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Chapter 1

 

 

KGC-1

 

General  

Operation 

Manual

 

1.1.3  For proper use of GPS Compass 

In the following circumstances the GPS Compass will take time to establish a correct bearing. 

„

 

The unit is first operated. 

„

 

The unit is left unused for a long period of time. This causes the stored orbital data to become old 

and not useable. 

„

 

The unit is carried to a distant area with power off and turned on again there. 

„

 

The satellite positional dispersion is not perfect. This may causes the bearing computation to be 

not established even though the positioning fix is available. 

A GPS receiver is arranged to store the orbital data of the satellites viewable from its site. Due to this 

arrangement, a fast position fix is possible. When the GPS unit is first turned on, no orbital data has 

been stored in memory, causing the GPS unit to take about 15 minutes to acquire local orbital data 

from the satellites. From next operation the orbital data used immediately before the unit is turned off 

will be stored into memory and used for subsequent position fix. This causes the position fix time to be 

reduced to one minute or the less. 

 

1.2 Equipment overview 

From the radio wave broadcast from the GPS satellites, the KGC-1 computes own ship’s bearing in 

high accuracy by measuring the phase difference between two GPS antennas. 

Four output ports are available on the KGC-1, two for the compass bearing output, the other two for 

the GPS position/speed data. 

 

1.3 Applicable technical standards 

The KGC-1 is fully compliant with the requirements of IEC 60945 3

rd

 Edition, general requirements for 

maritime navigational equipment. 

 

1.4 Equipment configuration 

The following table lists the name of the unit, type name and the system configuration diagram is 

shown in Fig. 1.2. 

Unit name

 

Type name

 

Processing unit 

KGC-1 

GPS Antenna 

GA-11 with 15 m cable   

Standard antenna cable length is 15 m. Extra cable lengths of 30 m and 60 m are available on option 

basis. 

 

1.5 Software type name 

Two types of software are used in KGC-1 as follows: 

1-2 

         

 

 

93121652-01 

 

Summary of Contents for KGC-1

Page 1: ......

Page 2: ......

Page 3: ...et are modified and the rest of the sheets are not changed The document number is shown in the footer area right or left bottom of each sheet c 2004 2005 2006 2007 2008 Koden Electronics Co Ltd All ri...

Page 4: ...each symbol before carrying out inspection and maintenance of this equipment Warning mark Warning To handle the equipment ignoring this sign may lead to injury to the human body or damage to the equi...

Page 5: ...on for the purpose of adjustment test as well as orbital modification Caution MAINTENACE PRECAUTIONS z Disconnect Main Power It is still possible to receive an electric shock caused by unintentional s...

Page 6: ...etailed information for your specific requirement Chapter 1 General About GPS Compass Equipment overview Applicable technical standards Equipment configuration Software type name Chapter 2 Equipment C...

Page 7: ...ions Connecting the units Check up after installation Chapter 5 Operation Panel layout and operating switches Output ports Selecting the output data Chapter 6 Maintenance and troubleshooting Periodica...

Page 8: ...GPS compass 1 1 1 1 1 Principle of GPS positioning system 1 1 1 1 2 How the GPS Compass works 1 1 1 1 3 For proper use of GPS Compass 1 1 1 2 Equipment overview 1 2 1 3 Applicable technical standards...

Page 9: ...ioning system own position is obtained by analyzing the CA code sent from the satellites to compute the distance from the satellites to the user In contrast the GPS Compass utilizes the radio wave its...

Page 10: ...e orbital data used immediately before the unit is turned off will be stored into memory and used for subsequent position fix This causes the position fix time to be reduced to one minute or the less...

Page 11: ...KGC 1 Chapter 1 Operation Manual General Software type name Application KM D92 Program ROM System control KM D93 Program ROM System control 93121652 01 1 3...

Page 12: ...ble VV 2D8 3M Power Rectifier PS 003A DC Power Cable CW 255 2M Antenna cable CW 392 15M 2 pcs Connecting Cable CW 376 5M Fuse 3 A Flying lead on one end NMEA 0183 Radar NMEA 0183 Radar NMEA 0183 Navig...

Page 13: ...pment Composition Chapter 2 Equipment Composition Page No 2 1 Standard equipment list 2 1 2 2 Spare Parts list 2 1 2 3 Installation Material list 2 1 2 4 Available antenna cable types 2 2 2 5 Optional...

Page 14: ...ead other end 5m 1 6 Bird repellent fixture D73MB23040 0 05kg 2 7 Spare parts Refer to Spare Parts list 1 set 8 Installation material Refer to Installation Material list 1 set 9 Operation Manual Engli...

Page 15: ...me Remarks Weight Length 1 Connectingcable CW 373 5M 6P water proof connector LTW both ends 5m 2 Connectingcable CW 374 5M 6P connector one end water proof connector LTW the other end 5m 3 Connectingc...

Page 16: ...e No 3 1 Functional specification 3 1 3 2 Serial data 3 1 3 3 Power supply requirements 3 2 3 4 Compass safety distance 3 2 3 5 Environmental conditions 3 2 3 6 External dimensions and weight 3 3 3 6...

Page 17: ...ion GPS 15m 2drms SA OFF PDOP 3 Velocity 1m sec rms SA OF PDOP 3 Datum 86 system WGS 84 Tokyo etc Output data port Heading data output 2 50ms 1s Navigational data output 2 1s Output data Format Headin...

Page 18: ...ier PS 003A is used Input voltage range 100 115 VAC or 200 230 VAC Input voltage tolerance 10 Input voltage frequency tolerance 47 63 Hz 3 4 Compass safety distance Unit name Type Standard Steering Pr...

Page 19: ...al Specifications 3 6 External dimensions and weight 3 6 1 Processor unit KGC 1 External dimensions 220 W x 245 D x 85 H unit in mm Weight 1 2kg External dimensions Unit mm inch Fig 3 1 External dimen...

Page 20: ...C 1 Specifications Operation Manual 3 4 93121652 00 3 6 2 GPS Antenna GA 11 External dimensions 593 W x 150 D x 160 H unit in mm Weight 1 4kg External dimensions Fig 3 2 External dimensions of GA 11 U...

Page 21: ...3 4 5 1 1 Installing the Bird repellent fixture 4 5 4 5 1 2 Heading adjust 4 6 4 5 1 3 Waterproofing on the connector jointing section 4 6 4 5 1 4 Connecting the 60m antenna cable kit CW 394 KIT to G...

Page 22: ...11 must be installed where good radio wave reception is achieved No obstacles should be located above the antenna otherwise the radio wave reception may be interrupted This causes the available GPS s...

Page 23: ...4 m or more 1 m or more Avoid radar beam illumination 30o to 40o 5 m or more See NOTE 1 5 m or more 4 m or more Do not scale Radar beam MF HF Inverted L Antenna Loop Antenna Inmarsat Antenna 3 m or mo...

Page 24: ...ing holes on the platform using the template attached 2 Connect the coax cable and apply waterproofing Refer to 4 5 1 3 for detail Secure the waterproofed coax cable to the platform post with a weathe...

Page 25: ...g instructions The bow side antenna must be connected to the Processor unit as follows z Bow side antenna cable to ANT 1 plug z Stern side antenna cable to ANT 2 plug Fig 4 5 GPS Antenna GA 11 Fig 4 4...

Page 26: ...en each device using a weather resistive tie through the GA 11 fixing hole We recommend that the devices are co fastened with the waterproofed antenna cable If these are attached after the antenna cab...

Page 27: ...5 1 3 Waterproofing on the connector jointing section 1 Wind the self bonding tape around the joint section Pull the end of the tape and stretch it to twice its length Wrap it around joint section a...

Page 28: ...a the cable kit as shown in the following figure 1 Connection at GPS Antenna side Conversion connector NP BNCP Antenna cable CW 394 60M To Processor unit GPS Antenna Waterproof the jointing section us...

Page 29: ...nit Please arrange the suitable screws locally Fig 4 9 Service space required for the Processor unit Unit mm inch 4 6 Cable layout and connections 1 Secure the Antenna cable connection 2 Secure the Jo...

Page 30: ...side antenna cable is connected to ANT 1 and the stern side antenna cable to ANT 2 respectively GPS Antenna GA 11 Fig 4 10 Interconnection diagram of KGC 1 Processor unit KGC 1 Nav data output NMEA018...

Page 31: ...erial input RX Serial input RX NC NMEA IEC61162 IN OUT DATA1 3 Locations of connectors on the Processor unit DC 10 8 31 2VDC DC DC NC POWER Ground GND Serial output TX Serial output TX Serial input RX...

Page 32: ...ecting diagram in Chapter 1 Appendix Connecting the Data cable CW 376 5M to PC Rx Signal input Hot Rx Signal input Cold White Red D SUB 9 pin Solder side Link between pin 7 and pin 8 White Blue Black...

Page 33: ...er 5 Operation PageNo 5 1 Panel layout and operating switches 5 1 5 1 1 POWER switch 5 1 5 1 2 MODE switch 5 1 5 1 3 POWER lamp 5 1 5 1 4 ALARM lamp 5 1 5 1 5 DATA lamp 5 1 5 2 Output port 5 2 5 3 Sel...

Page 34: ...nit The lamp goes off when the POWER switch is pressed again to turn the unit off 5 1 4 ALARM lamp The ALARM lamp blinks when an abnormal condition is detected in the unit as a result of self diagnosi...

Page 35: ...ta Interval Navigational data Interval 0 HDT 50ms N A 1 HDT 100ms N A 2 HDT ROT 100ms N A 3 HDT 200ms N A 4 HDT 100ms GGA VTG 1s 5 HDT 200ms GGA VTG 1s 6 HDT 100ms GGA VTG 1s 7 HDT 1s GGA VTG 1s GGA G...

Page 36: ...ance and troubleshooting Page No 6 1 Periodic inspection and cleaning 6 1 6 1 1 Monthly check 6 1 6 1 2 Maintenance 6 1 6 2 Trouble shooting 6 1 6 2 1 Information required for service 6 1 6 2 2 Troubl...

Page 37: ...port of call ship s agent name fax number email address etc 5 Faulty conditions precisely as possible and the result of on board check 6 2 2 Trouble shooting The following table provides information a...

Page 38: ...lamp keeps flashing and no bearing data is output The bearing calculation time may be prolonged in case effective GPS satellites are not properly dispersed 1 Are the GPS antenna cables firmly connecte...

Page 39: ...enna connections are reversed i e Bow side antenna to ANT2 and Stern side antenna to ANT1 faulty bearing information is output Correct the antenna connection 2 Check the GPS antenna installation If th...

Page 40: ...A1 which is mounted on the Main Printed Board D73 700 in the Processor unit The location of the battery is shown in Fig 7 1 Back up battery Fig 7 1 The location of the back up battery Removing the bat...

Page 41: ...References PageNo 7 1 Detail of the serial output data 7 1 7 1 1 Start bit configuration of output data 7 1 7 1 2 Serial data specification 7 1 7 1 3 Detail of output sentences 7 1 7 2 Data input outp...

Page 42: ...Serial data specification Transmission rate Output data level Output current Output sentences included Refresh rate 4800 baud RS 422 20mA max Refer to page 5 2 Refer to page 5 2 7 1 3 Detail of output...

Page 43: ...itude W West longitude Status of GPS fix measurement 0 Fix unable 1 GPS fix 2 DGPS fix Number of satellite in use Checksum HDOP value Antenna height Negative Meter Negative Meter Gioid height DGPS dat...

Page 44: ...M S Sentence name Start of sentence Checksum E East longitude West longitude Magnetic deviation Date D M Y Sentence name Start of sentence Talker device Meassurement Time H M S A Data valid V Alarm va...

Page 45: ...EN proprietary sentence Start of sentence Satellite No in use 1 4 channel S N ratio of the satellite in use 1 4 channel Ground speed Antenna height KODEN modification code P PDOP H HDOP PDOP value Met...

Page 46: ...Type TLP181 or TLP115A Toshiba Serial data input circuit Serial Data output talker side The IEC 61162 1 standard signal can be transmitted Output Device Driver IC HD26C31FP Hitachi 5V TX HD26C31FP TX...

Page 47: ...or interruption to calculate bearing 60 sec 0 sec 5 Datum selection Tokyo WGS84 6 Limits of elevation angle 5 degree 20 degree 7 Initialization Cold start Initialized Not initialized 8 For technical u...

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