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APC-1 

DIGITAL INTERFACE (IEC61162-1) 

Output sentences of channel 1 (OUTPUT) 

AAM, BOD, BWC, BWW, GLL, RMA, RMB, VTG, WCV, WNC, WPL, XTE, ZTG   

Transmission interval 

1 s for any sentence 

Data transmission 

Data is transmitted in serial asynchronous form in accordance with the standard referenced in 2.1 of 
IEC 61162-1. The first bit is a start bit and is followed by data bits, least-significant-bit as illustrated 
below. 

The following parameters are used: 
Baud rate: 4800 
Data bits: 8 (D7 = 0), parity none 
Stop bits: 1 

D0    D1     D2    D3     D4     D5     D6    D7

Start
bit

Stop
bit

Data bits

 

Schematic diagrams 

OUTPUT port (input) 

1

3

 6

 4

J3

2

7

6

5

6

OUTPUT

FL6

04P4061

SRCNA16-10P

FL5

R29
47

  CR6
SS355

TLP121
  U23
   

+5V

R37
2.7K

RD-H

RD-C

1

 

Содержание LC-90 Mark-II

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Страница 2: ...o m i y a J a p a n Telephone 0798 65 2111 Telefax 0798 65 4200 Your Local Agent Dealer A l l r i g h t s r e s e r v e d PUB No O M E 4 3 2 70 L C 90 MARK 2 Y O S H FIRST E D I T I O N D E C 198 8 L1 A U G 21 2 0 0 2 Printed in Japan ...

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Страница 92: ...ance with the standard referenced in 2 1 of IEC 61162 1 The first bit is a start bit and is followed by data bits least significant bit as illustrated below The following parameters are used Baud rate 4800 Data bits 8 D7 0 parity none Stop bits 1 D0 D1 D2 D3 D4 D5 D6 D7 Start bit Stop bit Data bits Schematic diagrams OUTPUT port input 1 3 6 4 J3 2 7 6 5 6 OUTPUT FL6 04P4061 SRCNA16 10P FL5 R29 47 ...

Страница 93: ...arm AAM A A x x N c c hh CR LF 5 4 3 2 1 1 Status A arrival circle entered 2 Status A perpendicular passed at waypoint 3 Arrival sircle radius nautical miles 4 Waypoint ID 5 Checksum BOD Bearing origin to destination BOD x x T x x M c c c c hh CR LF 5 4 3 2 1 1 Bearing degrees true 2 Bearing degrees magnetic 3 Destination waypoint ID 4 Origin waypoint ID 5 Checksum ...

Страница 94: ...t longitude E W Bearing degrees magnetic Waypoint latitude N S UTC of observation NOTE 1 Positioning system Mode indicator A Autonomous mode D Differential mode E Estimated dead reckoning mode M Manual input mode S Simulator mode N Data not valid The Mode indicator field shall not be a null field Not used BWW Bearing waypoint to waypoint BWW x x T x x M c c c c hh CR LF 5 4 3 2 1 1 Bearing degrees...

Страница 95: ...ator see note 6 Checksum NOTE Positioning system Mode indicator A Autonomous D Differential E estimated dead reckoning M Manual input S Simulator N Data not valid The Mode indicator field supplements the Status field The Status field shall be set to V invalid for all values of Operating Mode except for A Autonomous and D Differential The positioning system Mode indicator and Status field shall not...

Страница 96: ...etic variation see note 1 degree E W 9 Mode indicator see note 2 10 Checksum NOTE 1 Easterly variation E subtracts from true course Westerly variation W adds to true course NOTE 2 Positioning system Mode indicator A Autonomous D Differential E Estimated dead reckoning M Manual input S Simulator N Data not valid The Mode indicator field supplements the Status field The Status field shall be set to ...

Страница 97: ... 10 Destination closing velocity knots 11 Arrival status A arrival circle entered or perpendicular passed 12 Mode indicator see note 3 13 Checksum NOTES 1 If range to destination exceeds 999 9 nautical miles display 999 9 2 If cross track error exceeds 9 99 nautical miles display 9 99 3 Positioning system Mode indicator A Autonomous D Differential E estimated dead reckoning M Manual input S Simula...

Страница 98: ... Differential E estimated dead reckoning M Manual input S Simulator N Data not valid The positioning system Mode indicator field shall not be a null field WCV Waypoint closure velocity WCV x x N c c a hh CR LF 4 3 2 1 1 Velocity component knots 2 Waypoint identifier 3 Mode indicator see note 4 Checksum NOTE Positioning system Mode indicator A Autonomous D Differential E estimated dead reckoning M ...

Страница 99: ...point latitude N S 2 Waypoint longitude E W 3 Waypoint identifier 4 Checksum XTE Cross track error measured XTE A A x x a N a hh CR LF 7 6 5 4 3 2 1 1 Status A data valid V LORAN C blink or SNR warning V general warning flag or other navigation systems when a reliable fix is not available 2 Status A data valid V LORAN C cycle lock warning flag 3 Mgnitude of cross track error 4 Direction to steer L...

Страница 100: ...APC 9 ZTG UTC and time to destination waypoint ZTG hhmmss ss hhmmss ss c c hh CR LF 4 3 2 1 1 UTC of observation 2 Time to go hh 00 to 99 3 Destination waypoint ID 4 Checksum ...

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