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APC-5 

RMA – Recommended minimum specific Loran-C data 

$--RMA,A,llll.lll,a,yyyyy.yy,a,x.x,x.x,x.x,x.x,x.x,a,a*hh<CR><LF>
              |    |     |         |      |   |     |     |     |    |    |  |   |
              |    |     |         |      |   |     |     |     |    |    |  |   +------- 10
              |    |     |         |      |   |     |     |     |    |    |  +--------- 9
              |    |     |         |      |   |     |     |     |   +---+----------- 8
              |    |     |         |      |   |     |     |    +------------------ 7
              |    |     |         |      |   |     |    +---------------------- 6
              |    |     |         |      |   |    +-------------------------- 5
              |    |     |         |      |   +------------------------------ 4
              |    |     |        +----+--------------------------------- 3
              |    +---+-------------------------------------------- 2
             +------------------------------------------------------- 1

    1. Status: A=data valid, V=blink, cycle or SNR warning
    2. Latitude, degrees N/S
    3. Longitude, degrees E/W
    4. Time difference A, microseconds
    5. Time difference B, microseconds
    6. Speed over ground, knots
    7. Course over ground, degrees true
    8. Magnetic 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 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 be null fields.

 

Summary of Contents for LC-90 Mark-II

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Page 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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Page 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 ...

Page 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 ...

Page 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...

Page 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...

Page 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 ...

Page 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...

Page 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 ...

Page 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...

Page 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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