Meinberg GPS167TGP User manual

Technical Information
Operating Instructions
GPS167TGP
- AP336.505

Impressum
Meinberg Funkuhren GmbH & Co. KG
Auf der Landwehr 22
D-31812 Bad Pyrmont
Phone: [phone] / 9309-0
Fax: [phone] / 9309-30
Internet: http://www.meinberg.de
Email: [email protected]
May 05, 2006

Table of Contents
Impressum ............................................................................................ 2
General Information ............................................................................. 7
The Modular System GPS167TGP ...................................................... 8
GPS167 Features .................................................................................. 9
Time Zone and Daylight Saving............................................... 10
Pulse and Frequency Outputs ................................................... 10
Time Capture Inputs ................................................................. 11
Asynchronous Serial Ports (optional 4x COM)........................ 11
DCF77 Emulation ..................................................................... 12
Programmable pulse (optional) ................................................ 13
Timecode outputs (optional)..................................................... 13
Abstract ........................................................................... 13
Installation .......................................................................................... 14
Power Supply ............................................................................ 14
Mounting the Antenna .............................................................. 14
Antenna Short-Circuit .............................................................. 15
Assembly with CN-UB/E (optional) ........................................ 16
Powering Up the System .......................................................... 17
The Front Panel Layout ..................................................................... 18
FAIL LED ................................................................................ 18
LOCK LED .............................................................................. 18
LC Display ................................................................................ 18
MENU Key ............................................................................... 18
CLR/ACK Key ......................................................................... 18
NEXT Key ................................................................................ 19
INC Key .................................................................................... 19

The Menus in Detail ........................................................................... 19
Root Menu ................................................................................ 19
Menu RECEIVER POS. ........................................................... 21
Menu SV CONSTELLATION ................................................. 21
Menu SV POSITION ............................................................... 22
Menu USER CAPTURE .......................................................... 22
Menu SETUP............................................................................ 22
SETUP FREQUENCY OUTPUT................................... 23
SETUP ENABLE OUTPUTS ........................................ 23
SETUP TIME ZONE ...................................................... 24
SETUP DAYLIGHT SAV ON/OFF .............................. 24
SETUP SERIAL PORT PARM ...................................... 25
SETUP SERIAL STRING TYPE ................................... 26
SETUP SERIAL STRING MODE ................................. 26
SETUP POUT X (optional) ............................................ 27
Mode ...................................................................... 27
Timer mode ............................................................ 27
Single Pulse ........................................................... 28
Cyclic mode ........................................................... 28
PPS, PPM, PPH Modes ......................................... 28
Menu Quick Reference for progr. Pulse ................ 29
SETUP IRIG SETTINGS (optional) .............................. 30
SETUP INITIAL POSITION ......................................... 30
SETUP INITIAL TIME .................................................. 31
INIT USER PARMS ....................................................... 31
INIT GPS PARMS .......................................................... 31
FORCE BOOT MODE ................................................... 32
ANTENNA CABLE ....................................................... 32
Resetting Factory Defaults ................................................................. 33

Firmware Updates .............................................................................. 33
Skilled/Service-Personnel only: Replacing the Lithium Battery ....... 34
CE Label ............................................................................................ 34
Technical Specifications GPS167 ...................................................... 35
Oscillator specifications............................................................ 37
Technical Specifications GPS167 Antenna .............................. 38
Time Strings ............................................................................. 39
Format of the Meinberg Standard Time String ............... 39
Format of the Meinberg Capture String .......................... 40
Format of the SAT Time String ...................................... 41
Format of the Uni Erlangen String (NTP) ...................... 42
Format of the NMEA 0183 String (RMC) ...................... 44
Format of the ABB SPA Time String ............................. 45
Format of the Computime Time String........................... 46
Timecode (optional) ................................................................. 47
Principle of Operation ..................................................... 47
Block Diagram Timecode ............................................... 47
IRIG Standard Format ..................................................... 48
AFNOR Standard Format ............................................... 49
Assignment of CF Segment in IEEE1344 mode............. 50
Generated Timecodes ...................................................... 51
Selection of Generated Time Code ........................ 52
Outputs ............................................................................ 52
AM Sine Wave Output ........................................... 52
PWM DC Outputs .................................................. 52
Technical Data ................................................................ 53
Signal Description GPS167 V7.x ............................................. 54
Rear Connector Pin Assignments GPS167 V7.x ...................... 55
Menu Quick Reference GPS167 ........................................................ 56

6
Technical appendix ............................................................................ 57
Technical Specifications GPS167TGP .............................................. 58
Rear Panel Connectors.............................................................. 58
CE Label ................................................................................... 58
Rear panel view GPS167TGP .................................................. 59
SUB-D Connector Assignments ............................................... 60
Connector Assignment Error Relais (Time Sync) .................... 60
Technical Specifications Power Supply Unit PULS AP336.505 ...... 61
Front Panel and Rear Connector Pin Assignments................... 61

7
General Information
The satellite receiver clock GPS167 has been designed to provide extremly precise
time to its user. The clock has been developed for applications where conventional
radio controlled clocks can´t meet the growing requirements in precision. High
precision available 24 hours a day around the whole world is the main feature of the
new system which receives its information from the satellites of the Global Posi-
tioning System.
The Global Positioning System (GPS) is a satellite-based radio-positioning, naviga-
tion, and time-transfer system. It was installed by the United States Departement of
Defense and provides two levels of accuracy: The Standard Positioning Service (SPS)
and the Precise Positioning Service (PPS). While PPS is encrypted and only available
for authorized (military) users, SPS has been made available to the general public.
GPS is based on accurately measuring the propagation time of signals transmitted
from satellites to the user´s receiver. A nominal constellation of 21 satellites together
with several active spares in six orbital planes 20000 km over ground provides a
minimum of four satellites to be in view 24 hours a day at every point of the globe.
Four satellites need to be received simultaneously if both receiver position (x, y, z)
and receiver clock offset from GPS system time must be computed. All the satellites
are monitored by control stations which determine the exact orbit parameters as well
as the clock offset of the satellites´ on-board atomic clocks. These parameters are
uploaded to the satellites and become part of a navigation message which is retrans-
mitted by the satellites in order to pass that information to the user´s receiver.
The high precision orbit parameters of a satellite are called ephemeris parameters
whereas a reduced precision subset of the ephemeris parameters is called a satellite´s
almanac. While ephemeris parameters must be evaluated to compute the receiver´s
position and clock offset, almanac parameters are used to check which satellites are in
view from a given receiver position at a given time. Each satellite transmits its own set
of ephemeris parameters and almanac parameters of all existing satellites.
7

8
The Modular System GPS167TGP
GPS167TGP is a set of equipment composed of a satellite controlled clock GPS167
together with a power supply unit PULS AP336.505, both installed in a metal desktop
case and ready to operate. The interfaces provided by GPS167 are accessible via
connectors in the rear panel of the case. Details of the components are described
below.
NEXT INC
CLR
ACK
MENU
FAI L LOC K
GPS167 assembled in desktop case (front view)

9
GPS167 Features
The hardware of GPS167 is a 100mm x 160mm microprocessor board. The 105mm
wide front panel integrates a 4 x 16 character LC display, two LED indicators and 4
push buttons. The receiver is connected to the antenna/converter unit by a 50 ohm
coaxial cable (refer to "Mounting the Antenna"). Feeding the antenna/converter oc-
curs DC insulated via the antenna cable. Optional an antenna splitter for up to four
receivers connected to one antenna is available.
GPS167 is using the "Standard Positioning Service" SPS. The navigation message
coming in from the satellites is decoded by GPS167´s microprocessor in order to track
the GPS system time. Compensation of the RF signal´s propagation delay is done by
automatical determination of the receiver´s position on the globe. A correction value
computed from the satellites´ navigation messages increases the accuracy of the
board´s oven controlled master oscillator (OCXO) and automatically compensates the
OCXO´s aging. The last recent value is restored from the battery buffered memory at
power-up.
The GPS167 provides different optional outputs, i.e. three progammable pulse
outputs, modulated/unmodulated timecode output, and up to a total of four RS232
COM ports. Additionally, you can order the GPS167 with different OCXOs (e.g.
OCXO-LQ / MQ / HQ or an external Rubidium) to match the required accuracy.
The hard- and software configuration of the clock is dis-
played if the NEXT key is pressed two times from the root
menu.

10
Time Zone and Daylight Saving
GPS system time differs from the universal time scale UTC (Universal Time Coordi-
nated) by the number of leap seconds which have been inserted into the UTC time
scale after GPS has been initiated in 1980. The current number of leap seconds is part
of the navigation message supplied by the satellites, so GPS167´s internal real time is
based on UTC. Conversion to local time including handling of daylight saving year by
year can be done by the receiver´s microprocessor if the corresponding parameters are
set up by the user.
Pulse and Frequency Outputs
The pulse generator of GPS167 generates pulses once per second (P_SEC) and once
per minute (P_MIN). Additionally, master frequencies of 10 MHz, 1 MHz and 100
kHz are derived from the OCXO. All the pulses are available with TTL level at the
rear connector. The included synthesizer generates a frequency from 1/8 Hz up to 10
MHz synchronous to the internal timing frame. The phase of this output can be shifted
from -360° to +360° for frequencies less than 10 kHz. Both frequency and phase can
be setup from the front panel or using the serial port COM0. Synthesizer output is
available at the rear connector as sine-wave output (F_SYNTH_SIN), with TTL level
(F_SYNTH) and via an open drain output (F_SYNTH_OD). The open drain output
can be used to drive an optocoupler when a low frequency is generated.
In the default mode of operation, pulse outputs and the synthesizer output are
disabled until the receiver has synchronized after power-up. However, the system can
be configured to enable those outputs immediately after power-up. An additional TTL
output (TIME_SYN) reflects the state of synchronization. This output switches to
TTL HIGH level when synchronization has been achieved and returns to TTL LOW
level if not a single satellite can be received or the receiver is forced to another mode
of operation by the user.

11
Time Capture Inputs
Two time capture inputs called User Capture 0 and 1 are provided at the rear connector
(CAP0 and CAP1) to measure asynchronous time events. A falling TTL slope at one
of these inputs lets the microprocessor save the current real time in its capture buffer.
From the buffer, capture events are transmitted via COM0 or COM1 and displayed on
LCD. The capture buffer can hold more than 500 events, so either a burst of events
with intervals down to less than 1.5 msec can be recorded or a continuous stream of
events at a lower rate depending on the transmission speed of COM0 or COM1 can be
measured. The format of the output string is ASCII, see the technical specifications at
the end of this document for details. If the capture buffer is full a message "** capture
buffer full" is transmitted, if the interval between two captures is too short the warning
"** capture overrun" is being sent.
Asynchronous Serial Ports (optional 4x COM)
Four asynchronous serial RS232 interfaces (COM0 ... COM3) are available to the
user. In the default mode of operation, the serial outputs are disabled until the receiver
has synchronized after power-up. However, the system can be configured to enable
those outputs immediately after power-up. Transmission speeds, framings and mode
of operation can be configured separately using the setup menu. COM0 is compatible
with other radio remote clocks made by Meinberg. It sends the time string either once
per second, once per minute or on request with ASCII ´?´ only. Also the interfaces can
be configured to transmit capture data either automatically when available or on
request. The format of the output strings is ASCII, see the technical specifications at
the end of this document for details. A separate document with programming instruc-
tions can be requested defining a binary data format which can be used to exchange
parameters with GPS167 via COM0.

12
DCF77 Emulation
The GPS167 satellite controlled clock generates TTL level time marks (active HIGH)
which are compatible with the time marks spread by the German long wave transmit-
ter DCF77. This long wave transmitter installed in Mainflingen near Frankfurt/
Germany transmits the reference time of the Federal Republic of Germany: time of
day, date of month and day of week in BCD coded second pulses. Once every minute
the complete time information is transmitted. However, GPS167 generates time marks
representing its local time as configured by the user, including announcement of
changes in daylight saving and announcement of leap seconds. The coding sheme is
given below:
M Start of Minute (0.1 s)
R RFTransmission via secondary antenna
A1 Announcement of a change in daylight saving
Z1, Z2 Time zone identification
Z1, Z2 = 0, 1: Daylight saving disabled
Z1, Z2 = 1, 0: Daylight saving enabled
A2 Announcement of a leap second
S Start oftime code information
P1, P2, P3 Even parity bits
0
10
20
30
40
50
R
M
1
4
2
1
20
10
8
4
2
1
P2
20
10
8
4
2
1
2
4
8
10
1
2
4
8
10
20
40
80
P3
A1
Z1
Z2
A2
S
1
2
4
8
10
20
40
P1
Minute
(reserved)
Hour
Day of Month
Day of Week
Year of the Century
Month of Year
Time marks start at the beginning of new second. If a binary "0" is to be transmitted,
the length of the corresponding time mark is 100 msec, if a binary "1" is transmitted,
the time mark has a length of 200 msec. The information on the current date and time
as well as some parity and status bits can be decoded from the time marks of the 15th
up to the 58th second every minute. The absence of any time mark at the 59th second
of a minute signals that a new minute will begin with the next time mark. The DCF
emulation output is enabled immediately after power-up.

13
Programmable pulse (optional)
At the male connector Typ VG64 there are three programmable TTL outputs (Prog
Pulse 0-2), which are arbitrarily programmable.
Other technical details are described at the end of this manual.
Timecode outputs (optional)
Abstract
The transmission of coded timing signals began to take on widespread importance
in the early 1950´s. Especially the US missile and space programs were the forces
behind the development of these time codes, which were used for the correlation of
data. The definition of time code formats was completely arbitrary and left to the
individual ideas of each design engineer. Hundreds of different time codes were
formed, some of which were standardized by the "Inter Range Instrumentation Group"
(IRIG) in the early 60´s.
Except these "IRIG Time Codes", other formats like NASA36, XR3 or 2137 are still
in use. The board GPS167 however generates the IRIG-B, AFNOR NFS 87-500 code
as well as IEEE1344 code which is an IRIG-B123 coded extended by information for
time zone, leap second and date. Other formats may be available on request.
At the male connector Typ VG64 there are also IRIG-B modulated (3Vpp into 50
Ohm) and IRIG-B unmodulated DC level shift.

14
Installation
Power Supply
The power supply used GPS167TGP see "Technical Appendix" at the end of this
manual.
Mounting the Antenna
The GPS satellites are not stationary but circle round the globe in a period of about 12
hours. They can only be received if no building is in the line-of-sight from the antenna
to the satellite, so the antenna/converter unit must be installed in a location from which
as much of the sky as possible can be seen. The best reception is given when the
antenna has a free view of 8° angular elevation above horizon. If this is not possible
the antenna should be installed with a mostly free view to the equator because of the
satellite courses which are located between latitudes of 55° North and 55° South. If
even this is not possible problems occure especially when at least four sattelites for
positioning have to be found.
The antenna/converter unit can be mounted on a pole with a diameter up to 60 mm
or at a wall. A 50cm plastic tube, two holders for wall-mounting and clamps for pole-
mounting are added to every GPS167. A standard coaxial cable with 50 ohms
impedance should be used to connect the antenna/converter unit to the receiver. The
maximum lenght of cable between antenna and receiver depends on the attenuation
factor of the used coaxial cable.
Example:
Type of cable diameter
Ø [mm]
Attenuation at 100MHz
[dB]/100m
max. lenght
[m]
RG58/CU 5mm 15.9 300 1
RG213 10.5mm 6.9 700 1
1)This specifications are made for antenna/converter units produced after January, 2005
The values are typically ones; the exact ones are to find out from the data sheet of the
used cable.
Up to four GPS167 receivers can be run with one antenna/converter unit by using the
optional antenna diplexer. The total length of one antenna line between antenna,
diplexer and receiver must not be longer than the max. lenght shown in the table
above. The position of the diplexer in the antenna line does not matter.
When installing the high voltage protector CN-UB/E (CN-UB-280DC) be aware to set
it directly after reaching indoor. The CN-UB/E is not for outdoor usage.

15
Antenna Short-Circuit
In case of an antenna line short-circuit the following message appears in the display:
If this message appears the clock has to be disconnected from the mains and the defect
is to eliminate. After that the clock can be powered-up again. The antenna supply
voltage must be in a range of 18.5VDC (free) and 16VDC (connected GPS antenna).

16
Assembly with CN-UB/E (optional)
Optional the overvoltage protector CN-UB/E is available. Standard you connect the
antenna converter directly with the antenna cable to the system.
Type N / BNC
male
Type N
male
Type N
male
CN-UB/E
1.5m max.
Type N
male
GPS167
Antenna
Meinberg
GPS
As short as possible!

17
Powering Up the System
If both the antenna and the power supply have been connected the system is ready to
operate. About 10 seconds after power-up the receiver´s (OCXO-LQ) until 3 minutes
(OCXO-MQ / HQ) has warmed up and operates with the required accuracy. If the
receiver finds valid almanac and ephemeris data in its battery buffered memory and
the receiver´s position has not changed significantly since its last operation the
receiver can find out which satellites are in view now. Only a single satellite needs to
be received to synchronize and generate output pulses, so synchronization can be
achieved maximally one minute after power-up (OCXO-LQ) until 10 minutes
(OCXO-MQ / HQ) . After 20 minutes of operation the OCXO is full adjusted and the
generated frequencies are within the spezified tolerances.
If the receiver position has changed by some hundred kilometers since last operati-
on, the satellites´ real elevation and doppler might not match those values expected by
the receiver thus forcing the receiver to start scanning for satellites. This mode is
called Warm Boot because the receiver can obtain ID numbers of existing satellites
from the valid almanac. When the receiver has found four satellites in view it can
update its new position and switch to Normal Operation. If the almanac has been lost
because the battery had been disconnected the receiver has to scan for a satellite and
read in the current almanacs. This mode is called Cold Boot. It takes 12 minutes until
the new almanac is complete and the system switches to Warm Boot mode scanning
for other satellites.
In the default mode of operation, neither pulse and synthesizer outputs nor the serial
ports will be enabled after power-up until synchronization has been achieved. Howe-
ver, it is possible to configure some or all of those outputs to be enabled immediately
after power-up. If the system starts up in a new environment (e. g. receiver position
has changed or new power supply) it can take some minutes until the OCXO´s output
frequency has been adjusted. Up to that time accuracy of frequency drops to 10-8
reducing the accuracy of pulses to ±5µs.

18
The Front Panel Layout
FAIL LED
The FAIL LED is turned on whenever the
TIME_SYN output is low (receiver is not syn-
chronized).
LOCK LED
The LOCK LED is turned on when after power-
up the receiver has acquired at least four satelli-
tes and has computed its position. In normal
operation the receiver position is updated conti-
nuously as long as at least four satellites can be
received.
LC Display
The 4 x 16 character LC display is used to show the receiver´s status and let the user
edit parameters. The keys described below let the user select the desired menu. The
next chapter lists all available menus in detail. A quick reference of the available
menus and submenus can be found at the end of this document.
MENU Key
This key lets the user step through several display menus showing specific data.
CLR/ACK Key
This key has to be used when parameters are to be modified. When this key is pressed
the parameters that have been edited are saved in the battery buffered memory. If the
menu is left without pressing CLR/ACK all changes are discarded.
NEXT INC
CLR
ACK
MENU
FA I L L O C K

19
NEXT Key
When editing parameters (LCD cursor is visible) this key moves the cursor to the next
digit rsp. to the next parameter to be edited. If the current menu just displays data
(cursor not visible) pressing this key switches to a submenu (if available).
INC Key
When editing parameters this key increments the digit or letter at the cursor position.
The Menus in Detail
Root Menu
The root menu is shown when the receiver has completed initialization after power-
up. The first line of the display shows the receiver´s mode of operation as described
above. The text "NORMAL OPERATION" might be replaced by "COLD BOOT",
"WARM BOOT", "UPDATE ALMANAC". If the antenna is disconnected or not
working properly, the text "ANTENNA FAULTY" is displayed instead.
The next two lines display the current date, the name of the time zone (as defined in
the setup menu) and local time. The last line shows the state of the synthesizer. It
might look like following:
"Synth disabled" Synthesizer is disabled (frequency setted on 0.000)
"F.synth inhibited" GPS167 is not synchronized jet, but the synthesizer will be en-
abled after synchronisation.
"..............(free)" The frequency is generated, but the phase is not synchronous
to the pulse output P_SEC, either because the synthesizer is
enabled although GPS167 has not synchronosized jet or be
cause the frequency is setted to more than 10kHz.
"..............(drft)" The frequency is generated and the phase was already syn-
chronous to the pulse output P_SEC, but in the moment the
phase can´t be controlled or adjusted because no satellite is
received now.

20
If the NEXT key is pressed one time from the root menu a submenu is displayed
showing the receiver´s software revision:
If the NEXT key is pressed for second time a submenu is displayed showing other
receiver´s infos
Meaning of the abbreviations and adjusted standard value:
"PROUT: 0" programmable pulse
standard: 0 (not available)
optional: 3 (until three prog. pulse)
"NCOM: 2" serial interface
standard: 2 (COM0 and COM1)
optional: 4 (COM0 - 3)
"SYNTH: variable" frequency synthesizer
standard: available
optional: N/A (only TCXO)
"OCXO_LQ" used oscillator (see Oscillatorspecifikations)
"GPS167_i" EPLD Version