DAGR - Defense Advanced GPS Receiver
© Brooke Clarke 2008 - 2009
Background
GPS Signals
Major Influences
DAGR (Polaris Guide)
GB-GRAM (Polaris Link)
Capabilities
Classical PVT
North Finding (Gun Laying System)
Target Location
Carrier Phase Data
Time
PLGR-II
Comparing PLGRII and DAGR
External Antenna Jacks
Polaris
Batteries
J4 External DC Power
Stock Turck PKG3
DAGR Specific
J1 & J2 D-Sub 15 Pin Connectors
Have Quick & 1 PPS J2 Cable
Mystery Cable
Shipping Container
Applications
Azimuth Determination
Zero Baseline Testing Single Receiver Method
Survey Equipment
Time Display
Operating Modes
Maps & Images
Mounting
Antenna
DC Power
Rockwell Patents
Pruchasing Polaris
Glossary
Links
Background
The first military use of the GPS system was around 1990 in the desert wars where the SLGR (
Trimpack) was used. It started out as a three channel L1 CA code (i.e. civilian) receiver. A few years later the
PLGR
was introduced. It's a 5 channel L1 receiver that can be used
with both the CA and P (when keyed) codes.
The diagrab below shows the evolution of the Rockwell GPS
receivers. I think the PLGR III was an experimental receiver that
was not fielded or if it was only in small numbers.
GPS Signals
I suspect that a Software Defined Radio type architecture is used.
This means that the DAGR/Polaris can receive the in development L1C,
L2C, L5 and M codes with just a firmware upgrade. Also there are a
number of GNSS signals that probably can also be received.
When the receiver is reprogrammed it probably will still have the same
number of channels but how they are allocated in frequency and code is
TBD.
Link Designation
|
Name
|
Freq (x10.23) MHz
|
Code
|
Reference
|
L1
|
Everybody
|
1575.42 (154)
|
C/A WAAS P(Y)
|
IS-GPS-200D |
L1C
|
Civilian
Quasi-Zenith Satellite System |
"
|
BOC(1,1) TMBOC CNAV-2 |
IS-GPS-800 |
L1M
|
Military |
"
|
M MNAV |
|
L2
|
Military
|
1227.60 (120)
|
P(Y) |
IS-GPS-200D |
L2C
|
Civilian |
"
|
CM CL CNAV
|
IS-GPS-200D |
L2M
|
Military
|
"
|
M MNAV
|
|
L3
|
Nuclear Detonation Detection System |
1381.05 (135)
|
|
|
L4
|
being studied for Iono correction
|
1379.913 (134.888)
|
|
|
L5
|
Safety of Life |
1176.45 (115)
|
I5 Q5 CNAV
|
IS-GPS-705 |
WAAS is for the Americas. The military WAGE is either global or
area specific. There are similar augmentation systems for other
parts of the world.
The L5 signal allows for ionospheric corrections making aircraft (and
all other) systems much more accurate. Another aspect of Safety
of Life is signal integrity allowing the user to know he has a good
solution and when he doesn't.
Major Influences
- When GPS was a proposal it would have failed to be funded
if it were not for the Nuclear Detonation Detection System. (First
launch 1978 Feb 22, so the proposal stage may have been in the mid
1960s?)
- Prior to the 1 September 1983 shootdown of KAL007 (Wiki: President Ronald Reagan ordered the U.S. military to open their Global Positioning System (GPS) to civilian use.)
GPS was a secretand stelth technology. That's to say the
signal on the Earth's surface is below thermal noise, so if you don't
know where it is and how to demodulate it, you will not know it's there.
- Wiki: In the 1990s, the FAA started pressuring the military to turn off SA permanently and it was on 1 May 2000.
- The Safety of Life L5 signal, see above, is driven by the FAA.
DAGR (Polaris Guide)

The DAGR is the
current (accepted 2004, current 2008) receiver. It's a 12 satellite L1 (12 chan) & L2 (12 chan) receiver
that can be crypto keyed.
It has many improvements when compared to the PLGR.
As of Oct 2008 there are two versions.
AN/PSN-13 p/n 822–1873–001
Firmware: 984-2461-011
and
AN/PSN-13A p/n 822-1873-002
The "A" version has a faster serial port to allow the use of USB to serial converters and it has another 1 PPS output.
Firmware: 984-3006-001
The DAGR is
procured under specification SS-M/V-600A, SS-M/V-600B, SS-M/V-600C as of 2007.
GB-GRAM (Polaris Link)

In addition to the handheld DAGR there is a
12 Channel printed cricuit board version called the Ground Based - Gps Receiver
Application Module (
GB-GRAM).
Note a Ground Based application will have velocitiy, acceleration and
jerk values much less than those encountered in air and space craft and
a GPS can exclude the higher values making for a better
solution. More importantly GPS receivers rated for
air or space usage have more controls on their distribution.
The military DAGR and GB-GRAM are CCI items that can not be sold to civilians, but
the Polaris Guide is the civilian version and the Polaris Link is the
civilian version of the GB-GRAM.
Capabilities
Classical PVT
The classical military uses for GPS are
Position (including waypoints and Routes), Velocity and Time (PVT) and the DAGR has all
the capability of the
PLGR in this regard. But in addition it can
do more.
Gun Laying System Civilian: Azimuth Determination
This is listed first since it's the feature that I'm most interested in.
Since both bearing and distance between the two locations is calculated this can be used as a
surveying method.
GLS will shortly be called Azimuth Determination for both the DAGR and
Polaris. This way it's OK for the Polaris to have Azimuth
Determination.
Real Time Kinematic (RTK) is the surveying term for a GPS receiver that
tracks while it is being moved. But in the surveying application
there's a radio link from the base station to the rover and the actual
position of the rover is known. The North Finding system does not
need to know the actual position of either point.
6181274 Satellite navigation receiver for precise relative positioning
in real time, MIT, Jan 30, 2001, 342/357.04 ; 342/357.08 - is a similar
patent but includes a radio link for code and carrier phase
corrections.
The next generation Rockwell GPS receiver may have RTK capability, but
it takes more channels since L1 and L2 must be on seperate channels.
Single Receiver Method
Using a single DAGR with a survey grade
GPS antenna attached to the top of a stake and then moving it
to another stake you can determine the bearing and distance between the
stakes. This would allow surveying using a single DAGR.
Accuracy of 3 mils (1 mil at 1 km = 1 metre, in NATO countries
it's 1/6400 of a circle). 3 MILs is about 10 arc minutes of
angle. Note that the SIN(3 MIL) * base line length is an estimate
of the error in the length part of the measurement. In 100 feet
that's about 3.5 inches radius.
The method used is covered in patent 5999123 and involves carrier
phase tracking rather than differential corrections. That's how
they get such good accuracy. Rockwell has a number of patents
relating to the detection of carrier phase cycle slip and precision
carrier phase tracking methods which would help in this
application. For example excluding some satellites from the
beginning if they have carrier phase characteristics that make cycle
slip hard to detect.
The accuracy can be improved by minimuzing the time of the measurement because many of the error sources change at a slow rate.
The accuracy can be improved by using a long base line.
The above two accuracy improvements work aginst each other. The
longer the base line the more time it takes to move the receiver.
See
zero baseline test results below for the Polaris Guide civilian receiver.
5999123 Time-relative positioning for static applications, Dec 7, 1999,
342/357.08
This is a method based on tracking the
carrier phase as a single receiver is moved from one stake to
another. The path between stakes does not need to be along a
straight line, but the view to all the satellites being tracked must
not be blocked.
|
| 5021792 | System for determining direction or attitude using GPS satellite signals | Jun 4, 1991 |
| 5266958 | Direction indicating apparatus and method | Nov 30, 1993 |
Dual Receiver Method (Sub Mil)

This
provides about the same accuracy as the AG8 gyroscope +
Theodolite system but is much more rugged, smaller, lighter and less
expensive than the fragile AG8. But the AG8 does work in
underground locations where there is no GPS signal so probably is still
being used.
In the dual receiver method you specify a walk time with the two
receivers next to each other and cabled together so they can do a
precision time sync. After you have moved the rover to the out post
and the walk time expires both receivers make and record a single
measurement at the same instant. Then when the rover GPS is brought
back to the master GPS and they are cabled together, an L1 carrier
phase calculation is made to determine the difference between the
master and rover locations. The improvement comes about because both
measurements are made at the same time. In the single receiver method
there is a time difference between the measurements.
Accuracy in the 0.5 mil area or around 1 arc minute of angle.
Antennas for Azimuth Determination
They say survey grade external antenna(s) is(are) required for both
methods. Also during the walk between stakes a clear
view of the sky must be maintained but the walk does not need to be in
a straight line. The reason for the survey grade antennas is that
when a lesser antenna, like the RA1 is used multipath during the walk
causes one or more satellites to break lock making the method non
operational. Survey grade GPS antennas typically have choke rings
below the antenna to prevent multipath, but you could mount the RA-1
(or maybe the DAGR/Polaris) over a ground plane to achieve the same
result.
Triple Receiver Method?
This is NOT supported on any DAGR as far as I know, but may be on some systems, like on ships.
5021792 System for determining direction or attitude using GPS satellite signals
This is a system that uses three GPS receivers and three antennas.
Maybe a future enhancement on the dual receiver method, i.e. 3 Receiver method
The antennas are used:
First in a straight line
Second two of them are interchanged
Third one of them is moved away from the line by the distance between the remaining two.
|
| 3766556 | CHANNEL SWITCHING PHASE - for canceling IF non linearities
| Oct 1973 |
| 4719469 | Direction-determining system - two fast switched antennas and interferometry
| Jan 12, 1988 |
| 4845502 | Direction finding method and apparatus - two antennas on rotating platform are combined in balanced mixer
| Jul 4, 1989 |
| 4881080 | Apparatus for and a method of determining compass headings, Navy - uses two antennas, ant switch and one GPS receiver
| Nov 14, 1989 |
Target Location (Civilian: Way Point Determination)
This was also supported with the PLGR. By using a compatible
Laser Range Finder cabled to the DAGR (or manual input of range,
bearing and elevation angle to the target) you can get the coordinates
of a
target. This requires that the Laser Range Finder sends at least
the magnetic bearing and distance to the target and better in addition
the elevation angle. So far I haven't found LRFs on the open
market that have a range of more than about 1 km whereas the military
LRFs may be good for 10 km.
An alternate way to get target location would involve taking multiple
sightings from a different locations (maybe even from a moving vehicle)
where you only know magnetic bearing and elevation angle. Then
triangulate the readings. Note by using more than two sightings
averaging can be used to improve the precision of the target
location. The DAGR does support multiple sightings of the same target thus reducing the error.
6064942 Enhanced precision forward observation system and Method, Rockwell Collins, May 16, 2000,
701/213 ; 342/118; 342/357.01; 342/357.06; 342/357.08; 434/1; 701/207 - employs multiple measurements to reduce the CEP
|
| 5736960 | Atomic
clock augmented global positioning system receivers and global
positioning system incorporating same | Apr 7, 1998 |
| 5739786 | GPS transfer initialization system | Apr 14, 1998 |
| 5757316 | Attitude
determination utilizing an inertial measurement unit and a plurality of
satellite transmitters | May 26, 1998 |
Low cost
astronomical orientation sensors
are available that can tell you the magnetic bearing and elevation
angle to any target. For example the Clestron SkyScout or Mead
mySKY.
Laser Range Finders
There are civilian LRFs made for golf and sporting applications with ranges up to about 1 km, most are a fre hundred yards.
Leica Vector IV
Litton Mark VII - 7.3
x 18 day optics, 4 x 50 image
intensifier, Nd:YAG laser, eye-safe 1.57 micron
Riegl LASERTAPE FG21 - up to 2500 meters
The military LRFs typically have a max range of about 10 km.
AN/GVS-5 (MX-9838) Nd:YAG 1.06 micron) hand held fielded 1980 - Class 4 Non-Eye Safe, only usable in daytime
AN/PVS-6 Mini Eyesafe Laser Infrared Observation
Set (MELIOS), only usable in daytime
MLR 30 - 20 km range, 1.064 microns
MLR 40 - 20 km range, 1.54 microns
LH30 - 80 m to 20 km
LH40C - erbium:glass laser, 1.54 microns, built in compass & inclinometer
Leica
Geosystems ZVBA
Brashear LP MLRF 100 - 1.54 microns, mounts on personal weapons
AN/PEQ-21B Common Laser Range Finder (CLRF) - similar
in magnification and field of view to the M-22 binoculars, built in compass & inclinometer, GPS interface
AN/AAS-37
AN/AAS-38 Nite Hawk
LRM 2500
CI - 2500 m, built in compass & inclinometer
LRB 25,000 25 km - 1.54 micron eye safe,
Carrier Phase Data
The DAGR supports carrier phase data output. This is the method
used by surveyors to get very high levels of precision. To use
the carrier phase data for surveying you need to convert it into RINEX
format and then use post processing software to remove the integer
ambugity. RINEX conversion software is not currently available
(Oct 2008). Also it's not clear of the Polaris Guide (civilian
DAGR) supports carrier phase on just L1 or on both frequencies.
Time
Frequency hopping radios need the current date and time accurate to
less than a second. The Polaris supports both Have Quick and
SINCGARS time formats.
PLGR-II
The PLGR-II was made for Special
Operations and some foreign governments (Australia, UK?).
It's a 12 channel L1& L2 receiver.
Montgomery Design page about PLGR and PLGR II. "MDI worked with Rockwell to adjust the surfaces of their
prototype unit, minimizing the potential for cavitation."
There are three versions:
SofTouch Standard green case - 1 meter underwater
Dive Capable black case - 10 meters operational (20 meters survive)
Deep Dive gray case - 24 meters operational (36 meters survive)
Batteries
The removable battery tray can hold up to 8 AA cells. There is a
menu item for Alkaline or Lithium cells and for 6 or 8 cells. (not sure
which 6 to install for this option).
The memory battery is the 3.6 V 1/2 AA just like the DAGR.
After installing the batteries the SV Status page shown ALM AGE: 99
DAYS. But after more than a half hour later the ALM AGE: drops to
1 DAY when for sattelites are being tracked.
Comparing PLGRII and DAGR
Once any GPS receiver has locked onto one satellite it can then
download the almanac data for all the other satellites.
That takes a little less than 15 minutes. Once that's happened
the ALM AGE: will change from some number between 2 and 99 days to 1
day. Prior to taking these two photos the almanac was made
current. The key difference of the PLGRII is it's heavier and the
buttons take much more force to activate, probably both of those
differences are because this PLGRII can be operated down 10 meters and
stored at a much greater depth in water. The DAGR is only
specified for 1 meter of water.
The PLGRII uses an 8 AA cell battery tray with the option of a 6 AA
tray that has an external DC power connector. If you don't have
the optional 6 AA battery tray you can not use external DC power.
Outdoors

|
Indoors

|
PLGRII External Antenna Jack
(0
The PLGRII external antenna connector is a waterproof type. I
expect the mating connector looks just like the plug shown here.
It's 6.17 mm (0.243") O.D. Now to find out what it is.
This is the same O.D. as the 75 Ohm SMB, but should be 50 Ohms and the SMB male pin does not look to be in the correct location.
|
DAGR External Antenna Jack

The DAGR External antenna connector is the very common SMA (3mm).
Notice the nut on the external antenna cable will be recessed into the
pocket so you can not tighten it with your fingers. There is a
"Spinner" available for this. It's a plastic wheel with fingers
that snap onto the hex nut.
|
They both work about the same outdoors and indoors.
Menus
Holding down MENU gets you to the Quick Menu page. Use the arrow keys to select and ENTER to goto that menu.
When in Quick Menu is PAGE is pressed the menus rotate as:
Quick Menu -> Operations Menu -> Setup Menu -> Data Menu ->
WPT/RTE Menu -> Calc Menu -> SV Menu -> Apps Menu -> Quick
Menu
Setup Menu
Use the arrow keys to select and ENTER to goto that menu.
RECEIVER
|
UNITS
|
NAV-SETUP
|
INIT
|
USR-DTM
|
I/O |
USR-COORD
|
SUBMODE |
KOI-18
|
|
KEYPAD
|
P
|
INIT POS/PRECISE CLEAR
Lat
Lon
EL:
GS:
TRK:
TheTitle line POS or PRECISE can be selected and CLEAR activated.
Lat, Lon, Elevation, Ground Spped and Track can be initialized.
Pressing PAGE brings up the crypto key input in either
Hex or
Decimal notation.
KOI-18 Load
Select LOAD then pull tape.
LOAD
QUIT
Data Menu
Use the arrow keys to select and ENTER to goto that menu.
NAV
|
RCVRSTAT
|
POS
|
SVSTAT
|
RCVD SCRNS
|
TSS
|
POS RPT
|
ZERO/CLR
|
|
P
|
Help Menu
Note: to get to the Help menu from the Quick Menu instead of pressing down arrow four times just press up arrow once.
HELP TAB:[A]
If an arrow key is pressed the focus will jump down into the lower list.
If ENTER is pressed, then up or down arrow the letter after TAB: will
increment or decrement and the list will change being centered on the
new letter.
Once the correct TAB:Letter has been selected press any arrow key to
move the focus to the center of the list of topics. Now press
ENTER and notice that to the left of the current topic an Up and Dn
arrows appear. Now pressing UP or DN arrows scrolls the list.
Waypoint Route Menu
Use the arrow keys to select and ENTER to goto that menu.
WPTNEW
|
RTEEDIT
|
WPTEDIT
|
RTECOPY
|
WPTCOPY
|
RTECLEAR
|
WPTCLEAR
|
ALERTS
|
WPTSTATS
|
|
WPTGROUPS
|
P
|
Receiver Hardware Status
Pressing PAGE:
RCVR HW STATUS -> RCVR SW STATUS -> CONFIG STATUS -> RCVR HW STATUS
Data Transfer
Send To:[com-a] [com-b]
Type:[all] rcvr setup] [targets] [submode setup]
[user coord] [time] [user dtms] [units setup]
[sv data] [mission data] [all]
SEND QUIT
Operations Menu
Use the arrow keys to select and ENTER to goto that menu.
WPTNAV
|
RTENAV
|
MARK/MOB
|
SKIPWPT
|
UNITS SEL
|
REVRTE
|
TRACK-MODE
|
HSF-CFG
|
GOTO
|
SEND
|
SUBMODE SEL
|
P
|
SUBMODE SEL
Submodes: 1 Foot, 2 Gnd Veh, 3 Para HAHO, 4 Aircraaft, 5 Maritime, 6 Dive, 7 Survey, 8 Spare
ACTIVATE QUIT
HSF-CFG History File Configuration
Calculate Menu
Use the arrow keys to select and ENTER to goto that menu.
DISTANCE
|
LRF
|
FROM
|
|
BEARING
|
|
INTERSECT
|
|
|
P
|
LRF
Requires stored Laser Range Finder data
Applications Menu
Use the arrow keys to select and ENTER to goto that menu.
JAMMER FINDER
|
|
SELFTEST
|
|
TARGETING
|
|
|
P
|
JAMMER FINDER
SELFTEST
Targeting Menu
NEW
|
VIEW
|
CLEAR
|
WPCOPY
|
DEFINE
|
SETUP
|
Space Vehicle Menu
SVSTAT
|
SV SELECT/DESEL
|
DOP-CALC
|
SV-SCHED
|
Tailored Screen Sequence Page
It depends on the selected submode.
Polaris
Primary AA Batteries
All the printing is inside the battery compartment.
Notice that the title: Receiver, Hand Held SPS
The "SPS" means Standard Positioning Service" i.e. the legal to own civilian model.
SPS also appears on the lower right of the front panel.
When installing the AA batteries it's best to lower them into the
battery holder while holding level. If you tip the battery and
try to install it one end then the other it's a very tight fit.
Don't forget to put the removing strap unter the cells.
L-91 Lithium 1.5 V Primary NSN: 6135-01-333-6101 - these have more
capacity and work at temperature extreams where Alkaline batteries fail.
Memory Backup Battery
The White dot on the memory battery cover and the white dot on the main
battery cover are the vents. Single bump connector is J1, two
bump connector is J2.
Memory battery is 1/2 AA size 3.6 Volt Lithium. Radio Shack 23-026 aka:
3B26TC, 3B33TC, 3B955TC, 29045, ER3S, G3 ER3STC, LS3,
LS14250 NSN: 6135-01-435-4921
TO4, TL-5101, TL-5101/S, TL5111/S, TL5112, TL5112/S, TL5151
Note there is also a 3.0 Volt Lithium 1/2 AA size battery, but it probably will not last as long.
There is no pull strap for this battery and it's a very tight fit, so a small screwdriver may be needed to get it out.
J4 External DC Power
Polaris (DAGR) GPS receiver with Turck PKG3M6S90S Cable
This is the connector the Rockwell documents recomend.
BUT,
it is very difficult to install and remove because the stock nut is
almost completly surrounded by the recessed pocket so you need strong
fingernails to install it.
External Power Consumption vs. Input Voltage
Volts
|
ma
|
mw
|
<7.x
|
0
|
0
|
8
|
129
|
1032
|
10
|
99
|
990
|
15
|
65
|
975
|
20
|
52
|
1040
|
25
|
44
|
1100
|
Polaris (DAGR) with DAGR specific Cable

This cable was made for the DAGR, but may be very expensive. The
problem is there aree really two nuts, the one shown above is on the
cable and another nut is installed over it. The outer nut is not
tight aginst the internal nut so after it's been snugged when you
wiggle the outer nut you feel slop. That may cause someone who
has not been properely trained to overtighten and that may lead to a
broken plastic case.
The other problem is that the nut makes a ratteling noise when the
receiver is shaken. That might consume a lot of someone's time
trying to find where the rattle was located.
J4-1 = Ground = Brown
J4-3 = Positive = Blue
J4-4 = no connection
J1 & J2 D-Sub 15 Pin Connectors
The fifteen contact connector on the DAGR is the same one that's on the
PLGR.
Most of the functionally is the same as for the PLGR. For example
the PC cable is the same for either the PLGR or DAGR. They are
not exactly the same, but are very close. The 15 pin High Density
D-Sub connector is the same one used for PC video monitors. The
computer monitor cable has DB-15m connectors on both ends and so will
not mate to the DB-15m connectors on the DAGR. But, an HD15 video
extension cable has an HD15F connector on one end. You can just
cut off the HD15M connector to have a ready made cable.
Another problem is
that when the DAGR is in the mount there is not much room behind it, so
a normal DB-15 connector hood will stick out the back too far to allow
the mount to be used. If you know of a hood that can be installed
to the left or right
let me know.
The Right Angle type connectors have the angle going up or down which
is good, but there still isn't a commercial sideways shell.
Note PLGR J2 is very close to DAGR J2 (although there are small differences). See the DAGR manual J1: Tbl20-1, J2 Tbl20-2.

The Radio Shack 276-1502 is a "15 Position High Density Female D-Sub
connector with solder cups that fits the DAGR and PLGR allowing you to
make up your own cables. Jameco 164823 is much lower in cost.
Note one bump over J1 and two bumps over J2. Seems strange that
they didn't put three bumps over J3 and four bumps over J4.
In the photo it's not easy to see all three rows of pins on the
connector, but they are very clear on the bottom of the dust boot.
The PLGR used a fifteen contact size D-Sub shell to hold the external
antenna coax. That seemed a waste of space and the DAGR uses a
recessed SMA RF connector and two fifteen contact interface
connectors. Each of which can be setup to do various things.
J1 Functions
- COM3 with mandatory hardware handshake (RTS/CTS)
- RS-232 2-way coms (300 to 76800 baud), or
- Time Fill for SINCGARS
- 1 PPS In & Out
- Key Fill on DAGR
-
Accept Differential GPS (DGPS) corrections
-
Output NMEA sentences
- Input Laser Range Finder (Mk VII or Other)(data format TBD)
J2 Functions
- COM1 RS-232 2-way coms (no handshake)
- COM2 (no handshake)
- RS-422 2-way coms, or
- RS-232 2-way coms
- 300 to 115200 baud
- Time Fill for Have Quick
- 1 PPS In & Out
- Map Up or Down Loading to PC
- Remote On - Off switch (details TBD, probably open or gound connection)
- COM1 or COM2 can Accept Differential GPS (DGPS) corrections
- COM1 or COM2 can output NMEA sentences
- COM1 or COM2 can input Laser Range Finder (Mk VII or Other)(data format TBD)
TBD port Functions
DAGR/PLGR to/from DAGR/PLGR data set loading (soon firmware cloning)
Reprogram DAGR firmware
COM Port Protocols
Each COM port can be setup to support:
Inputs: ICD-153, Local Area DGPS, NMEA
Outputs: ICD-153, NMEA
Have Quick & 1 PPS J2 Cable
This
cable has the 1 PPS output on the BNC connector and the Have Quick data
on the wire pair. The 1 PPS can be used as the trigger source for
the scope and the have quick data then starts at the trigger
point. BUT, the
HP54501A Scope can
not display the seconds data because of limitations in the window
function. The problem is that there's a preamble on the Have
Quick data that's about 1/4 second long and there's a 20:1 relationship
between the main time base speed and the fastest possible window speed.
I think a way around this is to use the SRS
DG535
as a delay generator triggered from the 1 PPS on this cable and use
it's output to trigger the scope. Now the scope time base can be
set to a rate that will allow a number of samples to occur during each
600 micro second bit time. The plan is to have just the unit
seconds (and maybe part of the tens of seconds bits on the screen and
compare to a digital clock that turns over on the UTC second edge.
Unfortunately the DAGR/Polaris does NOT change it's seconds time
display on the UTC edge, but can be off by up to a second or slightly
more so you really don't know the time by just looking at the
display. Seeing the Have Quick data should show that it's very
accurate.
 |
The
1 PPS output from the Polaris Guide feeds the trigger input on the SRS
DG535. The DG535 can be set to create any desired delay, such as
268.8 ms to start of 10s of seconds. The DG535 output triggers
the scope Chan 1. Have Quick data is on Scope Channel 4.
It's a challenge to get all the software needed for the USB video camera to work.
Under the scope and above the plywood shelf is the Ultralink WWVB
receiver. That data waveform on the scope has been offset so it's
at the very bottom so that the video camera can see the data and the
time. |

|
Have Quick Cable p/n 987-5002-001 NSN: 5995-01-5212-680
This cable only works on J2.
DAGR plug marked P2 and has two raised dots.
PIN
|
Function
|
1
|
nc
|
2
|
nc |
3
|
black Ground
|
4
|
nc |
5
|
nc |
6
|
nc |
7
|
brown Have Quick
|
8
|
nc |
9
|
nc |
10
|
nc |
11
|
nc |
12
|
nc |
13
|
nc |
14
|
nc |
15
|
nc |
|
PC Cable
 |
p/n: 987-5012-001 NSN: 5995-01-5213-198
This cable only works on J2 COM1.
DAGR plug marked P2 and two raised dots.
Three wire interface.
No RTS/CTS like on COM3.
No connections for COM2 RS-422.
DAGR
Pin
|
DAGR
Func
|
PC
Pin
|
PC
Func
|
1
|
|
nc |
|
2
|
1PPS-In_Rtn
|
5
|
Gnd
|
3
|
|
nc |
|
4
|
|
nc |
|
5
|
|
nc |
|
6
|
|
nc
|
|
7
|
|
nc |
|
8
|
|
nc
|
|
9
|
|
nc |
|
10
|
|
nc |
|
11
|
|
nc |
|
12
|
|
nc |
|
13
|
|
nc |
|
14
|
COM1 Tx
|
2
|
RXD
|
15
|
COM1 Rx
|
3
|
TXD
|
1PPS-In_Rtn is the same as COM1_RTN
There is no jumper on the computer DB-9 between 7 and 8 so the computer
must have it's serial port set for no hardware handshake.
|

|
The P2 Cable has a dog leg or
double bend to reduce the distance it sticks out the back to a
minimum. The connector is marked both with two dots and with
"P2". This might be a PC or Have Quick cable.
What are the two brass threaded inserts used for? Let me know.
|
DAGR/PLGR to DAGR/PLGR Cable

|
NSN: 6150-01-375-8663
p/n 426-0141-020
This is a 42" long cable to allow connecting two GPS receivers toghther either DAGRs, PLGRs or a mix.
The cable is symetrical and does not have markings for port 1 or port
(the PLGR only had one port) and this cable was made for PLGRs but is
also used on the DAGR.
Pin
|
Port 1 |
Port 2 |
|
Pin
|
Port 1
|
Port 2
|
1
|
1 PPS In |
1 PPS In |
6
|
1 PPS Out |
1 PPS Out |
2
|
-
|
1 PPS Rtn
|
11
|
-
|
PPS_O_Rtn
|
3
|
-
|
-
|
nc
|
-
|
-
|
4
|
-
|
-
|
nc
|
-
|
-
|
5
|
-
|
-
|
nc
|
-
|
-
|
6
|
1 PPS Out
|
1 PPS Out |
1
|
1 PPS In
|
1 PPS In |
7
|
-
|
-
|
nc
|
-
|
-
|
8
|
-
|
-
|
nc
|
-
|
-
|
9
|
-
|
-
|
nc
|
-
|
-
|
10
|
-
|
-
|
nc
|
-
|
-
|
11
|
-
|
PPS_O_Rtn |
2
|
-
|
1 PPS Rtn |
12
|
-
|
-
|
nc
|
-
|
-
|
13
|
-
|
-
|
nc
|
-
|
-
|
14
|
COM 3 Tx
|
COM 1 Tx
|
15
|
COM 3 Rx |
COM 1 Rx |
15
|
COM 3 Rx
|
COM 1 Rx
|
14
|
COM 3 Tx |
COM 1 Tx |
|
Mystery Cable

May be the Vehicle Mount Fill Cable.
|
DB-15m
Pin |
Function
|
U-228
Pin
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
Shipping Container
Received in double box. This is the inner box with a very cleaver
cardboard fold, it's not shrink wrap, you can remove the Polaris after
unfolding.

In addition to the Polaris there was a two page packing slip.
Order placed 17 Oct 2008 received 14 Jan 2009, pretty close to 3 months.
No batteries or other paperwork is included with the unit.
This is the same box used to ship the DAGR.
Applications
Azimuth Determination, North Finding, Survey Mode (mil speak: Gun Laying System)
Once in the AZ Determination page proceed as follows:
4AK = 4 Arrow Keys
- Press Menu and scroll to Create New, press Enter
- With
the name highlighted, press Enter and 4AK select the letters and
numbers for you chosen name then 4AK to move to SAVE and press enter.
- With the Walk Time highlighted press Enter, 4AK to set between 1 and 180 seconds, then press Enter
- The display will ask you to press Enter to start the
process. (Prior to this the receiver should have been in
Continuous mode and locked on a number of satellites, but if not then
you will need to wait here). You can't start until at least 4
satellites are being tracked, more is much better because while you are
walking you may loose some and if the total number goes below 4 then
you need to start over.
- After you are stratified with the number of starting satellites press Enter and the display will switch to the walk time count.
- Walk to the second point and when in position press Enter while
holding the receiver still, it will take maybe 5 to 10 seconds to
determine position 2.
- When it's down press the down arrow to proceed.
- The data defaults to military units. Changing the units in
the main Menu does not effect this page, so 4AK highlight each field
press Enter, and select which units to change, for example the bearing
change to degrees and the reference change to True, distance in Miles
and feet, etc.
The first result window shows:
- Single Receiver Method (I think you need to connect a second receiver in order for this to change, it's not a menu choice)
- Azimuth: 62.29 deg True
- Back Azimuth: 242.29 deg True
- Range 47.02 Feet (0.01 feet is approximately 1/8 Inch!)
- Estimated Azimuth Error: +/- 000.49 deg.
- Press the down arrow to move to Point 1 Information
- 10 S 405008 East
- 37905 North
- 988 Ft MSL
- Press the down arrow to move to Point 2 Information
- 10 S 485021 East
- 443379 North
- 987 Ft MSL
Questions:
Is it better to carry the receiver so the LCD is vertical or should the
LCD be level? LCD level both for compass and GPS reception.
Where inside the receiver is the internal antenna located? just above the LCD.
Thoughts
Using a choke ring antenna would prevent multipath and so you would not
loose as many satellites. Once one looses lock it is removed from
the solution because after it relocks the cycle count is no longer
valid.
17 Apr 2009
Zero Baseline Testing Single Receiver Method
A way to test the accuracy of the azimuth determination system is to NOT move the antenna. In this case the
roof top GPS antenna was used for both the first and second positions. If the Azimuth Determination procedure is run using a fixed
antenna the result should be a distance of zero with an arbitrary angle.
Things that can be varied are the receiver
mask angle.
Zero degrees increases the
number of SVs but also allows for more multipath errors.
It’s also location dependant.
The walk time is controlled by making the
setting greater than the actual time and then pressing ENTER at the desired
test time.
Note there is no display in
the results that will tell you the actual walk time so there’s a few seconds of
error in the estimate of the actual walk time.
The number of SVs can be controlled to a small extent by when the test
is run since the satellite configuration changes with in a 12 hour cycle.
The Walk Time input for the single receiver method just sets the
maximum allowed walk time, so it's best to just use two up arrow
presses to set it to 180 seconds. The actual second measurement
is made when you press ENTER at the second location. My
guess is that when the ENTER is pressed the first time the DAGR starts
logging carrier phase data. When ENTER is pressed the second time
the DAGR does the calculations involving processing the logged
data. So the time it takes to process the data depends on the
actual walk time and is very close to half that time. For example
if the walk time was 2 minutes it will take 1 minute to process the
data.
Plot of Range error in Inches vs. Walk time in Seconds

What's not shown is the number of SVs used for the solution. When
the test is started there may be 8 to 10 SVs being tracked, but once
any of them drop out they can not be used in the solution so it's not
uncommon to loose one or two sattelites by the time the test has
finished. Maybe because of the change in number of SVs
and/or different DOPs the test results are not easy to nail down, but
you can see there's a definate relationship
between walk time and accuracy. A very rough rule of thumb might be:
Accuracy (Inches) = Walk Time (Seconds) / 20
For example at 20 seconds the accuracy varies from 1/2 Inch to 2 Inches.
At 60 seconds it varies from slightly more than 2 Inches to slightly more than 5 Inches.
The accuracy seems to get better than the rule of thumb when the walk
time exceeds 2 minutes. I'm not sure of this is real, or not?
The problem with trying to use walk times near 180 seconds is that the
DAGR aborts the measurement at 180 seconds instead of making a
measurement. It's impossible to have a walk time of more than
about 175 seconds because the pressing of ENTER has some time delay
before it stops the test.
So for the single receiver method the possible angle accuracy depends
on how quickly you can move the DAGR while not blocking any SVs.
These are just calculations that have not yet been tested.
If normal walking speed is three miles per hour (4 feet per
second), then after 180 seconds the baseline would be a little under 800 feet
(241 meters).
An error of 9 inches in 792
feet is 0.054 deg (3.26 arc min) or 0.96 Mils.
If a running person traveled at 8 miles per hour (12 feet
per second) then at 180 seconds the angle would be 9/25344 or 0.0198 deg or
0.35 Mils.
If a car averaging 30 miles per hour moved the receiver and
the test lasted 2 minutes the expected accuracy might be 0.0054 deg or 0.096
Mils.
Survey Equipment to support Single Receiver Azimuth Determination
SECO makes a number of poles used to
sup[port either GPS antennas or prisim retro reflectors that are
suitable for this application and have some very handy features.
Since minimuzing the walk time is important a system where the antenna
is just plugged in rather than locted is important. Although SECO
makes a number of clamps to hold survey data collectors they don't have
anything that's DAGR specific so I'm going to try and modify one of
their plain pole clamps to allow the stock DAGR mounting bracket to be
attached. (13 April 2009)
Part of Azimuth Determination Setup

The
Pole and bipod are standard SECO (Survey Equipment Co) items.
This is a very modular system where all the pole sections have 5/8-11
female threads on both ends.
A friction clamp is holding the DAGR standard mount with a 10-32 screw
and flat washer making the connection. The left mounting hole in
the DAGR mount is used so that the back connector area is clear of the
pole.
Just below the DAGR there is a circular bubble level (black object to left of pole).
Just below the bubble level is a quick disconnect fitting. The
black pole is attached to the pole above and can be lifted off the
lower pole.
The lower pole is fitted with the bipod. The upper part of both
bipod legs has a lever actuated length adjustment to allow easy
plumbing of the pole.
Rather than spend a lot to get another of these pole setups, I just got
a male quick connect pin with a 5/8-11 female thread to put on top of
my existing surveying tripod for the second location.
The pole plus bipod arrangement has an advantage over a tripod in that
the distance between the GPS antenna and the mark on the ground is a
fixed distance. That's not the case with a tripod.
This setup breaks down to a much shorter length and fits into a carry bag.
DOP Planning
Yesterday (17 Apr 09) there were 7 satellites being tracked but after
moving the receiver 33 paces away and returning to the pole the error
message was poor satellite geometry. So some planning needs to be
done before hand to chose a time when the geometry is good.
Trimble has a free program called "Planning" to do this.
Trimble Planning Software Downloads -
They also have a web page where you can get current GPS data.
GPS Data Resources - Almanac files
Outdoor Zero Base Line Walk
21 Apr 2009 - Choose 11:45 to 12:05 window and tried two walks.
The first for about 2 minutes resulted in a no solution, poor DOP message.
I'm guessing that if I walk too close
to my house some sats are blocked and dropped and the remaining sats
don't have a good enough DOP. So to access some locations the
path may need to be curved to keep clear of the house GPS shadow.
The second for about 1 minute resulted in a distance error of about 4 inches.
28 Apr 2009- It's straight forward to modify the 987-5006-001
mount by adding SECO p/n: 103868-005 and the associated 1/8 x 7/16
spring pin and 1/4-20x1/2 cap screw. Then it plugs into the p/n
5198-052 Pole Clamp and can be adjusted for tilt. You can just
see the spring pin below the quick release pin on the mount that mates
with one of the the small holes on the pole clamp.
Time Display
The DAGR / Polaris Guide POSition page, when scrolled down, shows the
current time and date. But, the displayed time is often in error
by 1 second. This is in my opinion a bug in the Rockwell Collins
firmware. All my other receivers that display time have the
seconds change at the UTC second boundry. The Trimble Scoutmaster
even displays the tenths of a second correctly, see image below.

The
Polaris Guide (DAGR) is showing the time as 0852:00 but the time is
really 0852:01.0 as shown on the Trimble Scoutmaster to the right.
An interisting thing about the Scoutmaster display is that the date is shown as:
WED 06 Sep89
That's off by 1024 weeks, i.e. the GPS week rollover problem.
I wonder what the DAGR/Polaris Guide will show in 20+ years?
Internal Magnetic Compass
The Internal Magnetic Compass does not have tilt compensation.
The compass can be found at <press and hold POS> then <down
arrow> to see the compass (you may need to press Enter and arrow
keys to highlight the compass, the Enter and activate it since the
normal mode is not continous operation). I found that the first
calibration was no longer working by turning in a circle and noting
that the display did NOT show the expected 0 to 359.9 deg range but
instead showed numbers around 160 degrees plus or minus maybe 30
degrees. After a simple calibration it was working fine.
To check for tilt:
Face magnetic North (or magnetic South) and tilt up or down about 10
degrees and note the change in reported bearing is only a few degrees.
While holding the receiver level, Face magnetic East (or magnetic West)
then tilt up or down about 10 degrees. This causes about a 10 degree
error in the bearing because there is no internal tilt compensation.

The Suunto Vector wrist instrument has a bubble level (just above the 7 in 337) on it's face to aid in holding it level.
The small rectangle in the upper left is the barometric pressure history.
"N" for North which is the closest of the three letter compass points.
337 degrees magnetic bearing.
The black bar below the bearing has a band at the right end below COMP for compass mode.
The modes are left to right: Time, Alti, Baro, Comp
3:57 local time.
On the very outer circumference at the top is a single black
tick. Opposite it are three ticks. These form a North
pointing arrow.
The Bezel was set to the local magnetic devation years ago and you will
see that the North Arrow is pointing very close to the "N" on the
bezel. So the line from 6:00 to 12:00 is pointing close to
True North.
See:
Experiment Relating to the Vertical Component of the Earth's Field for a similar experiment to that above for the Polaris/DAGR.
Operating Modes
When MENU is pressed (from any of the Position pages) one of the choices is Select Op Mode. The choices are:
Continuous -a new fix each second
Standby - no satellite tracking to conservi battery power, but data input and all other operations can be done
Fix - get a single fix then go into Standby
Average -
In average mode the Present Position page shows Averaging
nnnnn under the L/L info, but the max number of averages is limited to
32400 seconds, i.e. 9 hours. Seems strange that it's not one
orbital period of a GPS satellite or longer. For example after 32400 averages on my house antenna the position was:
Surveyed Position
|
39:11:24.5833 N
|
123:09:50.4842 W
|
Polaris
|
39:11:24.63 N
|
123:09:50.51 W
|
Delta (7.3 feet)
|
0.0467"
|
-0.0258"
|
Time Only - all the effort is put into getting the time BUT in any mode
the time display can be off by 1 second. i.e. you don't
know the time to a second.
Maps & Images
The DAGR & Polaris can make use of .gpm map files and .??? images files. The map can be zoomed in or out.
The civilian map loader is Rockwell p/n 811-1213-006.
ESRI has a number of mapping products that may be related.
The
USGS has free maps for download in the store. For Ukiah they have the 7.5 minute, 30 minute and 1x2 degree maps.
The county planning office has a GIS system and has made custom paper
maps for me. It may be that case that they can also make a custom
electronic map that can be loaded into the Polaris?
|
DAGR
|
Polaris
|
GPS Map Toolkit Software
|
984-3095-xxx
|
822-1213-006
|
The Toolket includes both the Map Creator and Map Loader.
July 2009 -xxx is -006. Price for the Polaris is $751 but I think also requires a multi thousand dollar
ESRI GIS software pcakage in order to use it.
To use the Map Creator the PC also needs:
Commercial Joint Mapping Toolkit (C/JMTK) ArcObjects software
National Geospatial-Intelligence Agency (NGA) map data
Support of raster maps: Compressed Arc Digitized Raster Graphics CADRG) and
Controlled Image Base in C/JMTK
The map capacity of the DAGR is limited to 32 MB max and 100 items
max. Each item can have up to 16 characters in it's name.
Raster maps are used with the image viewer and vector maps with the situational awareness window.
Maps can be loaded from a PC to the DAGR/Polaris, between two receivers, or from the receiver to the PC.
Mounting

|

|
Mounting Bracket
The spring loaded pins will stay retracted if rotated.
marked p/n: 907-5006-001
Strange that there's no provision for a padlock.
|
Mounting Bracket Adapter
This adapter bracket has the same four hole pattern as the
plastic PLGR mount. So by using this bracket you
can mount a DAGR in the same holes that held a PLGR.
The top center hole was made by a prior user.
marked p/n: 987-5177-001
may also be: p/n 987-5007-001
|

Polaris in military DAGR mount
The threaded hole at the bottom center is for a ground connection.
|
Antenna
Internal
The internal patch antenna is at the top facing up so the receiver should be laying flat so the antenna can see the sky.
External
In order to detect the external antenna and not cause
an antenna fault warning message it needs to draw 15 to 60 ma from the
nominal 3.3 Volt supply.
3.3 V / 15 mA = 220 Ohms max to 3.3 V / 60 mA = 55 Ohms min.
Trimble 28367-40

|
Seems to work OK. It has an SMA connector mag mount.
L1
Volts
|
mA
|
1
|
5
|
2
|
10
|
3
|
14
|
3.188
|
15
|
4
|
17
|
5
|
20
|
|
Trimble 17572-100 16240-00

|
This is a survey grade antenna with 5/8-11 threads.
A couple of tie-wraps holding the mount to the threaded rod.
L1 or L1/L2?
Works well at about 37 mA.
Volts
|
mA
|
1
|
9
|
2
|
20
|
3
|
37
|
3.047
|
37
|
4
|
98
|
5
|
150
|
|
AeroAntenna Technology AT575-75AW-TNCF-000-RG-36-NM
 |
This is a survey grade antenna with North Arrow and 5/8-11 threads.
The threaded rod is rrequired since the TNC connector on the antenna would otherwise hit the black tripod adpter.
L1
AT575-75
Frequency: 1575 +/- 5MHz(L1)+ Glonass Polarization: Right Hand Circular Axial Ratio: 3 db max Gain: 00,12dB,26dB,36dB Voltage: 00,05,RG(5-18VDC) Impedence: 50 OHMs Connector: TNCF,BNCF,NTPF VSWR: <=2.0:1 Magnet: NM(No) Finish: Weatherable Polymer Color: W,O Weight:13 oz max.
Volts
|
mA
|
1
|
1
|
2
|
11
|
3
|
17
|
3.167
|
18
|
4
|
23
|
5
|
36
|
|
AeroAntenna Technology AT2775-42 with the Choke Ring

|
Now being used with Ashtech Z12R
GPS receiver, but probably will work with DAGR. It should be the
best antenna so far for North Finding because of the choke ring
lowering multipath fading.

|
Sensor Systems S67-1575-58
 |
This is a passive antenna, i.e. no gain and is a DC short circuit. The Polaris Guide protests:
L1
WARNING! EXTERNAL ANTENNA FAULT DETECTED
This is caused by the DC shorted nature of the antenna. You can
see in the photo at left that the Polaris Guide (DAGR) is working fine
with a passive antenna. All that's needed is a series resistor
choonen to present the minimum acceptable power consumption to make the
receiver happy and allow the passive antenna to be used. |
Garmin GPSIII Plus Antenna
|
This is a DC open antenna so the
receiver does not know it has an external antenna attached. Tried
to fool the receiver by pointing it up and covering the top with my
hand while not coverning the external antenna, but this caussed a
jamming warning message. A DC load would needs to be added to try
it. |
The DAGR uses a three terminal power connector, different from the PLGR's commercial type coaxial two terminal connector.

The
connector is made by
TURCK and the manual says is in their PKG 3M-6
series. But that connector will not work. The problem is
that the DAGR J4 connector is recessed into a pocket, like the J3 RF
connector, and so you can not grab the kunrled part of the nut as shown
in the photo at left.
Turck will sell a raw connector, but they are priced about 4X
higher than a connector assembled onto a cable like the one shown at
left.
There are at least three versions of the connector applicable to the DAGR:
- Stock nut as shown at left
- longer stock nut but about the same diameters
- DAGR nut that looks very similar to the spinner used on the J3 RF connector.
Rockwell Patents
In addition to the patents listed here
Rockwell has many many more. They are heavily into all parts of
GPS including satellites and aircraft systems in addition to the ground
units that are the focus of this web page. In addition they have
patents that make use of GPS for things like factory automation.
7142159 Pseudolite navigation system, Nov 28, 2006, 342/386 ; 342/357.02; 342/357.06; 455/13.2 -
Uses communication satellites with custom up and down link signal formats to get around jamming or poor visibility
7230999 Method for extended coherent data demodulation for GPS
receivers, Jun 12, 2007, 375/316; 375/340; 701/213; 701/214; 701/215;
329/304 -
Uses two I&Q signals offset in time and then differenced.
7190746 Multiple lobe dot product detector for M-code GPS receivers,
6973150 Cycle slip detection using low pass filtering, Dec 6, 2005, 375/371; 375/376 -
Works with single antenna systems.
6959057 Method of enhancing signal tracking in global positioning system receivers
Instead of using a FFT method of searching for the signal frequency, a filter bank is used which is faster and more robust
6738015 Vector extended range correlation tracking of global positioning system (GPS ...
A Kalman filter uses pseudorange errors
to calculate position and velocity corrections in order to better
process weak signal code tracking
6687316 High resolution correlator technique for spread spectrum ranging system code ...
Multipath mitigation by using three high resolution correlators, one early, one on time, and one late allowing interpolation
6683867 Parallel precise time transfer to multiple GPS units
Often GPS receivers are turned off
prior to a mission to conserve battery power. Then just prior to
commencing the mission are powered up and loaded with precision time
and position data from a receiver that's been kept hot. When
there are many receivers that are off this patent teaches combining the
1 PPS with the serial data onto a single data line.
6647080 Carrier phase initialization with sub-LSB accuracy
A method of computing the command word to an NCO to get sub-LSB accuracy
6636558 Multipath mitigation approach for spread spectrum ranging/positioning systems
Multipath is detected as slope differences prior to and after the correlator peak
6590528 Low cost interference reduction system for GPS receivers
Multiple antenna system in front of GPS receiver
6570531 Satellite navigation receiver designed for compatibility with aircraft
automatic landing systems
An attempt to recognize failures by comparing two GPS solutions
6556167 Direct acquisition of very large PN sequences in GPS systems
Direct acquisition of the P(Y) sequence
without the Hand Over Word from the L1 C/A code by breaking up the P(Y)
code into a number of sub sequences and testing all of them.
Instead 15000 sub sequences that have gaps between them are repeatedly
tested thus covering the gaps. 320 seconds should be enough time
to search the full weekk of code. This is an important capability
for cases where the L1 C/A code is not available, like when it's being
jammed.
6501424 Use of GPS correction data on trans-oceanic route
HF radio is used to send the airplane differential corrections like are now sent to coastal ships using LF radio
6421006 GPS augmentation using time offset code modulation
By offsetting the PN code by a large
amount (hours) relative to the actual GPS time pseudolites will not
interfer with normal GPS operation
6393291 Method and apparatus for deriving a high rate output in a GPS system
Combines kinematic and differential corrections to achieve high rate precision corrections
6388611 Method and system for dynamic surveillance of a remote object using GPS
Combines GPS and TV image to determine target coordinates
6369752 Direct acquistion of very large PN sequences in GPS systems
see
6556167 above
6359585 Apparatus and method of determining an orientation of a GPS receiver
Based on using a directional antenna in the GPS receiver either in max signal or null methods.
6336076 Long range GNSS ephemeris data transfer method and apparatus using the same
Pseudolites are sued to transfer ephemeris data - maybe when the L1 C/A code is not available/jammed
6336061 System and method for attitude determination in global positioning systems (GPS)
Uses two receiver - antenna units
6311127 Satellite navigation system having redundant signal processing and matched ...
Aimed at aircraft systems that need to know if they are not working
6307514 Method and system for guiding an artillery shell
Uses a four segment antenna that can be electronically steered
6297769 System and method to estimate carrier signal in global positioning systems (GPS)
A dual receiver approach to attitude determination
6272174 Multiple frequency bin processing
see 6959057 above
6266009 Method to improve carrier smoothing of code pseudorange for global
positioning and GNSS receiver implementing the same
By using dual frequency carrier phase methods the ionospheric variability is reduced
6259400 Fast acquisition of GPS signal corrupted by doppler or time delay effects
Artillery shell converts GPS to another frequency which is reconverted back to GPS at a base station.
6256583 GPS attitude determination system and method using optimal search space ...
Optimized integer ambiguity searching
6208289 System and method for monitoring and reporting GPS pseudo range correction data
A second fixed GPS receiver is used to test differential correction data before it's sent to mobile units
6204806 Method of enhancing receiver autonomous GPS navigation integrity monitoring ...
For aircraft fault finding
6198430 Enhanced differential GNSS carrier-smoothed code processing using dual ...
Dual GPS frequency differential corrections
6188353 Interbuilding and urban canyon extension solution for global positioning systems
Concept for a second positioning system powered by utility lighting
6166683 System and method for high-integrity detection and correction of cycle slip ...Dec 26, 2000, 342/357.04 ; 342/357.11
Excludes satellites where a cycle slip would be hard to detect and uses the delta phase from two antennas to detect a slip
6163021 Navigation system for spinning projectiles
Magnetic sensor used to generate a despun reference frame for an INS system and GPS receiver
6098547 Artillery fuse circumferential slot antenna for positioning and telemetry
see
6307514 above
6069585 Personal direction finding apparatus,May 30, 2000, France
342/443 ; 340/979; 342/147; 342/195; 342/29; 342/417; 342/450;
342/454; 342/455; 367/107; 367/116; 367/124; 367/125; 367/126; 367/99;
381/300; 381/309
Stereo headphones provide an audiable signal to maintain a given magnetic bearing
6067503 Method and apparatus for compensating unexpected frequency shifts in
positioning receivers
Method to overcome the launch high G shock that can break lock of GPS receiver in artillery shell
6064942 Enhanced precision forward observation system and method
6020854 Artillery fuse antenna for positioning and telemetry
Design compatible with the above GPS and telemetry antennas
6018314 Method for obtaining PPS accuracy using an unclassified GPS receiver ...
About limiting the security boundry inside a GPS receiver to lower it's cost
6016121 Multiple frequency GPS receive operation using single frequency sequencing
5990831 FFT implementation of digital antenna arry processing in GNSS receivers
5 more?
5990826 Interbuilding and urban canyon extension solution for global positioning systems
5943008 Single global positioning system receiver capable of attitude determination
5940027 High accuracy low power GPS time source
Time of day clock for GPS receiver (why better than the DS32khz?)
5903654 Method and apparatus for eliminating ionospheric delay error in global ...
5886665 GNSS local constellation/acquisition aiding system
5883597 Frequency translation method and circuit for use in GPS antenna electronics
5883596 ?
5883595 Method and apparatus for mitigating multipath effects and smoothing ...
5748136 Electronic landmark enhancement to GPS based navigation systems
5742207 Tracking loop having instantaneous frequency shift protection
5606732 Direct connect radio and antenna assembly
5552794 Position estimation using satellite range rate measurements
5495408 Method and apparatus for signal tracking using feedback control loop
5488378 Method and apparatus for determining positions on the earth
corresponding to an observed rate of change of satellite range
Cold start position improvement by using the first pseudorange and doppler shift
5403197 Antenna extender apparatus
Looks like the
PLGR antenna
5249027 Inter-vehicle distance measuring system
Not GPS, but based on IR between vehicles on digital highway
5202693 GPS signal processing with 5-level carrier injection demodulation function ...
5021792 System for determining direction or attitude using GPS satellite signals
"A system for determining spatial orientation based on the carrier phase
of signals received from a set of GPS satellites. The system comprises
an antenna array including a number of antennas coupled to GPS radio
receivers, a mechanism for reconfiguring the positions of the antennas
within the array and a signal processing module for processing the data
collected by the antennas and the receivers. The mechanism for
reconfiguring the antenna array is adapted for exchanging the positions
of one pair of antennas and for rearranging the antennas from collinear
into non-collinear patterns. Phase measurements are taken by the
antennas and their associated receivers, both before and after antenna
exchange and after antenna rearrangement in order to provide the data
necessary to determine direction or attitude."
This may be the method used in the dual receiver GLS.
4910525 Audio verification system and technique for GPS receivers, Mar 20, 1990, 342/418 ; 342/356 -
Rockwell has a patent on making the Doppler shift from a selected SV into an audio signal.
but based on the issue date doubt this is currently being offered.
Pruchasing Polaris
Starting Sep 13, 2008 I am trying to
pruchase one or more Polaris receivers. Which ones and what
accessories depend on the quote. On 14 Oct 2008 I learned that a
number of the items that I have asked for quotation are non standard
and must be priced which can take up to a month.
My current thought is to get the Polaris Guide and accessories for a
single receiver North Finding system, except instead of getting it's
case get the case for the dual receiver North Finding System to that it
would be easy to expand to that system. The operational
difference between the single and dual receiver systems is not yet
known, but has been requested.
The long process was expected since when purchasing a battery adapter
for the PLGR a similar thing happened. It took a very long time
to buy a simple part. I think this is because they are setup to
sell to the U.S. Government and need a lot of paper work to do that so
do poorly when trying to sell a simple item.
Glossary, GPS
MPE Minature PLGR Engine
WAAS Wide Area Augmentation System promoted by the FAA, geostationary
satellites transmit GPS corrections similar to RTCM-104 differential
corrections
WAGE Wide Area GPS Enhancement, military version of WAAS (< 4 meters)
GB-GRAM Ground Based - Gps Receiver Application Module uses the same SAASM
ICD-numbers
ICD-GPS-060 Have Quick
ICD-GPS-153 Programming serial Interface includes both hardware and commands
ICD-GPS-200 Signal from satellites
SINCGARS - Single Channel Ground and Airborne Radio System, frequency hopping mode needs Time Of Day and date
Have Quick (SS110990) - Frequency hopping mode needs Time Of Day and date
NMEA 0183 National Marine Electronics Association spec for serial data
messages to allow interoperation of instruments 4800 baud, limited
capability
RTCM-104
TTFF
DS101
DS102
PPS (
SPS (<100 meters)
PLGR Precise Time (SS-M/V-500)
SA
AS
SAASM
Codes
Frequency
Channels
TOD Time Of Day
GPS Global Positioning System (
Wiki has a good treatment)
Links
Rockwell Collins - DAGR - Polaris Guide - GB-GRAM - Polaris Link -
U.S. Army Product Manager, GPS -
Space and Naval Warfare Systems Command (SPAWAR) - GPS & Nav Systems -
Wiki: GPS - GPS Modernization - GPS Signals - Wide Area Augmentation System (WAAS) -
Air Force Space Command - High Frontier Vol 3 Nbr 2 "Global Positioning System International Challenges and Opportunities in the 21st Century"
Caltrans -Surveys Manual - Ch 4 Survey Datums -easy to understand explanation about how NAD83 differes from NAD27 - Ch 9 Control Surveys -
GPS Explorer - a page to locate GPS reference stations and geodetic markeres
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