FURUNO Multi-GNSS Disciplined Oscillator

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Transcription:

FURUNO Multi- Disciplined Oscillator Models GF-8701, GF-8702, GF-8703, GF-8704, GF-8705 (Document No. ) www.furuno.com

IMPORTANT NOTICE No part of this manual may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopying and recording, for any purpose without the express written permission of the publisher, FURUNO ELECTRIC CO., LTD. FURUNO ELECTRIC CO., LTD. All rights reserved. FURUNO ELECTRIC CO., LTD. reserves the right to make changes to its products and specifications without notice. All brand and product names are registered trademarks, trademarks or service marks of their respective holders. The following satellite systems are operated and controlled by the authorities of each government. - GPS(USA) - GLONASS (Russia) - Galileo(Europe) - QZSS(Japan) - SBAS(USA: WAAS, Europe: EGNOS, Japan: MSAS) FURUNO is not liable for any degradation while using these satellite systems. FURUNO cannot guarantee specifications if any of these systems experience degradation. Based on these conditions the user is expected to be familiar with these systems and is fully responsible for their use.

Revision History Version Changed contents Date 0 Initial release 2017.03.08

Table of Contents 1 Outline 1 2 General Functional Block Level Diagram 1 3 General Performance Data 2 3.1 PPS 2 3.2 VCLK 3 3.3 VCLK_SIN 6 4 General Time Sequence 7 4.1 Parameter Input Sequence 7 4.2 Normal Operation 7 4.2.1 Initial Power ON Sequence 8 4.2.2 Hardware External Reset Sequence 8 4.2.3 Software Reset Sequence 9 4.2.4 Holdover Sequence 9 4.2.5 Out of Holdover Sequence 10 5 Holdover Operation with HOSET 11 6 Phase Skip Operation with PHASESKIP and MODESET 14 7 Measurement Configuration Using 53132A 15 8 Antenna Configuration 18

1 Outline This document describes the essential information for achieving proper operation and performance of the following FURUNO Multi- Disciplined Oscillator (DO) solutions. It is a guide for user development, design, manufacturing and quality control. Products: GF-870x series (GF-8701, GF-8702, GF-8703, GF-8704 and GF-8705) 2 General Functional Block Level Diagram This chapter describes main functions of the DO. Figure 2.1 shows an example block level diagram of the DO. The DO has the following two kinds of PPS; - Reference PPS: This PPS is synchronized with UTC using the receiver or with an external 1Hz signal (EPPS). - Local PPS: This PPS is a signal divided from 10MHz which is controlled by PLL. The DO operates the adaptive feedback control with two PPS signals as an output PPS source. The DO is able to achieve a high precision holdover by means of the adaptive control regarding voltage of Oscillator. Antenna EPPS Receiver PPS Reference PPS Local PPS Phase Detector Voltage Control Control voltage Oscillator 1) 10MHz BPF VCLK_SIN 2) 1/10MHz VCLK 1PPS Figure 2.1 GF-870x General Block Level Diagram Notes: 1) GF-8701:VTCXO, GF-8702/03/04/05: OCXO 2) GF-8701, GF-8702 and GF-8703 do not support VCLK_SIN. 1

3 General Performance Data GF-870x This chapter describes each signal of the specification and typical test data values in order to check the consistency between the product specifications and customer requirement specifications. 3.1 PPS Table 3.1 shows the specifications and the actual values of PPS at Holdover. Specifications item Time precision Time accuracy -: Not Applicable Table 3.1 PPS Performance Specifications and Test Data GF-870x series Receiver Holdover Status condition Unit 8701 8702 8703 8704 8705 Fine Lock - ns ±15 (at 1σ) Holdover - - - Fine Lock - ns ±100 ±50 24 hours guaranteed Holdover time us - ±50 ±10 ±5 ±1.5 ±10us 16 - - - ±5us 8 16 - - Holdover ±1.5us 2 4 8 - test data 3) hour - ±1.1us 1 3 6 18 ±400ns - 1 2 6 ±100ns - - - 2 Environment Condition Refer to Condition in Table 7.1 and Table 7.2 at Hardware Specifications. Notes: 3) This Holdover time data is not guaranteed in Holdover time specifications because it is based on internal Holdover test estimations. 2

3.2 VCLK Table 3.2 shows an overview of VCLK specifications. There is no definition of frequency precision because the short term stability of VCLK defines the same stability specifications noted in this table. The phase noise of 10MHz at GF-8701/02/03 is actual value test data. Therefore there is no description of this value in hardware specifications. User can check the performance using test data in Figure 3.1, Figure 3.2 and Figure 3.3. The phase noise of 10MHz at GF-8704 and GF-8705 is described as performance specifications in the hardware specifications. To guarantee the performance specification, the phase noise exceeding 10kHz is specified the same as 1kHz (-140dBc/Hz). However the actual value of phase noise exceeding 10kHz is better than 1kHz. User can check the performance using test data in Figure 3.4. Specifications item Long term stability Root Allan deviation τ=1sec Frequency accuracy 10MHz Phase noise Accumulating phase noise -: Not Applicable 1Hz 10Hz 100Hz 1kHz >10kHz 1Hz 10Hz 100Hz 1kHz >10kHz 10 to 10kHz Table 3.2 VCLK Performance Specifications GF-870x series Receiver Status Unit 8701 8702 8703 8704 8705 Fine Lock - ±1E-11 ±1E-12 (Max) (Max) Holdover - - Fine Lock 1E-9 2E-10 1E-10 - Holdover (Max) (Max) (Max) Fine Lock N/A - Holdover - ±3E-9 ±1E-9-70 -75-85 -85 (Typ) (Typ) (Typ) (Max) -100-106 -110-120 (Typ) (Typ) (Typ) (Max) Fine Lock -122-134 -135-130 (Typ) (Typ) (Typ) (Max) -141-146 -148-140 (Typ) (Typ) (Typ) (Max) -148-149 -155-140 dbc/hz (Typ) (Typ) (Typ) (Max) -70-75 -85-85 (Typ) (Typ) (Typ) (Max) -100-106 -110-120 (Typ) (Typ) (Typ) (Max) Holdover -122-134 -135-130 (Typ) (Typ) (Typ) (Max) -141-146 -148-140 (Typ) (Typ) (Typ) (Max) -148-149 -155-140 (Typ) (Typ) (Typ) (Max) Fine Lock - - - -95 dbc Holdover - - - (Max) Environment Condition Refer to Condition in Table 7.1 and Table 7.2 at Hardware Specifications. 3

10 100 1K 10K 100K GF-8701 Figure 3.1 VCLK Phase Noise Data (GF-8701) Figure 3.2 VCLK Phase Noise Data (GF-8702) 4

Figure 3.3 VCLK Phase Noise Data (GF-8703) 10 100 1K 10K 100K Figure 3.4 VCLK Phase Noise Data (GF-8704, GF-8705) 5

3.3 VCLK_SIN Table 3.3 shows an overview of VCLK_SIN specifications. There is no single definition of frequency precision. The overall short term stability specifications of VCLK_SIN are defined in Table 3.3. To guarantee the performance specification, the phase noise exceeding 10kHz is specified the same as 1kHz (-140dBc/Hz). However the actual value of phase noise exceeding 10kHz is better than 1kHz. User can check the performance using test data in Figure 3.5. Table 3.3 VCLK_SIN Performance Specifications GF-870x series Specifications item Receiver Status Unit 8704 8705 Long term stability Fine Lock - ±1E-12 (Max) Holdover - - Root Allan deviation Fine Lock τ=1sec Holdover - 1E-10 (Max) Frequency accuracy Fine Lock N/A - Holdover ±1E-9 1Hz -85 (Max) 10Hz -120 (Max) 100Hz Fine Lock -130 (Max) 1kHz -140 (Max) 10MHz >10kHz -140 (Max) dbc/hz Phase noise 1Hz -90 (Max) 10Hz -120 (Max) 100Hz Holdover -130 (Max) 1kHz -140 (Max) >10kHz -140 (Max) Accumulating 10 to Fine Lock phase noise 10kHz Holdover dbc -95 (Max) -: Not Applicable Environment Condition Refer to Condition in Table 7.1 and Table 7.2 at Hardware Specifications. 10 100 1K 10K 100K Figure 3.5 VCLK_SIN Phase Noise Data (GF-8704, GF-8705) 6

4 General Time Sequence GF-870x This chapter describes the general transition time chart and the main behavior of external event trigger. 4.1 Parameter Input Sequence Figure 4.1 shows an overall response time using a command from the host side. T SET_INTVL Host processor status Send 1 st parameter Send 2 nd parameter T SET_DLY GF status Default status 1 st parameter status 2 nd parameter status Figure 4.1 Parameter Input Sequence Table 4.1 Parameter Input Sequence Symbol Description Unit Min Typ Max T SET_DLY T SET_INTVL The response time after the host command is transmitted until the command is accepted by the internal operation. The waiting time of the next command transmission after the previous command is sent. second - - 2 second - - 0 4.2 Normal Operation This section describes the relationship between the receiver status and the frequency mode without EPPS in a normal operation sequence. DO has the following two kinds of the relationship between the PPS reference status and the frequency mode based on the time difference between UTC decoding and Coarse Lock processing. Case 1: Coarse Lock processing time is faster than UTC decoding time. The frequency mode changes to Coarse Lock by synchronizing with GPS. Case 2: UTC decoding time is faster than Coarse Lock processing time. The frequency mode changes to Coarse Lock by synchronizing with UTC. In this section, Case 1 is applied as normal time sequence. 7

4.2.1 Initial Power ON Sequence Figure 4.2 shows the process time from completing Warm Up and position fixed after power on and until Fine Lock are achieved. VCC/VBK status Acquisition/ Tracking Position fixed PPS reference source Free running GPS UTC(USNO) Frequency mode Warm Up Pull-In Coarse Lock Fine Lock T WU_ FL(VCC) Figure 4.2 Initial Power ON Sequence Table 4.2 Initial Power ON Sequence Symbol Description Condition Unit Min Typ Max The process time from position fixed until Fine Lock is achieved Power on sequence minute - - 5 T WU_FL(VCC) 4.2.2 Hardware External Reset Sequence Figure 4.3 shows the process time from completing Warm Up and position fixed after an external hardware reset release and until Fine Lock is achieved. TRST RST_N status Position fixed Reset status Acquisition/ Tracking Position fixed PPS reference source UTC(USNO) Reset status Free running GPS UTC(USNO) Frequency mode Fine Lock Warm Up Pull-In Coarse Lock Fine Lock TWU_FL(HWRST) Figure 4.3 External Reset Sequence Table 4.3 External Reset Sequence Symbol Description Condition Unit Min Typ Max T WU_FL(HWRST) The process time from releasing external hardware reset until Fine Lock External reset sequence by RST_N. Not dependent on reset time(t RST ) minute - - 5 8

4.2.3 Software Reset Sequence Figure 4.4 shows the process time from completing Warm Up and position fixed after executing RESTART command and until Fine Lock is achieved. RXD RESTART status Position fixed Acquisition/ Tracking Position fixed PPS reference source UTC(USNO) Free running GPS UTC(USNO) Frequency mode Fine Lock Warm Up Pull-In Coarse Lock Fine Lock T WU_ FL(SWRST) Figure 4.4 Restart Sequence with Power ON Table 4.4 Restart Sequence with Power ON Symbol Description Condition Unit Min Typ Max T WU_FL(SWRST) The process time from releasing external software reset until Fine Lock External reset sequence by RESTART command minute - - 5 4.2.4 Holdover Sequence Figure 4.5 shows the process time after Holdover executed, from reacquisition of position fixed until Fine Lock achieved. status Position fixed Position unfixed with zero SV Position fixed PPS reference source UTC(USNO) Free running GPS UTC(USNO) T FL_HO T PF_FL(HO) Frequency mode Fine Lock Holdover Coarse Lock Fine Lock Figure 4.5 Holdover Sequence Table 4.5 Holdover Sequence Symbol Description Condition Unit Min Typ Max T FL_HO The process time from Fine Lock until Holdover Position unfixed second - - 10 T PF_FL(HO) The process time from position fixed until final Fine Lock Holdover minute - - 5 9

4.2.5 Out of Holdover Sequence Figure 4.6 shows the process time after Out of Holdover executed, from reacquisition of position fixed until final Fine Lock. status Position unfixed with zero SV Position fixed PPS reference source Free running GPS UTC(USNO) T PF_FL(OHO) Frequency mode Holdover Out of Holdover Pull-In Coarse Lock Fine Lock Figure 4.6 Out of Holdover Sequence Table 4.6 Out of Holdover Sequence Symbol Description Condition Unit Min Typ Max The process time from position fixed until final Fine Lock Out of Holdover minute - - 5 T PF_CL(OHO) 10

5 Holdover Operation with HOSET GF-870x This chapter describes Holdover operation when using the HOSET command and CRZ (TPS4) status. - HOSET command: learning time set and available time set - CRZ (TPS4) status: learning time and available time Table 5.1 shows the relationship between the frequency mode and the learning time/available time. Table 5.1 Relationship between Frequency Mode and Control of Learning/Available Time frequency mode learning time available time Warm Up Set to 0 Holdover Set to 0 Coarse Lock 1 sec count down Fine Lock Refer to Figure 5.1 Out of Holdover 0 status 0 status Start LT=LTMax N Y Stop LT 1sec count up LT LTS0 Y N LT LTS1 N AT Set to ATS0 AT Set to ATS0 Y LT LTS2 N AT Set to ATS1 Y AT Set to ATS2 AT 1sec count down LT 1sec count up End Figure 5.1 Relationship between Learning Time and Available Time in Fine Lock State Here are the special messages in Figure 5.1. LT: Current Learning time count data LTMax: learning time set0 + 3600 LTS0: learning time set0 (HOSET Field 3) LTS1: learning time set1 (HOSET Field 5) LTS2: learning time set2 (HOSET Field 7) AT: Available time count data ATS0: available time set0 (HOSET Field 4) ATS1: available time set1 (HOSET Field 6) ATS2: available time set2 (HOSET Field 8) 11

Figure 5.2 shows an example based on the process of Table 5.1. The HOSET configuration is as follows: Configuration condition: HOSET LTS2=ATS2=0. There is no LTS2 and ATS2 operation. Frequency mode LT LTMax 4) Fixed FL Unfixed HO Fixed Unfixed Fixed X FL HO OHO X FL AT LTS0 5) LTS1 ATS0 ATS1 T0 T1 T2 T3 T4 T5 Figure 5.2 Relation of LT and AT to Frequency Mode t T0: Fine Lock is available 72 hours or more after power on of DO. T1: Holdover start time - Sets learning time to zero. Starts the available time count down. T2: Fine Lock start time - Starts learning time increment. Maintains available time count down. T3: Available time set time - Sets available time to available time set1 when the learning time equals learning time set1. T4: Available time set time - Sets available time to available time set0 when learning time equals learning time set0. T5: Out of Holdover start time - Starts Out of Holdover after available time reached zero. Notes: 4) Here are the special messages in Figure 5.2. FL: Fine Lock (frequency mode is 3) HO: Holdover (frequency mode is 4) OHO: Out of Holdover (frequency mode is 5) X: Pull-In or Coarse Lock (frequency mode is 1 or 2) 5) The decremental angle of available time is same as the incremental angle of learning time per unit of time. However in order to understand the behavior relationship between learning time and available time, both angles per unit of time are shown separately in this figure. The DO guarantees 24 hours Holdover performance by continuously learning time for a 72 hours period. To guarantee the performance specifications the default Holdover control parameters are as follows: -LTS0=72 hours -ATS0=24 hours -Others =0 If Holdover occurs before the learning time reaches the 72 hours default requirement, the frequency mode moves to Out of Holdover to avoid exceeding the 24 hours Holdover specification. If the user application does not require the 24 hours Holdover time specification, the user can control Holdover time using LTS1, LTS2, ATS1 and ATS2 to meet their specific requirement. Please ensure the operation parameters (except LTS0 and ATS0) meet the required Holdover specifications. It is the user s responsibility regarding the Holdover performance. Figure 5.3 shows two examples of Holdover operation. 12

Fixed FL Unfixed HO X Fixed FL Unfixed HO OHO X Fixed FL LTMax LTS0 ATS0 LTS1 LTS2 ATS1 ATS2 (a) T A Fixed FL Unfixed HO Fixed Unfixed Fixed X FL HO X FL LTMax LTS0 LTS1 ATS0 ATS1 LTS2 ATS2 T B Figure 5.3 Relation Default to Customization by LTS1 and ATS1 about Holdover Process Figure 5.3 (a) shows that the frequency mode moves to Out of Holdover at T A after elapse of 72 hour default learning time and 24 hour Holdover becomes available. Figure 5.3 (b) shows that the frequency mode does not move to Out of Holdover because the available time is set to ATS1 at T B and the learning time is set to LTS1.Therefore since ATS1 initiates the reduction of AT at Holdover start time, the frequency mode does not move to Out of Holdover when the frequency mode moves to Fine Lock within ATS1. (b) 13

6 Phase Skip Operation with PHASESKIP and MODESET GF-870x This chapter describes the relationship between PHASESKIP command and PPS behavior. Figure 6.1 shows the phase skip process at Pull-In mode is executed. Start Phase skip flag=1 N Y Phase skip control PPS timing error phase skip PPS timing N Set phase skip flag to 0 Y Set phase skip flag to 1 Normal control End Figure 6.1 Phase Skip Operation Flow with PHASESKIP The phase skip process is executed forcibly only when the frequency mode moves to Pull-In mode. If the user wants to execute the phase skip process again, the user should set the phase skip flag to 1. Figure 6.2 shows the phase skip process with the following internal operation when the frequency mode moved to Pull-In mode at T PI. The Local PPS has a PPS timing error with the number of N 10MHz against Reference PPS. By executing phase skip process, the Local PPS reaches 10MHz which is nearest Reference PPS after one second. Reference PPS 10MHz PPS timing error 1 N T PI PPS (Local PPS) T PI +1 Phase skip operation Figure 6.2 Relationship between Reference PPS and Local PPS with Phase Skip Process 14

7 Measurement Configuration Using 53132A GF-870x This chapter describes the measurement operations of PPS and VCLK using a 53132A (Keysight Technologies). Figure 7.1 shows a measurement environment for measuring the PPS accuracy based on the Time Interval Counter mode of 53132A. Figure 7.2 shows a measurement environment for measuring the VCLK precision based on the Frequency Ratio mode of 53132A. Both measurements use a GPS Disciplined Rubidium Oscillator as the Time Base. Antenna External power supply VCC Time Interval Counter GF-870x series Disciplined Oscillator PPS Ch1 3dB Divider Time Base 53132A ΔT GPS Disciplined Rubidium Oscillator PPS Ch2 External Reference 10MHz Figure 7.1 Measurement Environment of PPS Accuracy Antenna External power supply VCC Frequency Ratio GF-870x series Disciplined Oscillator VCLK Ch1 3dB Divider Time Base 53132A f GPS Disciplined Rubidium Oscillator Ch2 External Reference 10MHz Figure 7.2 Measurement Environment of VCLK Precision Figure 7.3 shows the simultaneously measurement data at room temperature of both PPS accuracy and VCLK precision at GF-8703 power on sequence. Figure 7.4 shows the Holdover characteristics after 72 hours learning time under 20 C dynamic temperature change condition of GF-8705 of which number of samples is ten. 15

nsec ppb GF-8703 1PPS accuracy GF-8703 VCLK accuracy(δf/f) Figure 7.3 Measurement Data of PPS and VCLK Accuracy for GF-8703 16

Fine Lock state Holdover state 0 6 12 18 24 24 hours holdover time Figure 7.4 Measurement Data of PPS Holdover Characteristics for GF-8705 17

8 Antenna Configuration This chapter describes the antenna interface function. Figure 8.1 shows the antenna configuration for the DO. The DO is able to stop over current condition with an internal threshold over current detection circuit. The antenna current shut down process triggers when the antenna detection circuit detects a shorted condition using a pre-determined current threshold. Figure 8.2 shows the antenna current status after shorted antenna condition has occurred. Antenna power supply voltage GF-8701/02/03:External GF-8704/05:Internal High-Side Switch IC Antenna Switch Controller Over current detector Antenna Open/Short detector RF_PIN is implemented on GF-8701/02/03 only RF signal from RF_PIN ANTSEL FORCE1L LNA1 RF signal from RF_COAX ANTSEL FORCE2 LNA2 Figure 8.1 Antenna Configuration Diagram I ANT (ma) 170 80 0 T1 T2 T3 Figure 8.2 Antenna Current Control Configuration at Short Mode t T1: Over current process works by detecting antenna short condition. T2: Antenna power supply voltage is shut down when circuit detects shorted condition of antenna. T3: Antenna power supply voltage recovers and available after antenna short removed. 18