed.
correctly.
Set the communication correctly.
The power supply for the echo
sounder is not turned on.
Turn on the power supply for the
echo sounder.
The connection with the echo
sounder is abnormal.
Check the connection with the echo
sounder.
Check that the LED of the
corresponding port in the SLC is lit
during data reception.
The power supply for the SLC
(CMH-2370) is not turned on.
Turn on the power supply for the
SLC.
The SLC (CMH-2370) is faulty.
Make a request to the distributor for
repair.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
6-219
6. Appendix > 6.10 Troubleshooting
Symptom
Sensor signals are not
displayed.
Cause
Action
The communication is not set
correctly.
Set the communication correctly.
The power supply for the sensor
equipment is not turned on.
Turn on the power supply for the
sensor equipment.
The connection with the sensor
equipment is abnormal.
Check the connection with the sensor
equipment.
Check that the LED of the
corresponding port in the SLC is lit
during data reception.
The power supply for the SLC
(CMH-2370) is not turned on.
Turn on the power supply for the
SLC.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The display unit such as the SLC
Make a request to the distributor for
(CMH-2370), AOC (CMJ-560), and repair.
CCU (NDC-1590) is faulty.
Auto sailing is disabled. The communication is not set
correctly.
Set the communication correctly.
The Auto sailing function is not
operated correctly.
Operate Auto sailing correctly.
The power supply for the Auto
sailing unit is not turned on.
Turn on the power supply for the Auto
sailing unit.
The connection with the Auto
sailing unit is faulty.
Check the connection with the Auto
sailing unit.
Check that the LED of the
corresponding port in the SLC is lit
during data reception.
The power supply for the SLC
(CMH-2370) is not turned on.
Turn on the power supply for the
SLC.
The SLC (CMH-2370) is faulty.
Make a request to the distributor for
repair.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
6-220
6. Appendix > 6.10 Troubleshooting
Symptom
Cause
Action
Contact signals are not The power supply for the SLC
Turn on the power supply for the
output.
(CMH-2370) is not turned on.
SLC.
(Case where contact signal output
is acquired from the SLC)
The SLC (CMH-2370) is faulty.
Make a request to the distributor for
(Case where contact signal output repair.
is acquired from the SLC)
The internal wiring is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
The scanner unit is not The connection with the scanner
recognized
unit is abnormal.
Check the connection with the
scanner unit.
Power is not supplied from the PSU Check the power supply wiring
to the scanner unit.
between the PSU and the RIF.
Check the power supply connection
inside of the scanner unit.
[Note]
For checking wiring inside of the
scanner unit, always request the
work to the specialized service
person. Before starting the work, turn
off the power supply of the display
unit. Otherwise, an unexpected
accident may occur.
Only AC power is supplied to the
PSU.
(NKE-2254 or NKE-2103 is
connected as the scanner unit)
To connect the NKE-2254 or
NKE-2103 scanner unit, the DC
power supply must be connected to
the PSU.
The RIF (CQD-2273) is not set
correctly.
Set the RIF correctly.
The RIF (CQD-2273) is faulty.
Make a request to the distributor for
repair.
The scanner unit is faulty.
Make a request to the distributor for
repair.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
6-221
6. Appendix > 6.10 Troubleshooting
Symptom
Cause
Action
The power is not
The connection with the scanner
supplied to the scanner unit is abnormal.
unit.
The connection with the scanner
unit is abnormal and overcurrent
protection is functioning in the PSU.
The preheat count
down of the scanner
unit is not displayed.
Check the connection with the
scanner unit.
Check the connection with the
scanner unit and remove the cause
of short-circuit.
DC power is not supplied to the
PSU.
(NKE-2254 or NKE-2103 is
connected as the scanner unit)
To connect the NKE-2254 or
NKE-2103 scanner unit, DC power
supply must be connected to the
PSU.
The DC24V output fuse is blown
out.
(NKE-2254 or NKE-2103 is
connected as the scanner unit.)
After removing the cause of fuse
blow-out, replace the fuse.
The fuse is the 15A blade fuse at the
front of the PSU (NBD-913).
The RIF (CQD-2273) is faulty.
Make a request to the distributor for
repair.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The PSU (NBD-913) is abnormal.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
The connection with the scanner
unit is abnormal.
Check the connection with the
scanner unit.
Set the safety switch of the scanner
unit to ON.
The safety switch of the scanner
unit is set to OFF.
[Note]
For operating the safety switch of the
scanner unit, always request the
work to the specialized service
person. Before starting the work, turn
off the power supply of the display
unit. Otherwise, an unexpected
accident may occur.
A solid-state scanner unit is
connected.
Preheat count-down is not displayed
for a solid-state scanner unit.
The scanner unit is faulty.
Make a request to the distributor for
repair.
The RIF (CQD-2273) is not set
correctly.
Set the RIF correctly.
The RIF (CQD-2273) is faulty.
Make a request to the distributor for
repair.
6-222
6. Appendix > 6.10 Troubleshooting
Symptom
The scanner unit does
not rotate even if the
[Transmit] button is
pressed.
Cause
Action
The internal wiring is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
The connection with the scanner
unit is abnormal.
Check the connection with the
scanner unit.
The safety switch of the scanner
unit is set to OFF.
Set the safety switch of the scanner
unit to ON.
[Note]
For operating the safety switch of the
scanner unit, always request the
work to the specialized service
person. Before starting the work, turn
off the power supply of the display
unit. Otherwise, an unexpected
accident may occur.
Power is not supplied from the PSU Check the power supply wiring
to the scanner unit.
between the PSU and the RIF.
Check the power supply connection
inside of the scanner unit.
[Note]
For checking the wiring inside of the
scanner unit, always request the
work to the specialized service
person. Before starting the work, turn
off the power supply of the display
unit. Otherwise, an unexpected
accident may occur.
The motor driver circuit inside of the
scanner unit is not set correctly.
(NKE-1632, NKE-2632, or
NKE-2632-H is connected as the
scanner unit.)
Set the motor driver circuit correctly.
[Note]
For setting the motor driver circuit,
always request the work to the
specialized service person. Before
starting the work, turn off the power
supply of the display unit.
Otherwise, an unexpected accident
may occur.
The rotating part of the scanner unit De-freeze the frozen section by using
is frozen.
the neck heater option.
6-223
6. Appendix > 6.10 Troubleshooting
Symptom
Cause
Action
Strong wind of relative wind velocity When strong wind of relative wind
exceeding 100 kt (about 51.5 m/s) velocity exceeding 100 kt is blowing,
is blowing.
the scanner unit does not rotate due
to the protection function.
No radar image is
displayed.
The scanner unit is faulty.
Make a request to the distributor for
repair.
The RIF (CQD-2273) is faulty.
Make a request to the distributor for
repair.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The PSU (NBD-913) is abnormal.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
The connection with the scanner
unit is abnormal.
Check the connection with the
scanner unit.
The GAIN value is set to the
minimum.
Set a proper value for GAIN.
The SEA/RAIN value is set to the
maximum.
Set a proper value for SEA/RAIN.
The magnetron is deteriorated
Replace the magnetron.
significantly.
(Case where an scanner unit that [Note]
For magnetron replacement, always
uses a magnetron is connected)
request the work to the specialized
service person. Before starting the
work, turn off the power supply of the
display unit. Otherwise, an
unexpected accident may occur.
The scanner unit is faulty.
Make a request to the distributor for
repair.
The RIF (CQD-2273) is faulty.
Make a request to the distributor for
repair.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The PSU (NBD-913) is abnormal.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
6-224
6. Appendix > 6.10 Troubleshooting
Symptom
Radar images cannot
be tuned
The azimuth of the
radar image is not
displayed correctly.
The range of the radar
image is not displayed
correctly.
Interswitch Unit does
not function.
Cause
Action
The magnetron is deteriorated
significantly.
(Case where a scanner unit that
uses a magnetron is connected)
Replace the magnetron.
A solid-state scanner unit is
connected.
Tuning bar is not displayed for a
solid-state scanner unit.
The azimuth is not set correctly.
Set the azimuth correctly.
CCRP is not set correctly.
Set CCRP correctly.
The GPS antenna position is not
set correctly.
Set the GPS antenna position
correctly.
The range is not set correctly.
Set the range correctly.
CCRP is not set correctly.
Set CCRP correctly.
The GPS antenna position is not
set correctly.
Set the GPS antenna position
correctly.
[Note]
For magnetron replacement, always
request the work to the specialized
service person. Before starting the
work, turn off the power supply of the
display unit. Otherwise, an
unexpected accident may occur.
Power for the Interswitch Unit is not Turn on the power for the Interswitch
turned on.
Unit.
The connection with the Interswitch Check the connection with the
Unit is abnormal.
Interswitch Unit.
The Interswitch Unit is faulty.
Make a request to the distributor for
repair.
The RIF (CQD-2273) is not set
correctly.
Set the RIF correctly.
The RIF (CQD-2273) is faulty.
Make a request to the distributor for
repair.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
If the power supply is
The CCU (NDC-1590) is faulty.
turned off, the trail data
is cleared without being
stored.
Make a request to the distributor for
repair.
6-225
6. Appendix > 6.10 Troubleshooting
Symptom
Radar images cannot
be overlaid.
Cause
Action
There is no optional license for
radar overlay.
Implement an optional license for
radar overlay.
The connection with the scanner
unit is abnormal.
Check the connection with the
scanner unit.
The connection with the radar
display unit is abnormal.
Check the connection with the radar
display unit.
The RIF (CQD-2273) is faulty.
Make a request to the distributor for
repair.
The internal wiring is faulty.
Make a request to the distributor for
repair.
The PSU (NBD-913) is faulty.
Make a request to the distributor for
repair.
The CCU (NDC-1590) is faulty.
Make a request to the distributor for
repair.
UPS does not function. The connection with UPS is faulty.
Check the connection with UPS.
UPS is not set correctly.
Set UPS correctly.
The UPS battery is extremely
depleted.
Replace the battery.
[Note]
At the battery replacement, make a
request for the work to the
specialized service staff. During the
replacement, turn off the
corresponding power supply breaker
in the ship. Otherwise, an
unexpected accident may occur.
The internal wiring is faulty.
Make a request to the distributor for
repair.
UPS is faulty.
Make a request to the distributor for
repair.
6-226
For further information,contact:
Not use the asbestos
URL http://www.jrc.co.jp
Marine Service Department
Telephone : +81-3-3492-1305
+81-3-3779-1420
Facsimile :
tmsc@jrc.co.jp
e-mail :
SEATTLE Branch
Telephone : +1-206-654-5644
Facsimile :
+1-206-654-7030
e-mail :
marineservice@jrcamerica.com
URL http://www.alphatronmarine.com
Rotterdam (Head office)
Alphatron Marine B.V.
Telephone : +31 (0)10- 453 4000
Facsimile :
+31 (0)10- 452 9214
e-mail :
service@alphatronmarine.com
Singapore Branch
Alphatron Marine Systems Pte Ltd
Telephone : +65 6863 0335
Facsimile :
+65 6863 3305
e-mail :
service@alphatronmarinesystems.com
CODE No.7ZPNA4466A
01ETM
JUL. 2015 Edition 3
ISO 9001, ISO 14001 Certified
JRC
Printed in Japan
JMR-9230-S/S3
JMR-9225-7X3/9X3/6X/9X/6XH
JMR-9210-6X/6XH
JMR-9272-S
JMR-9282-S/SH
JMR-7230-S/S3
JMR-7225-7X3/9X3/6X/9X/6XH
JMR-7210-6X/6XH
JMR-7272-S
JMR-7282-S/SH
JAN-9201
JAN-7201
JAN-9202
JAN-7202
MARINE RADAR EQUIPMENT
/ECDIS/CONNING
INSTALLATION MANUAL

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