Navigat 3000 operational manual.pdf

8/18/2019 Navigat 3000 operational manual.pdf

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Northrop Grumman Sperry Marine B.V. (Representative Office)Woltmanstr. 19 • D-20097 • Hamburg, Germany

Tel.: +49-40-299 00-0 • Fax: +49-40-299 00-146 • E-mail: [email protected]

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GYRO

1

MAIN MENU

F1 DISPLAY DATA

F2 MANUAL SETTINGS

F3 SETUP MENU

246.8 °

NAVIGAT

3000

Fiber-Optic Gyrocompass

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Dual Use Regulations / Fiber Optic Gyrocompass NAVIGAT 3000The NAVIGAT 3000 sensor unit, the software and the corresponding technical data and docu-mentation (operation, installation and service manuals) are export controlled in accordance tothe European Dual Use Regulations 428/2009 (EC).The Export Control Classification Number (ECCN) for the NAVIGAT 3000 sensor unit is 7A003d.Any export of the NAVIGAT 3000 sensor unit hardware, the software and the correspondingtechnical data and documentation from a Member State of the European Community are subjectto export restrictions and requires an appropriate export license granted by the competentauthorities of the Member State from where the export shall be conducted from.

A legal buyer of the NAVIGAT 3000 sensor unit is obliged to keep to the export control in accord-ance to the European Dual Use Regulations 428/2009 (EC) and is not allowed to sell theNAVIGAT 3000 sensor unit, the software and the corresponding technical data and documenta-tion or distribute copies of the software and technical data and documentation to third partywithout prior export license.

© 2014 Northrop Grumman Sperry Marine B.V.This document and the information herein is the intellectual property ofNorthrop Grumman Sperry Marine B.V. [NGSM BV] and it’s associate companies and may notbe copied, reproduced or translated without the express permission of NGSM BV.Specifications were correct at time of press but may be varied in accordance with NGSM BV’spolicy of continuous product development.Any technical content should be verified with NGSM BV.

Sperry Marine, with major engineering and support offices in New Malden, England, andHamburg, Germany, is part of the Northrop Grumman Navigation & Maritime Systems DivisionN&MSD.

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D 31 Oct 2014 Updated and reworked release, according to newNAVIGAT 3000 software version 1050, IPSU software version 2.401

C2 16 Dec2013 Client specific release

C1 17 Jul 2013 Client specific release

C 11 Feb 2013 Stationary mode added

B2 16 Jan 2013 Certificates amended for Gyrocompass HSC and ROTI, dual use regu-lation info added, technical data amended

B1 05 Dec 2012 Spare parts reworked

B 14 Nov 2012 Updated release, THS protocol added; installation check proceduresadded, IPL of spare parts added, dual gyrocompass system configura-

tion added

A 13 Apr 2012 Initial release


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NKN póëíÉã fåÑçêã~íáçå KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK NJN

fåíÉåÇÉÇ rëÉ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKNJN

kçí fåíÉåÇÉÇ rëÉKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKNJN

NKO póëíÉã lîÉêîáÉïKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK NJO

i~ÄÉä ~åÇ íóéÉ éä~íÉë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKNJS

NKP póëíÉã aÉëáÖå ~åÇ j~áå cÉ~íìêÉëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK NJT

NKQ léÉê~íáåÖ mêáåÅáéäÉ çÑ íÜÉ pÉåëçê KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK NJV

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pí~åÇ~äçåÉ dóêçÅçãé~ëë póëíÉã KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK NJNO

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NKS qÉÅÜåáÅ~ä a~í~KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK NJNR

cáÄÉêJléíáÅ pÉåëçê råáí KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKNJNR

fåíÉêÑ~ÅÉ ~åÇ mçïÉê pìééäó råáíKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKNJNT

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fåJ ~åÇ lìíéìí fåíÉêÑ~ÅÉë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKNJNV

póëíÉã mçä~êáíó aÉÑáåáíáçåë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKNJON

NKT aÉÅä~ê~íáçå çÑ `çåÑçêãáíó KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK NJOP

`Ü~éíÉê OW léÉê~íáçå

OKN léÉê~íáåÖ ̀ çåÇáíáçåë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJN

^äáÖåãÉåí oÉèìáêÉãÉåíë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJN

OKO aáëéä~ó ~åÇ léÉê~íáåÖ hÉóë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKOJP

`çåíêçä ~åÇ aáëéä~ó råáí `ar KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJP

OKP bñíÉêå~ä `çåíêçä aÉîáÅÉë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJQ

OKQ pí~êíìéL^äáÖå mêçÅÉÇìêÉ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJR

léÉê~íáåÖ jçÇÉ fåÇáÅ~íáçåëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJT

^äáÖåãÉåí `çåÇáíáçåëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJU

`çãéäÉíáçå çÑ ^äáÖåãÉåí KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKOJNM

OKR p~áäáåÖ jçÇÉ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJNN

OKS pí~íáçå~êó jçÇÉ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJNQ

OKT pÉäÉÅíáåÖ íÜÉ ^ÅíáîÉ eÉ~ÇáåÖ pçìêÅÉKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJNS

OKU ^ÇàìëíáåÖ íÜÉ aáëéä~ó _êáÖÜíåÉëë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJNS


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OKV léíáçå~ä cìåÅíáçåëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKOJNT

jìíáåÖ ^ä~êãë oÉãçíÉäó KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJNT

oÉîÉêëáåÖ íÜÉ eÉ~ÇáåÖ aáëéä~ó ENUMø çÑÑëÉíF KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJNT

oÉëÉííáåÖL^ÅâåçïäÉÇÖáåÖ ~ `Éåíê~ä t~íÅÜ ^ä~êã KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJNT

pÉäÉÅíáåÖ íÜÉ o~íÉ çÑ qìêå a~ãéáåÖ qáãÉ `çåëí~åí KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJNT

OKNM léÉê~íáåÖ jÉåì KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKOJNU

k~îáÖ~íáåÖ íÜÉ jÉåì KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJNU

pÉäÉÅíáåÖ m~ê~ãÉíÉê pÉííáåÖëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJNU

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`~éíáçå Ñçê m~ê~ãÉíÉê pÉäÉÅíáåÖ ~åÇ bÇáíáåÖKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJNV

OKNN pÉäÉÅíáåÖ ~ aáëéä~ó a~í~ m~ÖÉKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJNV

aáëéä~ó a~í~ m~ÖÉë J dóêçÅçãé~ëë jçÇÉ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJOM

aáëéä~ó a~í~ m~ÖÉë J pí~íáçå~êó jçÇÉ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJON

OKNO j~åì~ä pÉííáåÖë jÉåì KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKOJOO

j~åì~ä pÉííáåÖë Ó lîÉêîáÉï KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJOP

j~åì~ä pÉííáåÖë Ó m~ê~ãÉíÉêë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJOS

OKNP rëÉê pÉíìé KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKOJPOrëÉê pÉíìé Ó lîÉêîáÉï KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJPO

rëÉê pÉíìé Ó m~ê~ãÉíÉêë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK OJPQ

`Ü~éíÉê PW bêêçêë ~åÇ ^ä~êãë

PKN ^ä~êã fåÇáÅ~íáçåKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKPJN

^ìÇáÄäÉ ^ä~êã fåÇáÅ~íáçåKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK PJN

sáëì~ä ^ä~êã fåÇáÅ~íáçå KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK PJN

PKO ^ÅâåçïäÉÇÖáåÖ ^ä~êãëLjìíáåÖ ^ä~êãëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKPJO

^ä~êã ^ÅâåçïäÉÇÖÉ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK PJO

PKP bêêçê ãÉëë~ÖÉë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKPJP

`Ü~éíÉê QW pÅÜÉÇìäÉÇ j~áåíÉå~åÅÉ

QKN j~áåíÉå~åÅÉ Äó pÜáéÄç~êÇ mÉêëçååÉä KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKQJN

`Ü~éíÉê RW fåëí~ää~íáçå

RKN jÉÅÜ~åáÅ~ä fåëí~ää~íáçåKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKRJN

k^sfd q̂ PMMM dóêçÅçãé~ëë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJO

k^sfd q̂ PMMM fåíÉêÑ~ÅÉ ~åÇ mçïÉê pìééäó råáí EfmprFKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJP

k^sfd q̂ PMMM `çåíêçä ~åÇ aáëéä~ó råáí E`arF KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJQ

RKO bäÉÅíêáÅ~ä fåëí~ää~íáçåKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJS

fmpr ^` mçïÉê pìééäó `çåÑáÖìê~íáçå KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJS

táêáåÖ ré íÜÉ póëíÉãKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJT

RKP fåáíá~ä póëíÉã ̀ çåÑáÖìê~íáçå KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKRJU

`çåÑáÖìê~íáçå çÑ póëíÉãKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJU

cáå~äáò~íáçå çÑ póëíÉã `çåÑáÖìê~íáçå KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJV

aì~ä L qêáéäÉ dóêçÅçãé~ëë póëíÉã `çåÑáÖìê~íáçå KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJNM

RKQ ^äáÖåãÉåíI oçää ~åÇ máíÅÜ bêêçê `çêêÉÅíáçåKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJNN

`çêêÉÅíáçå mêçÅÉÇìêÉ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJNP

RKR j~ÖåÉíáÅ `çãé~ëë `~äáÄê~íáçåKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKRJNR`~äáÄê~íáçå mêçÅÉÇìêÉ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJNR


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RKS fåëí~ää~íáçå ̀ ÜÉÅâ mêçÅÉÇìêÉëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKRJNU

jÉÅÜ~åáÅ~ä fåëí~ää~íáçå `ÜÉÅâ mêçÅÉÇìêÉKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJNU

bäÉÅíêáÅ~ä fåëí~ää~íáçå `ÜÉÅâ mêçÅÉÇìêÉ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJNU

póëíÉã `çåÑáÖìê~íáçå `ÜÉÅâ mêçÅÉÇìêÉKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKRJNV

båîáêçåãÉåí~ä `çåÇáíáçåë `ÜÉÅâ mêçÅÉÇìêÉKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJOM

j~ÖåÉíáÅ `çãé~ëë `~äáÄê~íáçå mêçÅÉÇìêÉKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK RJON

`Ü~éíÉê SW póëíÉã `çåÑáÖìê~íáçå

SKN `çåÑáÖìê~íáçå jÉåì EpÉêîáÅÉ pÉíìé NFKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKSJN

pÉíìé ^ÅÅÉëë `çÇÉKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK SJN

pÉêîáÅÉJpÉíìé Ó lîÉêîáÉïKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK SJO

pÉêîáÅÉ pÉíìé N Ó m~ê~ãÉíÉêëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK SJS

SKO pÉêîáÅÉ fåÑç jÉåì EpÉêîáÅÉ pÉíìé OF KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK SJOM

pÉêîáÅÉ pÉíìé O Ó ̂ ÅÅÉëë `çÇÉ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK SJOM

pÉêîáÅÉ pÉíìé O Ó lîÉêîáÉïKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK SJON

pÉêîáÅÉ pÉíìé O Ó m~ê~ãÉíÉêëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK SJOO

SKP c~Åíçêó pÉííáåÖë jÉåì EqÉÅÜåáÅ~ä m~ÖÉëF KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK SJOP

pÉíìé ^ÅÅÉëë `çÇÉKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK SJOP

qÉÅÜåáÅ~ä m~ÖÉë Ó lîÉêîáÉïKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK SJOQ

qÉÅÜåáÅ~ä m~ÖÉë Ó m~ê~ãÉíÉêë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK SJOQ

`Ü~éíÉê TW qêçìÄäÉëÜççíáåÖ

TKN dÉåÉê~ä qêçìÄäÉëÜççíáåÖ fåëíêìÅíáçåëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK TJN

TKO fmpr eçìëáåÖ j~áå `çãéçåÉåíë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK TJQ

TKP fmprW bñÅÜ~åÖÉ~ÄäÉ `çãéçåÉåíëI `çååÉÅíçêëI aá~ÖåçëíáÅ ibaë KKKKKKKK TJR

içÅ~íáçå çÑ m~êíë çå íÜÉ fåíÉêÑ~ÅÉ m`_ ~åÇ mêçÅÉëëçê m`_ KKKKKKKKKKKKKKKKKKKKKKK TJRbñÅÜ~åÖÉ~ÄäÉ `çãéçåÉåíëI m~êíë mêçÅÉëëçê m`_KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK TJS

`çååÉÅíçêë Eq_LgF fmpr ~åÇ fåíÉêÑ~ÅÉ m`_KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK TJT

aá~ÖåçëíáÅ ibaëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK TJV

TKQ àrW bñÅÜ~åÖÉ~ÄäÉ `çãéçåÉåíëI `çååÉÅíçêëI aá~ÖåçëíáÅ ibaë KKKKKK TJNS

içÅ~íáçå çÑ m~êíë çå íÜÉ àr m`_ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKTJNS

bñÅÜ~åÖÉ~ÄäÉ `çãéçåÉåíëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKTJNT

`çååÉÅíçêë Eg~ÅâëI gF KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKTJNT

aá~ÖåçëíáÅ ibaëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKTJNT

TKR pÉåëçê aá~ÖåçëíáÅë jÉåì KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK TJNU

pÉåëçê aá~ÖåçëíáÅë Ó ^ÅÅÉëë `çÇÉKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKTJNU

pÉåëçê aá~ÖåçëíáÅë jÉåì Ó lîÉêîáÉïKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKTJNV

pÉåëçê aá~ÖåçëíáÅë Ó m~ê~ãÉíÉêë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK TJOM

pÉåëçê póëíÉã c~ìäí jÉëë~ÖÉëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK TJOQ

`Ü~éíÉê UW `çêêÉÅíáîÉ j~áåíÉå~åÅÉ

UKN bñÅÜ~åÖáåÖ íÜÉ fmpr pçÑíï~êÉKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK UJO

UKO bñÅÜ~åÖáåÖ íÜÉ àr pçÑíï~êÉ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK UJR

bñÅÜ~åÖáåÖ íÜÉ cä~ëÜÄç~êÇ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK UJR

UKP oÉéä~ÅáåÖ pçÅâÉíÉÇ f`ë KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK UJU


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`Ü~éíÉê VW k^sfd q̂ PMMM pé~êÉ m~êíë

VKN fääìëíê~íÉÇ m~êíë iáëí EfmiF lîÉêîáÉï KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK VJN

VKO içÅ~íáçå çÑ pé~êÉ m~êíëKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKVJP

pé~êÉ m~êíë áå fmpr eçìëáåÖ KKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKKK VJP

^ÄÄêÉîá~íáçåë

^ééÉåÇáñ

^ pÉíìé ~åÇ `çåÑáÖìê~íáçå q~ÄäÉë

_ aê~ïáåÖë


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p~ÑÉíó fåÑçêã~íáçå

p~ÑÉíó kçíáÅÉ `çåîÉåíáçåë

The following safety notice conventions are followed throughout thismanual:

a^kdbo A a~åÖÉê notice contains an operating or main-tenance procedure, practice, condition, state-ment, etc., which, if not strictly observed, ïáääêÉëìäí áå áåàìêó çê ÇÉ~íÜ çÑ éÉêëçååÉäK

t^okfkd A t~êåáåÖ notice contains an operating ormaintenance procedure, practice, condition,statement, etc., which, if not strictly observed,

ÅçìäÇ êÉëìäí áå áåàìêó çê ÇÉ~íÜ çÑ éÉêëçååÉäK

`^rqflk A `~ìíáçå notice contains an operating or main-tenance procedure, practice, condition, state-ment, etc., which, if not strictly observed, ÅçìäÇêÉëìäí áå Ç~ã~ÖÉ íçI çê ÇÉëíêìÅíáçå çÑ ÉèìáéJ

ãÉåíK

kçíÉ A kçíÉ contains an essential operating or main-tenance procedure, condition or statement,which is considered important enough to be

highlighted.

Special safety symbols may be used in thismanual to indicate:

oáëâ çÑ ÉäÉÅíêáÅ~ä ëÜçÅâK

Used in conjunction with a a~åÖÉê or t~êåáåÖ notice.

Electrical components are sensitive to electro-static discharge.

Used in conjunction with a `~ìíáçå notice.


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dÉåÉê~ä p~ÑÉíó fåÑçêã~íáçå Ñçê íÜÉ léÉê~íçê

tôkfkd oáëâ çÑ ãáëìë~ÖÉ

_ÉÑçêÉ ìëáåÖ íÜÉ k^sfd^q PMMM ëóëíÉãI çéÉê~íçêë ãìëí ÄÉ ~ééêçéêáJ

~íÉäó íê~áåÉÇ ~åÇ Ñ~ãáäá~ê ïáíÜ ~ää çéÉê~íáåÖ éêçÅÉÇìêÉë ~åÇ ë~ÑÉíó

áåëíêìÅíáçåë Åçåí~áåÉÇ áå íÜáë ã~åì~äK qÜÉ ã~åì~ä áë íç ÄÉ ÅçãéäÉíÉäó

êÉ~Ç ÄÉÑçêÉ íÜÉ Ñáêëí ìë~ÖÉ çÑ íÜÉ k^sfd^q PMMM ëóëíÉãK

hÉÉé ~ää ëóëíÉã ã~åì~äë áå ~ ïÉääJâåçïåI êÉ~Çáäó ~î~áä~ÄäÉ äçÅ~íáçå

tôkfkd oáëâ çÑ ÇÉîá~íáçå

kÉîÉê êÉäó çå çåÉ ÜÉ~ÇáåÖ ëçìêÅÉ ~äçåÉ íç å~îáÖ~íÉ ~ îÉëëÉäK

^äï~óë ÅçåÑáêã íÜÉ éä~ìëáÄáäáíó çÑ íÜÉ k^sfd^q PMMM ÜÉ~ÇáåÖ ~åÇ íÜÉ

ëéÉÉÇ ~åÇ éçëáíáçå áåéìí Ç~í~ ~Ö~áåëí ~ää ~î~áä~ÄäÉ ~áÇë íç å~îáÖ~íáçåK

tôkfkd oáëâ çÑ ÇÉîá~íáçå íÜêçìÖÜ ëí~íáçå~êó ãçÇÉ

qÜÉ ëí~íáçå~êó ãçÇÉ çÑ íÜÉ k^sfd^q PMMM áë ëéÉÅáÑáÅ~ääó ÇÉëáÖåÉÇ Ñçê ~

îÉëëÉä çéÉê~íáåÖ ìåÇÉê Çóå~ãáÅ éçëáíáçåáåÖ EamF ÅçåÇáíáçåë áå ~ ÑáñÉÇéçëáíáçåK léÉê~íáåÖ íÜÉ k^sfd^q PMMM áå ëí~íáçå~êó ãçÇÉ ïÜáäÉ íÜÉ

îÉëëÉä áë å~îáÖ~íáåÖ ìåÇÉê ëÉ~ çéÉê~íáåÖ ÅçåÇáíáçåë ïáää Å~ìëÉ ÇÉîá~íáçåK

^äï~óë ã~âÉ ëìêÉ íÜ~í íÜÉ ë~áäáåÖ ãçÇÉ çÑ çéÉê~íáçå áë ~ëëáÖåÉÇ ïÜáäÉ

íÜÉ îÉëëÉä áë å~îáÖ~íáåÖ ~í ëÉ~K

kÉîÉê ~ëëáÖå íÜÉ ëí~íáçå~êó ãçÇÉ ïÜáäÉ íÜÉ îÉëëÉä áë å~îáÖ~íáåÖ ìåÇÉê

ëÉ~ çéÉê~íáåÖ ÅçåÇáíáçåëK

tôkfkd oáëâ çÑ ÇÉîá~íáçå íÜêçìÖÜ ìåÇÉíÉÅíÉÇ ÜÉ~ÇáåÖ ÇáÑÑÉêÉåÅÉë

qÜÉ ÇáÑÑÉêÉåÅÉ ~ä~êã ÜÉ~ÇáåÖ ëÉåëçêë ÑìåÅíáçå~äáíó ~ääçïë Åçåëí~åí

ãçåáíçêáåÖ çÑ íïç ÇáÑÑÉêÉåí ÜÉ~ÇáåÖ Ç~í~ ëçìêÅÉë ~åÇ É~êäó ÇÉíÉÅíáåÖ çÑ

ÜÉ~ÇáåÖ Ñ~áäìêÉëK

^ë ~ âÉó ÑÉ~íìêÉ Ñçê å~îáÖ~íáçå ë~ÑÉíóI íÜÉ ÇáÑÑÉêÉåÅÉ ~ä~êã ÜÉ~ÇáåÖ ëÉåJëçêë ÑìåÅíáçå~äáíó ëÜ~ää ~äï~óë ÄÉ ~ÅíáîÉ Ñçê ~ ë~áäáåÖ îÉëëÉäK

kÉîÉê áå~Åíáî~íÉ íÜÉ ÇáÑÑÉêÉåÅÉ ~ä~êã ÜÉ~ÇáåÖ ëÉåëçêë ÑìåÅíáçå~äáíó

EZ ëÉííáåÖ lccF ïáíÜçìí ÖççÇ êÉ~ëçåK

tôkfkd iáãáíÉÇ Ç~í~ ~ÅÅìê~Åó ÇìêáåÖ ~äáÖåãÉåí

^ÑíÉê ~ ÅçäÇ ëí~êíI íÜÉ k^sfd^q PMMM êÉèìáêÉë ~ ÅçãéäÉíÉ ~äáÖåãÉåí

íáãÉ ~í ëÉ~ çÑ ìé íç PM ãáåìíÉë ÄÉÑçêÉ êÉäá~ÄäÉ ÜÉ~ÇáåÖ Ç~í~ áë ~î~áä~ÄäÉK

^äï~óë éçïÉê ìé íÜÉ ëóëíÉã ~åÇ ï~áí ìåíáä íÜÉ ~äáÖåãÉåí áë ÅçãéäÉíÉäó

Ñáå~äáòÉÇ ÄÉÑçêÉ äÉ~îáåÖ Ü~êÄçìêK

mçïÉê Ççïå íÜÉ ëóëíÉã ÇìêáåÖ äçåÖ ÇçÅâáåÖ éÉêáçÇë çåäóK

^ ã~ÖåÉíáÅ Åçãé~ëë ÜÉ~ÇáåÖ ëçìêÅÉ ëÜçìäÇ ÄÉ ëÉäÉÅíÉÇ ~ë êÉÑÉêÉåÅÉçåäó áå Å~ëÉ çÑ Ñ~áäìêÉ çÑ íÜÉ ÖóêçÅçãé~ëëEÉëFK

tôkfkd kç Ç~í~ ~î~áä~Äáäáíó ÇìêáåÖ ÅçêêÉÅíáîÉ ã~áåíÉå~åÅÉ éêçÅÉÇìêÉë çÑ ~ ëáåÖäÉ

ÖóêçÅçãé~ëë ëÉåëçê ëóëíÉã

cçê ÅçêêÉÅíáîÉ ã~áåíÉå~åÅÉ éêçÅÉÇìêÉë ~ë ÉñÅÜ~åÖáåÖ çÑ íÜÉ fmpr ~åÇ

àr ëçÑíï~êÉ ~åÇ êÉéä~ÅáåÖ ëçÅâÉíÉÇ f`ë íÜÉ k^sfd^q PMMM ëóëíÉã áë

íç ÄÉ éçïÉêÉÇ Ççïå ~åÇ åç êÉäá~ÄäÉ å~îáÖ~íáçå Ç~í~ ~êÉ ~î~áä~ÄäÉ ìåíáä

íÜÉ éêçÅÉÇìêÉë ~êÉ ëìÅÅÉëëÑìääó ÅçãéäÉíÉÇK

^äï~óë ìëÉ Ü~êÄçìê ÇçïåíáãÉ çÑ íÜÉ îÉëëÉä íç éêçÅÉÉÇ ÅçêêÉÅíáîÉ ã~áåJ

íÉå~åÅÉ éêçÅÉÇìêÉëK ^äï~óë ã~âÉ ëìêÉ íç ëìÅÅÉëëÑìääó ÅçãéäÉíÉ ÅçêêÉÅJ

íáîÉ ã~áåíÉå~åÅÉ éêçÅÉÇìêÉë ÄÉÑçêÉ ìëáåÖ íÜÉ k^sfd^q PMMM ëóëíÉã

~Ö~áå Ñçê å~îáÖ~íáçå éìêéçëÉëK kÉîÉê ëí~êí ïáíÜ ÅçêêÉÅíáîÉ ã~áåíÉå~åÅÉéêçÅÉÇìêÉë ÇìêáåÖ ã~êáíáãÉ å~îáÖ~íáçå çÑ íÜÉ îÉëëÉäK


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`^rqflk Risk of harming European Dual Use RegulationsThe NAVIGAT 3000 sensor unit is export controlled in accordance to theEuropean Dual Use Regulations 428/2009 (EC).The Export Control Classification Number (ECCN) for the NAVIGAT 3000sensor unit is 7A003d.Any export of the NAVIGAT 3000 sensor unit hardware, software and or

technical data from a Member State of the European Community is sub-ject to export restrictions and requires an appropriate export licensegranted by the competent authorities of the Member State from wherethe export shall be conducted from.

`^rqflk Risk of erroneous operating conditions through inaccurate alignmentA successful alignment is essential for the error-free operation of theNAVIGAT 3000The system will immediately recognize if sensor measurements or exter-nal data inputs fall outside the permitted ranges. However, inaccurate orfalse data inputs (speed and/or position) within the permitted ranges can-

not be recognized.Should the system perform an alignment using inaccurate speed and/orposition data, the basis of the heading calculation will be flawed.As a result, erroneous heading values will be produced. This may happenafter a considerable time of apparently flawless operation.Restart the system and execute a new alignment using accurate speedand position inputs to make sure the system reaches error-free opera-tional mode.

`^rqflk Risk of erroneous operating conditions by using incorrect manual posi-tion input for the NAVIGAT 3000 systemIn the SAILING MODE as normal operational mode of the NAVIGAT 3000

system for a vessel navigating under sea conditions, the NAVIGAT 3000system receives automatic speed and position data from the GPS.For a vessel navigating under sea conditions, the use of manual positioninput is only allowed in case of emergency and when the automaticspeed/position input from the GPS is not available.Incorrect editing of manual position data can corrupt the functionality ofthe NAVIGAT 3000 system.Always use the SAILING MODE (with automatic GPS speed and GPSposition input) as normal operational mode of the NAVIGAT 3000 systemfor a vessel navigating under sea conditions.In case of emergency, be extremely careful to edit correct manual posi-tion data into the NAVIGAT 3000 system.

`^rqflk Risk of erroneous operating condition through inaccurate error alarmrecoveringIn systems incorporating the heading management system/compassmonitor NAVITWIN IV, make sure that the NAVIGAT 3000 fully recoversfrom the error when an alarm has been acknowledged remotely from theNAVITWIN IV. In certain cases, it may be necessary to take further actionto return the NAVIGAT 3000 to normal operation, e.g. it might berequired to change the speed/position data source or to initiate a newalignment (restart) of the system.


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`^rqflk Risk of recurring alarm conditionIn NAVIGAT 3000 systems incorporating the heading management sys-tem/compass monitor NAVITWIN IV, the „CHANGE TO INTERFACE“order MUST be assigned directly at the NAVITWIN IV, NOT at theNAVIGAT 3000 CDU.Assignment of „CHANGE TO INTERFACE“ at the NAVIGAT 3000 CDU

will be constantly rejected by the NAVITWIN IV, resulting in recurringindication of the initial Speed Failure.Always assign Change of Interface directly at the NAVITWIN IV, whenincorporated in the NAVIGAT 3000 system.

`^rqflk Risk of damage to the NAVIGAT 3000 gyrocompass through inadequateoperating conditionsInadequate operating conditions such as ambient over temperature,inadequate ventilation, wrong mounting position, instable fastenedmounting tray, caused by e.g. inadequate ground floor material, narrowmounting distances, flexible, instable or movable mounting surface, candamage the sensor and decrease the gyrocompass system performanceand the longevity of the system components.Always maintain, that the mounting tray must be installed full surface ona horizontal, stable, not swinging, metallic ground.Always maintain sufficient space and adequate ventilation conditionsaround the mounting position of the gyrocompass.Never use low heat conducting material close around the sensor orbeneath the mounting tray of the sensor.

`^rqflk Risk of erroneous heading accuracy caused by resonance frequencies orvibrationThe fiber optic sensor of the NAVIGAT 3000 gyrocompass is a highly sen-

sitive instrument. Resonance frequencies or vibrations caused by incor-rect install conditions will badly influence the heading accuracy.Always keep to the recommended install conditions and install themounting tray full surface on a horizontal, stable, not swinging, metallicground. Never install the sensor in a push drawer or console insertion.Make sure to minimise possible resonance frequencies or vibrationcauses at the mounting position of the NAVIGAT 3000 sensor.

`^rqflk Risk of erroneous heading accuracy caused by shockThe fiber optic sensor of the NAVIGAT 3000 gyrocompass is a highly sen-sitive instrument. Any external shock caused by impacts, heavy steps orthe like will be recognized and will badly influence the heading accuracy.

Always be extremely careful and avoid any shock or unnecessary touch-ing of the gyrocompass housing especially during operation.

`^rqflk Risk of damage through unauthorized serviceThe NAVIGAT 3000 sensor is not serviceable in the field. Defective sen-sor units must be returned to Sperry Marine for exchange.Any service work on the sensor is to be carried out by authorized servicepersonnel only.


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`^rqflk Breach of warrantyThe housing of the sensor carries two tamper seals. Breaking the sealsvoids the warranty.Never break the seals or open the housing of the NAVIGAT 3000 sensor.

`^rqflk Breach of warrantyUnauthorized service for the NAVIGAT 3000 sensor or theNAVIGAT 3000 system components voids the warranty.Never undertake unauthorized service.

`^rqflk Risk of erroneous heading accuracy caused by wrong speed inputThe NAVIGAT 3000 system requires two (2) Global Positioning System(GPS) receiver to be configured as source AUTO1 and AUTO2 for speedand position input data for a vessel operating under sea conditions.Speed data input from a speed log is not allowed to be configured as datainput and may corrupt the functionality of the NAVIGAT 3000 system.

Always make sure that two (2) GPS receiver are configured to providespeed and position data for the NAVIGAT 3000 system.

kçíÉ The connected GPS Receiver must be configured to transmit the GPSspeed and GPS position data to the NAVIGAT 3000 system via the follow-ing required messages:- VTG for speed and- GLL or GGA for position.

kçíÉ The two (2) GPS receiver need to become installed completely redundantto maintain GPS speed and position input, in case one GPS receiver fails.

kçíÉ Sperry Marine recommends that the two (2) GPS receiver are to be con-nected directly to the NAVIGAT 3000 system, not via any kind of distribu-tion or connection unit.

kçíÉ The REDUCED ACCURACY MODE can ONLY be indicated with the pre-condition of the vessel in SAILING MODE as previous operational mode,to highlight an occurring reduced accuracy condition of theNAVIGAT 3000 sensor.With the vessel in STATIONARY MODE as pre-condition, theREDUCED ACCURACY MODE can NOT be indicated.

kçíÉ The currently active operating mode of the NAVIGAT 3000 sensor is onlyindicated in the main menu and display data pages.

kçíÉ The SAILING Mode is the mandatory operational mode of any navigatingvessel and is preset by default according to factory settings.

kçíÉ The STATIONARY MODE is ONLY available as operational mode if spe-cifically preset by factory for a vessel designed to operate under dynamicpositioning (DP) conditions in a fixed position and MUST ALWAYS be

selected when the vessel is operating under DP conditions.


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kçíÉ If the STATIONARY MODE is preset for a specific vessel, the SAILINGMODE is ALWAYS selectable and MUST ALWAYS become selected incase the DP vessel is navigating under sea conditions.

kçíÉ In case the STATIONARY MODE as operational mode is necessary for a

vessel designed to operate under dynamic positioning (DP) conditions ina fixed position, but NOT PRESET by factory contact theSperry Marine Service for advice.

kçíÉ The new NAVIGAT 3000 system configuration described in thisOperation, Installation and Service Manual is only available from:NAVIGAT 3000 software version 1050,IPSU software version 2.401 andNAVITWIN IV software version 1.353 on.


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dÉåÉê~ä p~ÑÉíó fåÑçêã~íáçå Ñçê pÉêîáÅÉ mÉêëçååÉä

a^kdbo iáÑÉ Ç~åÖÉê íÜêçìÖÜ ÉäÉÅíêáÅ~ä ëÜçÅâ

tÜÉå íÜÉ k^sfd^q PMMM fmpr ^` ëìééäó éçïÉê áë ëïáíÅÜÉÇ çåI äáîÉ

îçäí~ÖÉë ~êÉ éêÉëÉåí ~í íÜÉ ^` áåéìí íÉêãáå~ä ÄäçÅâ Eq_ VFI íÜÉ äáåÉ ÑáäíÉê

Eic NF ~åÇ ~í íÜÉ éçïÉê íê~åëÑçêãÉêÛë íÉêãáå~ä ÄäçÅâ Eq_ NMFK^äï~óë ã~âÉ ëìêÉ íÜ~í íÜÉ fmpr ^` éçïÉê ëìééäó áë ëïáíÅÜÉÇ çÑÑ ~åÇ

ë~ÑÉÖì~êÇÉÇ ~Ö~áåëí ~ÅÅáÇÉåí~ä ëïáíÅÜáåÖJçåI ~äï~óë ÅÜÉÅâ íÜ~í íÜÉ

éçïÉê ëìééäó áë ~Åíì~ääó ëïáíÅÜÉÇJçÑÑ ~åÇ íÜ~í ÅçåÇìÅíáåÖ ÅçãéçåÉåíë

~êÉ ÅçîÉêÉÇI ÄÉÑçêÉ ÅçåÑáÖìêáåÖ íÜÉ ëóëíÉã Ñçê íÜÉ îÉëëÉäÚë ^` ëìééäó

îçäí~ÖÉK

kÉîÉê íçìÅÜ ~åó çÑ íÜÉëÉ é~êíë çê ~åó çÑ íÜÉ ÉäÉÅíêçåáÅ ÅáêÅìáíêó ïÜÉå

ëÉêîáÅáåÖ çê íêçìÄäÉëÜççíáåÖ íÜÉ ëóëíÉã ìåÇÉê éçïÉêK

^äï~óë ÉñÅäìÇÉ ~åó Åçåí~Åí íç ÉåÉêÖáòÉÇ ÅçãéçåÉåíëK

tôkfkd oáëâ çÑ ÉäÉÅíêáÅ~ä ëÜçÅâ çê Äìêå

e~ò~êÇçìë îçäí~ÖÉ áë éêÉëÉåí áåëáÇÉ íÜÉ k^sfd^q PMMM àrK

a~åÖÉê çÑ ÉäÉÅíêáÅ~ä ëÜçÅâ çê Äìêå ã~ó çÅÅìê ïÜÉå íÜÉ ``ci áåîÉêíÉêÅçååÉÅíáçåë ~êÉ íçìÅÜÉÇK

aáëÅçååÉÅí éçïÉê ÄÉÑçêÉ çéÉåáåÖ íÜÉ ÇÉîáÅÉK

kÉîÉê íçìÅÜ íÜÉ àr m`_ ïÜÉå ëÉêîáÅáåÖ íÜÉ ÇÉîáÅÉ ïáíÜçìí íÜÉ Ä~Åâ

ÅçîÉê áåëí~ääÉÇ ~åÇ ïÜáäÉ éçïÉê áë ~ééäáÉÇ íç íÜÉ Äç~êÇK

`^rqflk Risk of damage of electrostatic-discharge-sensitive componentsThe NAVIGAT 3000 system contains electrostatic sensitive components.Electrostatic discharge may permanently damage components.When troubleshooting the IPSU or CDU, take precautions to prevent elec-trostatic discharge. Avoid touching any of the electronic circuitry.

`^rqflk Risk of loss of parameter settings through software exchangeIt cannot be guaranteed that parameter settings in the User and Setupmenus and the entries made in the Magnetic Compass Calibration tableare left intact during an exchange of the system software.Before exchanging the flash-memory chip, IC 9, record all parameter set-tings to be able to re-enter them manually, if required.

`^rqflk Risk of damage to the NAVIGAT 3000 gyrocompass system throughinadequate installation / install conditionsInadequate install conditions or mounting distances can damage the sen-

sor and decrease the gyrocompass system performance and the longev-ity of the system components.Always keep the recommended install distances to ensure sufficientspace around the mounting position of the gyrocompass. Always installthe mounting tray full surface on a horizontal, stable, not swinging,metallic ground only. Always maintain adequate ventilation conditions.Never install the NAVIGAT 3000 sensor vertically or on instable, swing-ing or movable ground. Never install the sensor in a push drawer or con-sole insertion.Do not install the sensor in narrow boxes or small housings. Do notinstall the mounting tray on wooden floor or other low heat conductingmaterial. Never use low heat conducting material close around the sen-sor or beneath the mounting tray of the sensor.


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`^rqflk Risk of damage to the NAVIGAT 3000 gyrocompass through inadequateoperating conditionsInadequate operating conditions such as ambient over temperature,inadequate ventilation, wrong mounting position, instable fastenedmounting tray, caused by e.g. inadequate ground floor material, narrowmounting distances, flexible, instable or movable mounting surface, can

damage the sensor and decrease the gyrocompass system performanceand the longevity of the system components.Always maintain, that the mounting tray must be installed full surface ona horizontal, stable, not swinging, metallic ground.Always maintain sufficient space and adequate ventilation conditionsaround the mounting position of the gyrocompass.Never use low heat conducting material close around the sensor orbeneath the mounting tray of the sensor.

`^rqflk Risk of erroneous heading accuracy caused by resonance frequencies orvibrationThe fiber optic sensor of the NAVIGAT 3000 gyrocompass is a highly sen-sitive instrument. Resonance frequencies or vibrations caused by incor-rect install conditions will badly influence the heading accuracy.Always keep to the recommended install conditions and install themounting tray full surface on a horizontal, stable, not swinging, metallicground. Never install the sensor in a push drawer or console insertion.Make sure to minimise possible resonance frequencies or vibrationcauses at the mounting position of the NAVIGAT 3000 sensor.

`^rqflk Risk of erroneous heading accuracy caused by wrong speed inputThe NAVIGAT 3000 system requires two (2) Global Positioning System(GPS) receiver to be configured as source AUTO1 and AUTO2 for speed

and position input data for a vessel operating under sea conditions.Speed data input from a speed log is not allowed to be configured as datainput and may corrupt the functionality of the NAVIGAT 3000 system.Always make sure that two (2) GPS receiver are configured to providespeed and position data for the NAVIGAT 3000 system.

kçíÉ The connected GPS Receiver must be configured to transmit the GPSspeed and GPS position data to the NAVIGAT 3000 system via the follow-ing required messages:- VTG for speed and- GLL or GGA for position.

kçíÉ The two (2) GPS receiver need to become installed completely redundantto maintain GPS speed and position input, in case one GPS receiver fails.

kçíÉ Sperry Marine recommends that the two (2) GPS receiver are to be con-nected directly to the NAVIGAT 3000 system, not via any kind of distribu-tion or connection unit.


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kçíÉ The REDUCED ACCURACY MODE can ONLY be indicated with the pre-condition of the vessel in SAILING MODE as previous operational mode,to highlight an occurring reduced accuracy condition of theNAVIGAT 3000 sensor.With the vessel in STATIONARY MODE as pre-condition, theREDUCED ACCURACY MODE can NOT be indicated.



kçíÉ The STATIONARY MODE is ONLY available as operational mode if spe-cifically preset by factory for a vessel designed to operate under dynamicpositioning (DP) conditions in a fixed position and MUST ALWAYS be

selected when the vessel is operating under DP conditions.


kçíÉ Air-conditioning at place of installation for the NAVIGAT 3000 gyrocom-pass is recommended.

kçíÉ Swinging or instable metal ground at place of installation will cause res-

onance frequencies and vibration levels to the gyrocompass housing andtherefore interfere and decrease the accuracy of the fiber optic sensor.A push drawer or console insertion is therefore not allowed as mountingposition.

kçíÉ Low heat conducting material, as wood in example, close around thesensor or beneath the mounting tray may cause over temperature to thegyrocompass as such material does not sufficiently lead off waste heat.

kçíÉ For recording all parameter settings see “Setup and ConfigurationTables” in the appendix of this manual.

kçíÉ The new NAVIGAT 3000 system configuration described in thisOperation, Installation and Service Manual is only available from:NAVIGAT 3000 software version 1050,IPSU software version 2.401 andNAVITWIN IV software version 2.353 on.


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The NAVIGAT 3000 is a fiber-optic gyrocompass and attitude referencesystem for the maritime navigation of vessels and HSC (high speedcraft). Within the stationary mode, the NAVIGAT 3000 system is as wellapplicable as a stabilizer system for vessels operating under dynamicpositioning (DP) conditions in a fixed position, as drilling ships or float-ing platforms.

The NAVIGAT 3000 fiber-optic gyrocompass and attitude reference sys-

tem must only be operated from appropriately trained and educatedpersonnel familiar with all mandatory safety and operating procedures.

The NAVIGAT 3000 provides true heading data, rate of turn (ROT) data,pitch and roll angels and rates data and heave data for the navigation ofmaritime vessels and ships operating under dynamic positioning (DP)conditions in a fixed position.

Speed and position data itself are generated and received from externalsources. For intended use, the NAVIGAT 3000 system is dependent onspeed and position input data to be received from two separately con-nected GPS receiver.

The NAVIGAT 3000 can operate as a standalone system or as part of amulti gyrocompass system environment (Heading Management Sys-tem, HMS).

kçí fåíÉåÇÉÇ rëÉ

The NAVIGAT 3000 and/or all the provided true heading, ROT and othernavigation output data of the NAVIGAT 3000 are not allowed to be usedfor the navigation of inland water vessels and river boats.

The stationary mode of the NAVIGAT 3000 is expressly designed for avessel operating under dynamic positioning (DP) conditions in a fixedposition and must never be assigned while the vessel is navigatingunder sea operating conditions.

Although the NAVIGAT 3000 is a highly accurate system for providingnavigation data, the operator must not rely on it solely as the only head-ing source. The plausibility of the NAVIGAT 3000 navigation data mustalways be confirmed against all other available aids to navigation.

Since the NAVIGAT 3000 may additionally be used for displayingsecondary navigation data generated from other connected devices, theoperator must not take displayed secondary data for granted and is

obliged to confirm the validity of secondary data independently.


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NKO póëíÉã lîÉêîáÉï

cáÖìêÉ NJNW

cêçåí îáÉï

k^sfd q̂ PMMM

cáÖìêÉ NJOW cêçåí îáÉï ïáíÜ éçïÉê ÅçååÉÅíçê gNI íê~ó Ñ~å gO Eåçí áå ìëÉFI íÉëí fc ÅçååÉÅíçê gR

~åÇ ìëÉê ÅçååÉÅíçê gSK

LED

J1

J2

Mode

J6

J5

Button


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póëíÉã lîÉêîáÉï NJP

cáÖìêÉ NJPW

qçé îáÉï

k^sfd^q PMMM

Figure 1-3 shows top plate with product label, special care and cautionlabels and type label 1 (all labels are shown inversed).

kçíÉ The product label shows the ahead arrow sign for the installationdirection.


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cáÖìêÉ NJQW

páÇÉ éä~íÉ

k^sfd q̂ PMMM

Figure 1-4 shows the left side plate with the type label 2.

cáÖìêÉ NJRW

dêçìåÇ éä~íÉ

k^sfd q̂ PMMM

cáÖìêÉ NJSW

oÉ~ê éä~íÉ

k^sfd q̂ PMMM

Type label 2


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póëíÉã lîÉêîáÉï NJR

cáÖìêÉ NJTW

jçìåíáåÖ íê~ó

Figure 1-7 shows the mounting tray of the NAVIGAT 3000 with mount-ing tray type label, fixed clamping plates and attachment holes.

cáÖìêÉ NJUW

k^sfd^q PMMM çå

ãçìåíáåÖ íê~ó

Figure 1-8 shows the NAVIGAT 3000 sensor installed with clampingplates on the mounting tray.


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NJS póëíÉã lîÉêîáÉï

i~ÄÉä ~åÇ íóéÉ éä~íÉë

cáÖìêÉ NJVW

k^sfd q̂ PMMM

ä~ÄÉä

cáÖìêÉ NJNMW

k^sfd q̂ PMMM

íóéÉ ä~ÄÉä N

cáÖìêÉ NJNNW

k^sfd q̂ PMMM

íóéÉ ä~ÄÉä O

cáÖìêÉ NJNOW

jçìåíáåÖ íê~ó

íóéÉ ä~ÄÉä

cáÖìêÉ NJNPW

fmpr íóéÉ ä~ÄÉä

BAR CODE STOCK No

BAR CODE SER No

BAR CODE EQUIPMT. No

1PN 146179-5100-001

BAR CODE STOCK No

BAR CODE SER No

kçíÉ All labels on this page are shown inversed.

The original labels are black with white writing.


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póëíÉã aÉëáÖå ~åÇ j~áå cÉ~íìêÉë NJT

NKP póëíÉã aÉëáÖå ~åÇ j~áå cÉ~íìêÉë

The NAVIGAT 3000 is a fiber-optic gyrocompass and attitude referencesystem in a solid-state, fully electronic configuration.The NAVIGAT 3000 is designed for marine gyrocompass systems, inte-grated bridge systems and advanced high-speed vessels operating inthe gyrocompass mode (normal operational mode) and for vessel oper-ating under dynamic positioning (DP) conditions in a fixed position (sta-tionary mode), as drilling ships or floating platforms.

The Inertial Reference System of the NAVIGAT 3000 sensor is based ona fiber optical instrument assembly (FOG IMU) and micro mechanicalaccelerometer technology in a strapdown configuration to provide highaccurate attitude, heading, rate, heave, acceleration and geographicalposition.

The NAVIGAT 3000 needs external course over ground, velocity and lat-itude / longitude data provided from two separate Global Positioning

System (GPS) receiver when operating in the SAILING MODE (normaloperational mode).

In the STATIONARY MODE, the NAVIGAT 3000 does not need to receiveGPS data, as the stationary mode is designed to suit the purposes of sta-tionary vessels operating under dynamic positioning conditions in afixed position.

The REDUCED ACCURACY MODE can only be indicated with the pre-condition of the vessel in SAILING MODE as previous operational mode,to highlight an occurring reduced accuracy condition of the NAVIGAT3000 sensor. With the vessel in STATIONARY MODE as pre-condition,

the REDUCED ACCURACY MODE can not be indicated.

The NAVIGAT 3000 has been type approved by Germanischer Lloyd(GL), in accordance with the Marine Equipment Directive (MED) 96/98/ EC, as modified by Directive 2010/68/EC, as gyrocompass (certificate no.37 757-12 HH), gyrocompass for high speed craft (HSC) (certificate no.37 957-12 HH) and rate of turn indicator (ROTI) (certificate no. 37 959-12 HH).

The NAVIGAT 3000 complies with the following specified standards:Gyrocompass: IMO resolutions A.424 (XI), A.694 (17), MSC.191 (79)ISO 8728 (1997), IEC 60945 (2002) incl. corr. 1 (2008, IEC 62288 (2008),IEC 61162 series.

Gyrocompass for high speed craft (HSC): IMO resolutions MSC.97 (73),A.821 (19), A.694 (17), MSC.36 (63), MSC.191(79)ISO 16328 (2001), IEC 62288 (2008), IEC 61162-1, IEC 60945 (2002) incl.corr.1 (2008).Rate of turn indicator (ROTI): IMO resolutions: A.526 (13), A.694 (17),MSC.191(79), MSC.97(73), MSC.36(63)Testing standards: EN 61162 series, EN 60945 (2002) incl. corr. 1 (2008),ISO 20672 (2007), IEC 62288 (2008).

For further details see “Declaration of Conformity” on page 1-23.


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NKQ léÉê~íáåÖ mêáåÅáéäÉ çÑ íÜÉ pÉåëçê

Through the IPSU interfaces, the NAVIGAT 3000 sensor provides meas-ured and calculated data of heading, roll and pitch angles, heave, veloc-ities and angular rates, as well as mode of operation and statusinformation to the user systems. For the definition of the provided data

see “System Polarity Definitions” on page 1-21.

All system data are being transmitted via the RS422 interface to theNAVIGAT 3000 sensor. The scaling and protocols of how to transmit thedata are defined in Chapter ‘System Configuration” on page 6-1.

The sensor concept is based on an inertial system family of productswhich use an instrument assembly with high-performance fiber-opticalgyros (FOG's) and the micro-mechanical accelerometer triad. The Navi-gation Computer of the NAVIGAT 3000 sensor uses a high-performanceprocessor to execute all system software. The Navigation Computerreceives the inertial sensor data from the fiber-optical gyros and acceler-

ometers (angular increments, velocity increments) as well as data fromexternal inputs (EM Log/DVL, GPS) to execute the following tasks of theanalytic platform:

• inertial sensor error compensation

• platform calculation to provide attitude and heading data

• operation of the systems Kalman Filter

• calculation of navigation data such as heading, pitch and roll, heave

• handling of the external position input data

• incorporation of extensive built-in test (BIT) functions

• scaling, formatting and transmission of the output dataThe Power Supply Module receives the external 28 VDC supply voltagefrom the IPSU and generates the required internal secondary voltages.

cáÖìêÉ NJNQW

k^sfd q̂ PMMM ëÉåëçê

áåíÉêå~ä ÅçãéçåÉåíë ~åÇ

áåíÉêÑ~ÅÉ ÅçååÉÅíáçåë

Figure 1-14 shows internal main components and interface connectionsof the NAVIGAT 3000 sensor.

Power Supply

Module

Processor

Module

R

S - 4 2 2

H D L C

FOG

IMU

RS-422 User Interface

28 VDC Power Supply

(external)


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The north-seeking element used in the NAVIGAT 3000 sensor is thefiber-optic sensor unit type “5021”. The sensor unit is a solid-state

design with no moving parts. Designed in strapdown technology, it isattached directly to the vessel, eliminating the use of a gimbal system.

The NAVIGAT 3000 sensor unit contains three fiber-optic rate gyros, atri-axis MEMS accelerometer and a sensor processing unit in an fiberoptical instrument assembly (FOG IMU), a navigation processor unit anda power supply.

Figure 1-15 on page 1-10 shows the internal main components of theNAVIGAT 3000 sensor.

cáÖìêÉ NJNRW

k^sfd q̂ PMMM ëÉåëçê

áåíÉêå~ä ã~áå ÅçãéçJ

åÉåíë

The three rate gyros are mounted at right angles to each other, and thusmeasure the rotation of the system about the vessel-referenced X, Y andZ axes. The accelerometer sensor measures the inertial acceleration ofthe system about the vessel-referenced X, Y and Z axes.

This configuration is used to mechanize the so called „analytical plat-form“.

From the vessel-referenced sensor measurements and the externalspeed and position inputs, the navigation processor derives the direc-tion of true North, using a complex Kalman filter algorithm.

To initialize the gyro compass mode, an alignment is performed whenthe system starts up. During the gyro compass operation, the systemcontinuously performs two essential tasks which make it north-seeking,

namely horizontation and north orientation.

kçíÉ The 28 VDC power supply of the NAVIGAT 3000 sensor is provided fromthe IPSU.

FOG

IMU

Power Supply Module

Processor

Module


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As the tasks of horizontation and North orientation are performed con-tinuously, the NAVIGAT 3000 system is not subject to loss of accuracydue to drift effects, that occur in other inertial navigation systems usede.g. in aviation, which merely sum up changes of attitude over time.

At power-up, the system estab-lishes a virtual plane, fixed in space,the so-called inertial plane.

Evaluating the data from the MEMSaccelerometer, the system is able todetermine how the inertial planewould have to be tilted to bring itinto the horizontal at the vessel’slocation.Through transformation of themeasured rates, the system is alsoable to determine how the vessel’smovements and the earth’s rotationact on the virtual horizontal plane.

Evaluating the data from the exter-nal speed and position inputs, thesystem is able to calculate the com-ponent of the earth’s rotation which

acts upon the virtual horizontalplane and thus knows the rate atwhich the plane must be tilted toalways keep it horizontal on therotating earth’s surface.

Through evaluating the plane’smovements over time, it is also pos-sible to determine the direction oftrue North. This is accomplished bymathematically rotating the planeuntil its North-South axis will not tilt

due to the earth’s rotation.


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NKR bñ~ãéäÉ póëíÉã `çåÑáÖìê~íáçåë

pí~åÇ~äçåÉ dóêçÅçãé~ëë póëíÉã

In a standalone system, the NAVIGAT 3000 CDU displays heading andattitude data from the fiber-optic sensor unit.

cáÖìêÉ NJNSW

pí~åÇ~äçåÉ

dóêçÅçãé~ëëLqj`

ëóëíÉã

2nd GPS Receiver

1st GPS Receiver

Rudder Angle

Feedback Unit(s)

Status Signals In

Serial Repeaters

Equipment using

serial input

Equipment using

6 step/ input

AnalogueIndicators

Nav. Data

Printer

Status Signals Out

(ROT, Roll, Pitch)


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pí~åÇ~êÇ aì~ä dóêçÅçãé~ëëLqj` póëíÉã

Figure 1-17 below shows the standard configuration for a dualNAVIGAT 3000 gyrocompass system with a separate IPSU and CDU foreach NAVIGAT 3000 gyrocompass installed.In addition to the two NAVIGAT 3000 gyrocompasses, this system com-prises the NAVITWIN IV Heading Management System (HMS) and theSwitch-Over Unit Type 4932.

By selecting the active heading source at the NAVITWIN IV, the operatordetermines which compasses’ data is distributed via the Switch-OverUnit to external equipment, such as heading control systems, RADAR,compass repeaters etc.

The heading diff. alarm function permits to monitor the differencebetween any two of the available heading sources. The off headingalarm function permits to monitor the difference between the actualheading from the active source and the set heading order, as received

from a heading control system or entered manually.

Alarms generated locally by a NAVIGAT gyrocompass are indicated andmay be acknowledged at the NAVITWIN IV.In turn, the NAVITWIN IV transmits system-wide operational settingsand setup parameters to the NAVIGAT gyrocompasses.The available heading sources, the current source selection and the hdg.diff. threshold are also indicated at the gyrocompasses.

If a magnetic compass heading source is installed, the NAVIGAT 3000system applies magnetic variation and distributes the data to externalequipment (TMC function). In case of failure of the gyrocompasses, the

magnetic compass heading source may be activated to provide anemergency heading reference for repeaters and other peripheral equip-ment.

cáÖìêÉ NJNTW

k^sfd q̂ PMMM aì~ä

dóêçÅçãé~ëë póëíÉã

GYRO

1

GYRO

2

MAGN

COMP

246.8

246.7

247.0

G1 Hdg.

G2 Hdg.

M Hdg.

Source Sel.Status

Alarm Status (Hdg. Diff, Off Hdg)

G/ M Headings,

RoT, and all other

data/signals distributed via

Switch-Over Unit

Switch-Over Unit

NAVITWIN IV

G1

M

G2


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pí~åÇ~êÇ qêáéäÉ dóêçÅçãé~ëëLqj` póëíÉã

A standard configuration of a triple NAVIGAT 3000 gyrocompass sys-tem consists of three NAVIGAT 3000 gyrocompasses each with a sepa-rate IPSU and CDU, the NAVITWIN IV heading management system andthe Switch-Over Unit Type 4932.

All additional functionality (e.g. heading diff. alarm function) as men-tioned above for a dual gyrocompass system apply accordingly for a tri-ple gyrocompass system.

kçíÉ A dual gyrocompass system with one NAVIGAT 3000 and one NAVIGAT2100 or NAVIGAT X MK 1 gyrocompass is also possible in an otherwiseidentical configuration.

kçíÉ A triple gyrocompass system with a combination of NAVIGAT 3000 gyro-compasses and NAVIGAT 2100 or NAVIGAT X MK 1 gyrocompasses isalso possible in an otherwise identical configuration.


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qÉÅÜåáÅ~ä a~í~ NJNR

NKS qÉÅÜåáÅ~ä a~í~

cáÄÉêJléíáÅ pÉåëçê råáí

aáãÉåëáçåë ~åÇ tÉáÖÜí

Width 102 mm

Depth 278 mm

Height 128 mm

Weight 3 kg approx., 4 kg with mounting tray

^ÅÅìê~ÅáÉë EìåÇÉê ~ää çéÉê~íáåÖ ÅçåÇáíáçåëF

Heading ≤

0.4° secant latitude (RMS)Roll and pitch angles ≤ 0.1° for angles ≤ 45° (95%)

(reduced accuracy for anglesbetween 45° and 180°)

Rate of turn, ≤ 0.018°/minute

X and Y rates ≤ 0.4°/minute

Heave 0.1 m (95%); max. ± 128 mamplitudes less than 2.5 m;frequency: 0.16 Hz ≤ f ≤ 3 Hz

léÉê~íáçå~ä `Ü~ê~ÅíÉêáëíáÅëSettling time w/ static alignment ≤ 210 seconds (Latitude ≤ 45°)

Settling time w/ static alignment ≤ 10 minutes (Latitude ≤ 78°)

Settling time w/ alignment at sea ≤ 30 minutes (Latitude ≤ 78°)

Max. follow-up speed 100°/s

`çããìåáÅ~íáçå fåíÉêÑ~ÅÉë

User Input/Output RS422, Binary Digital Interface

mçïÉê ëìééäó

Supply voltage 28 VDC nom. (18 - 33 VDC)

Power input IEC 60945

Voltage spike, ESD IEC 60945

Max. ripple content DC supply ± 4 Vpp; extreme values may notexceed 36 V or fall below 18 V

Power consumption:Basic system (1 x IPSU + 1 x CDU+ 1 NAVIGAT 3000 sensor:

NAVIGAT 3000 sensor, aloneeach repeater compass:

64 W max. (at 234 VAC)40 W max. (at 23,35 VDC)

26 W max.6 W max.


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NJNS qÉÅÜåáÅ~ä a~í~

båîáêçåãÉåí~ä oÉèìáêÉãÉåíë

Environmental conditions / EMC In accordance with IEC 60945 orDO-160

mêçíÉÅíáçå dê~ÇÉ

Waterproofness IP 23

qÉãéÉê~íìêÉ `çåÇáíáçåë

Ambient temperature range,operation

- 15° C – + 55° C / 5° F – 131° F

Recommended operational tem-perature conditions for highestsystem longevity:

ambient temperature

ambient temperature variation

- 15° C – + 25° C / 5° F – 77° F

< 2° C/min / < 35,6° F/min

Ambient temperature, storage - 35° C – + 70° C / - 31° F – + 158° F

bäÉÅíêçã~ÖåÉíáÅ `çãé~íáÄáäáíó Ebj`F L bäÉÅíêçã~ÖåÉíáÅ fåíÉêÑÉêÉåÅÉ

according to IEC 60945:

minimum clearance to MF/HF transceiverunits and their antennas.

1.5 m

minimum clearance to high voltage powerlines > 380 VAC of other equipment

1.5 m

sáÄê~íáçå

according to GL: „Rules for Classification andConstruction, I - Ship Technology, Part 1 - Sea-going ships, Chapter 2 - Machinery Installa-tions“, Edition 2000

Applicable in Area Aclassified locations

according to IEC 60945 Vibration level

j~ÖåÉíáÅ `äÉ~ê~åÅÉ

To standard magnetic compass 0.70 m

To steering magnetic compass 0.50 mReduced, to standard magnetic compass 0.50 m

Reduced, to steering magnetic compass 0.30 m

kçíÉ To maintain the environmental requirements for the operation of theNAVIGAT 3000 sensor, it is mandatory to follow all safety and installationinstructions. Correct mounting distances and material requirementsneed always be followed; see chapter ‘Installation” on page 5-1 and therespective drawings in the appendix of this manual.


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qÉÅÜåáÅ~ä a~í~ NJNT

fåíÉêÑ~ÅÉ ~åÇ mçïÉê pìééäó råáí



Width 524 mm

Height 341 mmDepth 123 mm

Weight 15 kg approx.


Ambient temperature range,

operation

- 15° C – + 55° C / 5° F – 131° F





To steering magnetic compass 0.65 m

Reduced, to standard magnetic compass 0.60 m



According to IEC 60529/DIN 40050(bulkhead mounting per dwg. 4913-0120-01)

IP 23


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NJNU qÉÅÜåáÅ~ä a~í~

`çåíêçä ~åÇ aáëéä~ó råáí



mk TQUNQ EÑçê ÅçåëçäÉ ãçìåíáåÖF

Width 288 mmHeight 96 mm

Depth 44 mm; approx. 100 mm backward clearancefrom mounting surface required for connectorcable and plug

Weight 1 kg approx.

mk TVPSO Emk TQUNQ Ñ~ÅíçêóJ~ëëÉãÄäÉÇ áå ÅçåëçäÉ Ñê~ãÉF

Frame width 319 mm

Frame height 127 mm

mk TQUOM Eáå ÜçìëáåÖ ïáíÜ Äê~ÅâÉíF

Width 350 mm

Max. height (unit invertical position)

150 mm

Max. depth (unit inhorizontal position)

130 mm

Weight 2.15 kg approx.


Ambient temperature range,operation

- 15° C – + 55° C / 5° F – 131° F





To steering magnetic compass 0.30 m

Reduced, to standard magnetic compass 0.30 m



According to IEC 60529/DIN 40050,PN 74814, front side (console mounting)

IP 43

PN 74820 (in housing with bracket) IP 23


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qÉÅÜåáÅ~ä a~í~ NJNV

fåJ ~åÇ lìíéìí fåíÉêÑ~ÅÉë

a~í~ fåéìíë

True heading (2x) Fiber-optic sensoror NMEA 0183 / IEC 61162-1

or PLATH protocolor Lehmkuhl (1200, 2400, 4800 or9600 Bd.)

Magnetic compass heading NMEA 0183 / IEC 61162-1or PLATH protocolor NAVIPILOT

GPS Position (2x) NMEA 0183 / IEC 61162-1

GPS Speed (2x) NMEA 0183 / IEC 61162-1

Compass monitor NAVITWIN IV NMEA 0183 / IEC 61162-1

páÖå~ä ~åÇ pí~íìë fåéìíë

Magnetic compass heading,fluxgate sensor

Sin., cos. and ref. voltages fromSperry Marine fluxgate sensortype 4863

Rudder angle feedback unit(2x; reads rudder angle for outputto NAVIPRINT)

± 12 VDC return voltage fromfeedback potentiometer(s)

Steering mode status (auto/man) Connection to P.Gnd viaext. contact, latching

Switch-over unit status Connection to P.Gnd via

ext. contact, latching

Ext. alarm acknowledge (mute)1

1 if an ext. alarm mute input is required, the serial magn. heading input

is not available.

Connection to fluxgate Gnd viaext. contact, momentary


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NJOM qÉÅÜåáÅ~ä a~í~

a~í~ lìíéìíë

Heading sensor outputs(2x RS-422)

Fiber-optic sensorcontrol dataor NMEA 0183 / IEC 61162-1to ext. gyro / compass monitor

NAVITWIN IVSerial repeater outputs(12x TTL)

NMEA 0183 / IEC 61162-1

Sensor data outputs(2x RS-422, 2x TTL)

NMEA 0183 / IEC 61162-1

FAST output NMEA 0183 / IEC 61162-1or PLATH protocol(update rate 20 Hz)or TSS1 protocol (roll/pitch only)

SuperFAST output NMEA 0183 / IEC 61162-1or NMEA 0183 / IEC 61162-2

or PLATH protocol(update rate 20 Hz)

NAVIPRINT output Serial data to nav. data printer

páÖå~ä ~åÇ pí~íìë lìíéìíë

6 step/° output (2 x) 3 phases, switched to 0V potentialif active („minus switching“),common positive;internal supply 24 VDCmax. 18 W(12 – 70 VDC phase voltage w/ext.power supply)

Rate of turn, analogue ± 0.1 – 999.9 mV/°/min;max. 10 V, 10 mA

X rate or roll angle, analogue ± 0.1 – 999.9 mV/°/minor ±0.1 – 999.9 mV/°;max. 10 V, 10 mA

Y rate or pitch angle, analogue ± 0.1 – 999.9 mV/°/minor ± 0.1 – 999.9 mV/°;max. 10 V, 10 mA

X rate, current, analogue ± 0.1 – 99.9 mA/°/min;

range: 4 – 20 mA

Power failure/general alarm Potential-free relay contacts,each rated60 W/125VA,max. 220VDC/250VAC,max. 2.0 A

Heading difference alarm


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qÉÅÜåáÅ~ä a~í~ NJON

póëíÉã mçä~êáíó aÉÑáåáíáçåë

Max. ROT exceeded alarm Potential-free relay contacts,each rated30 VDC/1.0 A,100 VDC/0.3 A,

125 VAC/0.5 A

Heading source sel. status

Status out to switch-over unit

Watch alarm acknowledge

Mute out

Watch alarm (out)

Heading angle The heading angle is defined as posi-tive when the vessel front is more atEast then the aft. A starboard turn

causes an increasing heading angleand is defined as a positive rotation.

Roll angle The roll angle is defined as positivewhen the vessel rolls to starboardaround the vessel's center-line (star-board down is positive).

Pitch angle The pitch angle is defined as positivewhen the vessel rotates with bow ris-ing around the axis transverse to thevessel's centre line (bow up is posi-tive).

Heading rate The heading rate is measured in alocal horizontal plane and is definedas positive when the vessel turns tostarboard from North to East (clock-wise turn).

Roll rate The roll rate is measured in a localhorizontal frame and is defined aspositive when the vessel rolls to star-board around the vessel's centerline(starboard down is positive).

Pitch rate The pitch rate is measured in a local

horizontal frame and is defined aspositive when the vessel rotates withbow rising around the axis trans-verse to the vessel's centerline (bowup is positive).

X angular rate The X angular rate is measured in thesystems body frame and is definedas positive when the vessel rolls tostarboard around the vessel's center-line (starboard down is positive).

páÖå~ä ~åÇ pí~íìë lìíéìíë


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NJOO qÉÅÜåáÅ~ä a~í~

Y angular rate The Y angular rate is measured in thesystems body frame and is definedas positive when the vessel rotateswith bow rising around the axistransverse to the vessel's centerline(bow up is positive).

Z angular rate The Z angular rate is measured in thesystems body frame and is definedas positive when the vessel turns tostarboard from North to East.

Heave The Heave measurement is definedas positive when the vessel is belowaverage sea level.


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aÉÅä~ê~íáçå çÑ ̀çåÑçêãáíó NJOP

NKT aÉÅä~ê~íáçå çÑ `çåÑçêãáíó

j~êáåÉ bèìáéãÉåí aáêÉÅíáîÉ b` aÉÅä~ê~íáçå çÑ `çåÑçêãáíóW

Northrop Grumman Sperry Marine B.V.Woltmanstrasse 19D-20097 Hamburg, Germany.

as manufacturer hereby declares that the following specified equip-ment:

“NAVIGAT 3000 Fiber-Optic Gyrocompass and Attitude Reference Sys-tem”

complies with the Marine Equipment Directive 96/98/EC, as amended.

This equipment has been tested to verify compliance with the Regula-tions and Testing Standards as per EC Type Examination (B) and ECQuality System (D) issued by:

Notified Body No. 0098 Germanischer Lloyd.

kçíÉ The current issue of the detailedMarine Equipment Directive EC Declaration of Conformity ofNorthrop Grumman Sperry Marine B.V. Hamburg is part of the client CDstock no. 56 800.For further details please contact:Northrop Grumman Sperry Marine B.V. HamburgEngineering Support


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NJOQ aÉÅä~ê~íáçå çÑ ̀çåÑçêãáíó


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`Ü~éíÉê OW léÉê~íáçå

OKN léÉê~íáåÖ `çåÇáíáçåë

As a solid state device, the NAVIGAT 3000 is not subject to the mechani-cally induced errors which occur in conventional gyrocompasses.

However, because the heading is determined mathematically from thesensor measurements and from external data, the inputs to the systemmust lie within certain ranges.

The specified system accuracies will be attained if the following limitsfor internal (sensed) and external data are not exceeded:

• Roll and pitch angles: ± 45°.

• Turn rates, around all axes: ± 50°/s.

• Acceleration, along all axes: ± 19,5 m/s².

• Max. speed: ± 75 kn.

• Latitude: between 78° S and 78° N.

• Accuracy of speed input: ± 1.0 kn, update rate between 1 and 50 Hz.

The system will continue to operate with reduced accuracies within thefollowing maximum limits:

• Body angular rates (X, Y, Z angular rates), around all axes: ± 210°/s.

• Acceleration 98,1 m/s² (measurement range).

• Latitude: between 85° S and 85° N.

^äáÖåãÉåí oÉèìáêÉãÉåíë

`^rqflk Risk of erroneous operation condition through inaccurate alignmentA successful alignment is essential for the error-free operation of theNAVIGAT 3000.The system will immediately recognize if sensor measurements or exter-

nal data inputs fall outside the permitted ranges. However, inaccurate orfalse data inputs (speed and/or position) within the permitted ranges can-not be recognized.Should the system perform an alignment using inaccurate speed and/orposition data, the basis of the heading calculation will be flawed.As a result, erroneous heading values will be produced. This may happenafter a considerable time of apparently flawless operation.A new alignment using accurate speed and position inputs will be neces-sary to recover from such a condition.


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OJO léÉê~íáåÖ ̀çåÇáíáçåë

To perform a successful alignment, the following additional require-ments are to be met:

• In case of manual position input, the latitude value must be editedwithin an accuracy of ± 0.3°.

• Roll and pitch angles shall be ≤ 80°.

• The latitude shall be < 78°.

• Conditions for dynamic alignment are:

– Heading change < 30° and heading rate ≤ 3°/s(with GPS data available)

• Conditions for static alignment are:

– Angular rates < ± 0.2°/s

– Horizontal acceleration < ± 0.1 m/s²

kçíÉ See “Startup/Align Procedure” on page 2-5 and “Alignment Conditions”on page 2-8 for details.


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aáëéä~ó ~åÇ léÉê~íáåÖ hÉóë OJP

OKO aáëéä~ó ~åÇ léÉê~íáåÖ hÉóë

`çåíêçä ~åÇ aáëéä~ó råáí àr

cáÖìêÉ OJNWk^sfd^q PMMM

Åçåíêçä ~åÇ Çáëéä~ó ìåáí

àr

cáÖìêÉ OJOW

k^sfd^q PMMMàr çîÉêîáÉï Çáëéä~ó

~åÇ çéÉê~íáåÖ âÉóë

Fiber-Optic Gyrocompass

NAVIGATSperry Marine

eÉ~ÇáåÖ pçìêÅÉ táåÇçïW Shows the available heading source andthe actual heading value. The currently active heading source isindicated by a bold frame and arrows next to the source’s name.

eÉ~ÇáåÖ aáÑÑÉêÉåÅÉ ^ä~êã táåÇçïWShows heading difference alarm, heading source and headingthreshold, if active.

jÉåì táåÇçïW Shows the operating menu screens and displayssystem messages and alarm messages.

eÉ~ÇáåÖ pçìêÅÉ pÉäÉÅíçê hÉóëW Selects the currently active headingsource (disabled if source is selected through external devices).

^`h âÉóW Mute key, inactive for the NAVIGAT 3000 system.

k~îáÖ~íáçå hÉóé~ÇW Arrow keys navigate through menu screens; bkqbo key confirms and stores selections made in menus.

jbkr âÉóW Exits sub-menu and returns to next higher menu level.

cN LcOLcP âÉóëW Go to sub-menus or execute special functionassigned to respective key.

afjJ L afjH âÉóëW Adjust the display brightness.

GYRO1

SAIL MAIN MENU GYRO 1

F1 DISPLAY DATA

F2 MANUAL SETTINGS

F3 SETUP MENU

246.8 °

ALARM

HEAD. DIFF.

Sperry Marine

NAVIGAT 3000

4 1 6

83 9

752

SOURCE THRESH.

G1/G2 10°


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OJQ bñíÉêå~ä ̀çåíêçä aÉîáÅÉë

OKP bñíÉêå~ä `çåíêçä aÉîáÅÉë

Depending on the installation, external devices may be present whichremotely control certain functions of the NAVIGAT 3000:

• An external device may be used to select the “active” source, i.e. the

heading reference to be distributed to compass repeaters, headingcontrol system, RADAR, ECDIS etc.

• An external selector switch may be used to reverse the heading(apply a 180° offset to the heading data) e.g. for operation in double-ended ferries.

• The audible alarm at the NAVIGAT 3000 may be muted from aremote device, e.g. a central alarm panel.


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pí~êíìéL^äáÖå mêçÅÉÇìêÉ OJR

OKQ pí~êíìéL ä̂áÖå mêçÅÉÇìêÉ

The NAVIGAT 3000 system is not equipped with a power switch. Thesystem powers up as soon as the power supply is applied.

1. Upon power-up, the system test is executed:

2. Each system step test is indicated with the name of the step followedby „OK“, when the test is passed successfully.

3. When all the system test steps has been passed successfully, theNAVIGAT 3000 starts automatically with the initialization and align-ment phase of the fiber-optic sensor.

After a short period of time the initialization phase ends and the sensorstarts automatically with the alignment process.

A startup screen is shown.A status line at the bottom of thescreen indicates the progressand results of the following con-secutive system test steps:- System test- RAM test- I/O test- Checksum test- Setup Data test

The heading display shows„dashes“ (no data available)

alternating with „ALIGN“ and„SYSTEM ALIGN /ALIGN TIME: 0 MIN“ in themenu window.

NAVIGAT

System Test

NN.NN

GYRO

1

SYSTEM ALIGN

ALIGN TIME: 0 MIN

---.- °Sperry Marine

NAVIGAT 3000

kçíÉ If the alignment process does not start after a short period of time, theinitialization phase was not successful and the Startup/Align procedure

must be repeated.

In the menu window, the currentperiod of time in minutes sincethe start of the align phase isconstantly displayed (e.g. 5 min)as long as the alignment lasts.

GYRO

1

SYSTEM ALIGN

ALIGN TIME: 5 MIN


NAVIGAT 3000


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OJS pí~êíìéL^äáÖå mêçÅÉÇìêÉ

During the align phase, the heading data from the fiber-optic sensor arenot yet available at the data outputs. External devices, including anexternal gyro in a dual gyrocompass system and the NAVITWIN IV, willnot receive heading data from the NAVIGAT 3000 system as long as thealignment is not finalized.

During alignment, the operator may use all the display keys to scrollthrough the menu and submenus.

When returning from menu indication, the current period of time sincethe start of the alignment is again indicated in the menu window.

⇒ The currently active operating mode is also indicated in all displaydata pages, see “Display Data Pages - Gyrocompass Mode” on page 2-20 and “Display Data Pages - Stationary Mode” on page 2-21.

oÉJ^äáÖåãÉåí eÉ~ÇáåÖ fåÇáÅ~íáçå

After complete alignment, theindication “ALIGN” will disap-pear from the display, the com-puted heading data becomesavailable at the data outputs, theNAVIGAT 3000 system willbecome fully operational andthe main menu is shown in themenu window.

⇒ On the left side of the menuwindow the currently activeoperating mode is indicated inall main menu windows, e.g.„SAIL“ for sailing mode.

GYRO

1


F1 DISPLAY DATA

F2 MANUAL SETTINGS

F3 SETUP MENU

246.8Sperry Marine

NAVIGAT 3000


In case of re-alignment of thesystem the heading display ofthe fiber-optic sensor shows„dashes“ (no data available)and“INIT PHASE/PLEASE WAIT” inthe menu windowbefore starting with SYSTEMALIGN and continuing with thealignment as described above.

GYRO

1

NAVIGAT 3000

FIBER OPTIC GYROCOMPASS

INIT PHASE

PLEASE WAIT


NAVIGAT 3000


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pí~êíìéL^äáÖå mêçÅÉÇìêÉ OJT

léÉê~íáåÖ jçÇÉ fåÇáÅ~íáçåë

For the indication of the currently active operating mode of theNAVIGAT 3000 system, three different operating mode indications exist:

„SAIL“:The SAILING MODE, as theoperational mode of a navigat-ing vessel, is indicated.

„STAT“:The STATIONARY MODE, as theoperational mode of a vesseloperating under dynamic posi-tioning (DP) conditions in a fixedposition, is indicated.

„RA“:

The REDUCED ACCURACYMODE is indicated only in caseof a reduced accuracy conditionof the NAVIGAT 3000 sensorwith the vessel in SAILINGMODE as previous operationalmode.


F1 DISPLAY DATA

F2 MANUAL SETTINGS

F3 SETUP MENU

STAT MAIN MENU GYRO 1

F1 DISPLAY DATA

F2 MANUAL SETTINGS

F3 SETUP MENU

RA MAIN MENU GYRO 1

F1 DISPLAY DATAF2 MANUAL SETTINGS

F3 SETUP MENU

kçíÉ The REDUCED ACCURACY MODE can ONLY be indicated with the pre-condition of the vessel in SAILING MODE as previous operational mode,to highlight an occurring reduced accuracy condition of theNAVIGAT 3000 sensor.

With the vessel in STATIONARY MODE as pre-condition, theREDUCED ACCURACY MODE can NOT be indicated.



kçíÉ The STATIONARY MODE is ONLY available as operational mode if spe-

cifically preset by factory for a vessel designed to operate under dynamicpositioning (DP) conditions in a fixed position and MUST ALWAYS beselected when the vessel is operating under DP conditions.


kçíÉ In case the STATIONARY MODE as operational mode is necessary for avessel designed to operate under dynamic positioning (DP) conditions ina fixed position, but NOT PRESET by factory contact the

Sperry Marine Service for advice.


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OJU pí~êíìéL^äáÖå mêçÅÉÇìêÉ

^äáÖåãÉåí `çåÇáíáçåë

During the alignment process attitude, heading and moving conditionswill be determined. The length of alignment process is influenced by thecurrent conditions of the vessel and whether GPS position and GPSspeed data are available.

pí~íáÅ ^äáÖåãÉåí `çåÇáíáçåë

In case of a static alignment, the alignment will be complete after a min-imum of 5 to 7 minutes up to a maximum of 10 minutes.

aóå~ãáÅ ^äáÖåãÉåí `çåÇáíáçåë

In case of alignment at sea, the alignment will be complete after a maxi-mum of 10 minutes under typical conditions at sea and after up to 30minutes max. under hindered conditions at sea.

In case of an alignment at sea and currently no GPS position and noGPS speed data available, caused by blackout or breakdown of equip-ment, the sensor will NOT be able to continue and finalize the alignmentbefore the GPS data are again available, see “Sailing Mode underDynamic Conditions: No GPS Data” on page 2-11 for details.

tôkfkd iáãáíÉÇ Ç~í~ ~ÅÅìê~Åó ÇìêáåÖ ~äáÖåãÉåí

^ÑíÉê ~ ÅçäÇ ëí~êíI íÜÉ k^sfd^q PMMM êÉèìáêÉë ~ ÅçãéäÉíÉ ~äáÖåãÉåí

íáãÉ ~í ëÉ~ çÑ ìé íç PM ãáåìíÉë ÄÉÑçêÉ êÉäá~ÄäÉ ÜÉ~ÇáåÖ Ç~í~ áë ~î~áä~ÄäÉK

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mçïÉê Ççïå íÜÉ ëóëíÉã ÇìêáåÖ äçåÖ ÇçÅâáåÖ éÉêáçÇë çåäóK

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ìëáåÖ áíë ÜÉ~ÇáåÖ ~ë íÜÉ êÉÑÉêÉåÅÉ Ñçê ÜÉ~ÇáåÖ Åçåíêçä ëóëíÉãëI oâôI

bàfpI ÉíÅK

^ ã~ÖåÉíáÅ Åçãé~ëë ÜÉ~ÇáåÖ ëçìêÅÉ ëÜçìäÇ ÄÉ ëÉäÉÅíÉÇ ~ë êÉÑÉêÉåÅÉ

çåäó áå Å~ëÉ çÑ Ñ~áäìêÉ çÑ íÜÉ ÖóêçÅçãé~ëëEÉëFK

`^rqflk Risk of erroneous operation condition through inaccurate alignmentA successful alignment is essential for the error-free operation of theNAVIGAT 3000.The system will immediately recognize if sensor measurements or exter-nal data inputs fall outside the permitted ranges. However, inaccurate orfalse data inputs (speed and/or position) within the permitte

Documents

Navigat 3000 operational manual.pdf