Navigation Orientation & Position

Brooke Clarke, N6GCE

    Accuracy of Visual Fixes



Determining your position on the Earth (or elsewhere) is an exercise that depends on the interrelationship between time and position.  For example if you know the exact time and can sight a heavenly body with a Sextant then you can determine where on Earth you are. If you know were you are, on a Sunny day you can tell what time it is using a Sundial.  Because of the importance of Navigation at sea the British offered what today would be a $10 million reward for a clock that would be practical at sea to find the Longitude.  The pendulum clock would not work at sea.  Harrison spent most of his productive life developing clocks that would work at sea.

Finding the Latitude turned out to be an even more difficult problem.  At first glance it would seem that all that's needed to know your latitude is a sight on the Sun or a star.  But that fails because the axis of the Earth is wobbling.  For navigating a ship the wobble doesn't matter.  But for determining the distance between Earth and Sun, or make other key astronomical measurements the wobble was a real problem for many decades.  One of the Latitude Service Observatories is here in Ukiah, California.

For precision time transfer you need to know where you are then you can determine what time it is.  Because of this radio based time transfer methods follow the navigation systems.  When Loarn-C was the best nav system it was also the best time transfer method.  Now the GPS system was designed for both time and position determination and is currently (2002) the best system for time transfer.  See my Time and Frequency web page for more on time

Surverying has to do with determining positions on Earth. Many aspects of astronomy have a strong relation to time and position.


Once you know where you are, you still need to know in what direction lies your goal.  Even today with a GPS receiver that tells your position, you still need a compass to determine direction.  You can determine direction with GPS by taking a reading then moving to another location and computing the direction you traveled, but the GPS receiver when at rest does not provide any bearing information.

Accuracy of Visual Fixes

Going back well before the chronometer there were pendulum clocks that keep good time when placed on a solid foundation.  Although they are limited because of changes in gravity caused by the Sun and Moon (Wiki: Earth tides).  The pendulum clock can be set by observing the Sun and stars and so can be used to determine Longitude on land when combined with a transit or theodolite.  The accuracy of the position depends on the accuracy of the time and the pointing accuracy of the theodolite.

The British Longitude Prize (Wiki) did not specify the method but rather offered 3 prizes where the amount paid depended on the accuracy.  The range was 60, 40 or 30 nautical miles.  These distances are related to the distance between the lookout at the top of the main mast on a sailing ship and the peak of a mountain on land.  The idea was to keep ships from running aground which typically killed all on board.  Harrison (Wiki) won the prize be developing a balance wheel chronometer (Wiki) because the pendulum clock does not work on a ship.  The basis of  determining the longitude at sea at that time depended on knowing the time to enough accuracy.

When surveying on land your position can be determined using a theodolite and a source of accurate time.  But an efficient system would match the accuracy of the angle measuring instrument and the accuracy of the time.

The Earth makes one revolution around it's axis in about 24 hours (about 86,400 seconds Wiki).  Prior to 1967 the period of the Earth was exactly 86,400 seconds, but after that time defined based on a Cesium standard (see my FTS4060 & FTS4065 web page).  The Earth speeds up or slows down on a daily basis but the Cesium clock keeps much better time.  One revolution of the Earth is equivalent to a change in longitude of 360 degrees.  So we have a relationship between time and angle.
Unfortunately the units of time and angle are the same for minutes and seconds so for angle measurements I'll prefix the unit with arc, like: arc minutes (am) and arc seconds (as).

When using microwave radio frequencies (like the GPS system) or instrumented laser range finding to the Moon or some GPS satellites there is no "seeing" problem and so the accuracy can be much better than for visual methods.

Because of the relationship between time, angle and distance you can see what accuracy you need.  For example if using an instrument with one arc minute of angle accuracy you need a time standard good for about 4 seconds (one second would be great), but for a one arc second theodolite you need maybe 50 milliseconds time accuracy.

It's my understanding that there are a handful of stars (the brightest celestial (Wiki) navigation stars (Wiki)).  These are the brightest stars, those with the highest magnitude.

24 h
360 d1
40,030.230141 km
24,873.5821 mi
1 h2
15 d2
1667 km
1036 mi
4 m
1 d
1.195 km
69.09 mi
1 m
15 am
27.799 km
17.273 mi
3.999457 s
0.999864 am
1 nmi3
1853 m
6076.12 ft
4 s
1 am4
1853.25 m
1.151 mi
1 s
15 as
463.313 m
1520  ft
200 ms
3 as5
92.663 m
304 ft
100 ms
1.5 as
46.331 m
152 ft
66 ms
1.0 as6
 30.888 m
101.3 ft
10 ms
0.15 as
4.633 m
15.2 ft
6.6 ms
0.1 as7
3.089 m
10.13 ft

Note: 0: distance along  Equator (latitude = 0) (Wiki) , other constant latitude reduce by COS(|Lat|) or along great circle through both poles (use number in table).
Note 1: One revolution of the Earth, the speed at the equator is 1667 km/hr, 1036 MPH.
Note 2:  Nominal width of a time zone (Wiki)
Note 3: A Nautical mile (Wiki) is very close to one arc minute of angle.
Note 4: One arc minute is the accuracy of the Wild T16 theodolite which is about the same accuracy as the Leitz 115 transit.
Note 5: "Seeing" (Wiki), which varies with time, but on average puts a limit on the accuracy of any visual observation from Earth of about 3 as. (See: Stellar Time)
Note 6: One arc second is the accuracy of the Wild T2 theodolite (requires good seeing to be useful).
Note 7: A tenth of an arc second is the accuracy of the Wild T4 theodolite but that accuracy is used when observing ground based targets, not astronomical sights.


One of the classical uses of gyroscopes is in aircraft instruments and control systems.  The first inertial navigation systems used gyroscopic stabilized platforms and today modern flight control systems also use gyroscopes.  In all these cases the gyroscope is used for relatively short times.

A gyroscope can also be used to determine true North.  For example a surveyor inside a cave can use a North finding instrument that does not depend on sighting the Sun or stars yet produces a very precise horizontal angle "fix". The AG8 is the military nomenclature for one of these systems.

Note the drift rate of a gyroscope, independently of how it works, depends on it's volume.  The gyros on a chip are extremely small and drift quickly.  The huge spinning mass gyros have a much slower drift rate.


Inertial navigation depends on Sensors for orientation.  A classical system uses a three degree of freedom gyroscopic platform with accelerometers in each axis.  More modern systems use strap down fiber optic laser gyros.  The problem is drift.  If an inertial system is just placed in a static location and the position plotted for some time it will drift.  That means that the precision of the "fix" gets poorer and poorer as time goes by.  Inertial systems need periodic updates using some other method.  The Transit satellite navigation system was designed so Polaris missile subs could update their inertial nav system.

These systems are typically large and expensive and so you'll find them on large high value vehicles although I have seen that the military has a system that can be mounted in a jeep.




There are 3 types. 
The degree dial can be rotated.  One application would be to set it to the local magnetic deviation.  Dial in both degrees (red) and mils (black).

1) This one that has the glow in the dark paint Marked:
U.S. Compass, Magnetic
FSN: 6605-151-6337
RA Miller Elec.  Corp.
Grand Haven, Mich.
30 Jun 71

2) the one with Trintium (Wiki) vials that glow all the time.   Marked:
U.S. Compass, Magnetic
NSN: 6605-01-196-6971 Stocker & Yale  120 mCi (millicuries of tritium)
NSN: 6605-01-196-6971 Stocker & Yale U.S.
                    Compass, Magnetic
NSN: 6605-01-196-6971 Stocker & Yale U.S.
                    Compass, Magnetic
NSN 6605-01-196-6971
NSN: 6605-01-196-6971 Stocker & Yale U.S.
                    Compass, Magnetic
SandY 183
120 mCi 3H

NSN: 6605-01-196-6971 3H Cammenga (probably 120 mCi).  comes in OD, Black or Camo.

3) a version of the Trintium compass for Japan with a smaller amount of Trintium.
3HJP  with 27 mCi

                    Compass 1971 U.S. Army Marked:
FSN 6605-151-5337
RA Miller Elec. Corp.
Grand Haven, Mich.
30 Jun 71

2111829 Orientation Compass, F. Winterer, Mar 22, 1938, 33/272; 33/285
2487044 Compass, W.C. Cude (US Army), Nov 8 1949, 33/348; 33/345; 33/349; 33/354; 33/357 -
2003179 Magnetic Compass, H.T. Faus (GE), May 28 1935, 33/345; 33/355.00R; 318/466; 318/647; D10/68 -

M2 (Brunton)

M2 Pocket Transit

This is a very high quality compass and inclinometer.  There are two versions of the dial, one is in degrees and the other is in Mils.  Which is the military degree measurement used for artillery, it is equivalent to 1 yard at a range of 1,000 yards.  For most compass uses the degree version is much more useful, but all the military M2 compasses are in Mils.  Mils is for milli radians (Wiki). 1 yard offset at 1,000 yards is 1 mil (NATO).

The degree dial can be rotated relative to the compass body.  On mine, shown above, I've offset the dial my the local magnetic variation (Wiki).  That way when the North pointer is at zero the compass is pointing to True North rather than Magnetic North.

Although you can still buy this from Brunton in a number of different sizes it was originally patented by Brunton:

  526021 Pocket-transit, David W. Brunton, Sep 18, 1894, 356/142 ; 33/285; 356/147 -
1042079 Transit, David W Brunton Oct 22, 1912, 33/272, 356/143 -
1062582 Transit, David W Brunton, May 27, 1913, 33/272
1092822 Sight for transits and similar instruments, David W Brunton, Apr 14, 1914, 356/143, 356/142, 356/147
and later a version was patented by K&E
1571697   Transit, Bernegau Carl M (Keuffel & Esser Co), Feb 2 1926,  33/273, 33/352
There are a large number of replica "Brass" versions now for sale, who knows if they are even functional.
The M2 was/is used to setup artillery, mortar and other sites where you need a good magnetic bearing and also for rough field survey work.

1223615 Pocket Surveying Instrument, R.W. Richards, Apr 24 1917, 56/143 -
1339019 Illuminated Transit, D.W. Brunton, May 4 1920, 40/542; 33/285; 250/462.1 -
4395828 Combination geodetic transit compass and signal mirror, Allan P. Juhas, Aug 2, 1983,


Sperry Gyroscope Creagh Osborne Marching Compass MKVII  Mod. E

(United States Engineering Department)
Marching Compass
 MKVII  Mod. E
Sperry Gyroscope Co.
Brooklyn, N.Y.

1216953 Magnetic Compass, F.O. Creagh-Osboren & A.J. Hughes, Feb 20 1917, 33/348; 33/364; 250/462.1; 359/441; 362/29 -
1256442 Magnetic Compass, F.O. Creagh-Osboren & A.J. Hughes,Feb 12 1918, 33/350; 33/357; 33/364 -

MC-1 Magnetic Compass Flight line Calibration Set

Works with 400 Hz "Y" connected synchro type sensors and indicators as used in aircraft.
Flux Valve is the name associated with the sensors.


The surveying transit evolved from a compass coupled to a telescope.  Almost all transits have a compass built in so that magnetic North can be indicated and true North can then be determined. Leitz 115A Transit

Wrist Computer

Vector by Suunto - contains clock with time, date, alarms, magnetic compass, barametric pressure & altitude as well as temperature.

3 Axis Earth's Field

info wanted on this unit

Type 1811-1-B Aircraft Flux Gate Compass

            Instrument Type 1811-1-B Aircraft Compass

2188821 Compass, Bendix Aviation, Jan 30, 1940, 362/30; 33/348; 246/1.00C; 385/147 - illumination Looks like Type 188-1-B
1939374 Liquid Compass, A. Urfer (Pioneer Instrument Co), Dec 12, 1933, 33/364 - allow for expansion/contraction of fluid.
1679764 Magnetic Compass,  C.H. Colvin (Pioneer Instrument Co), Aug 7 1928, 33/364 - improved magnetic element
1334273 Magnetic Compass,  C.H. Colvin, Mar 16 1920, 33/364 - readable from side or top for aircraft use
1983103 Magnetic Compass, C.L. Seward Jr (Bendix Aviation), Dec 4, 1934, 248/638; 33/350 - aircraft shock absorbing and keeping the card from spinning
1873684 Compass, A. Urfer (Pioneer Instrument Co), Aug 23 1932, 33/348; 33/555; 246/1.00C; 385/147 - light pipe to liquid aircraft compass
2008475 Spring Mounting, G. Spiller (Bendix Aviation), Jul 16, 1935, - aircraft use pivot pin support
1910092 Instrument Cover Glass, C.H. Colvin (Pioneer Instrument Co), May 23, 1933, 362/23; 33/364; 359/601 - old convex glass reflects light
2008481 Magnetic Compass, P.F. Weber, W.E. Dankau (Bendix Aviation), Jul 16, 1935, 33/364 -
2127807 Indicating Instrument, V.E. Carbonara (Bendix Aviation), Aug 23, 1938, 116/287; 33/348; 116/299; 359/440 -
1596639 COmpass for Navigation Purposes, R. Vion, Aug 17, 1926, 33/359; 324/244 -

Aircraft Standby Compass

Aircraft Pilot's
              Standby Magnetic Compass

Earth Induction Compass (Wiki)

1047157 Device for Determining Direction, D.M. Bliss, Dec 17, 1912, 33/362; 324/257 - The Earth provides the magnetic filed and a rotating coil (could be powered by the air going past an airplane) generates a voltage that depends on the relative heading of the plane.
US2434324 Earth Inductor Compass, H. Ledhe, Jan 13, 1948, 33/362; 318/647 -  crystals vibrating to move sense coils



By manually sighting a star or the Sun the direction of true North can be determined.  This instrument was typically used in aircraft and was held in a "bubble"aka dome  requiring the optical distortion effects of the bubble to be corrected.

Periscopic Sextant

The periscope was mounted in a hole in the top of the plane and was out in the outside air.  It thus did not require any "bubble" correction and was much easier to use.  A huge improvement over the classical nautical sextant (Wiki) is the inclusion of a clockwork averager that makes the resulting elevation measurement more accurate.

Automatic Astro-Compass

This unit has a star tracker assembly with its own glass "bubble" and is pressurized, probably with dry Nitrogen, to prevent fogging of the optics.  It has a larger prism at the objective end than the periscopic sextant, probably to gather more light for the photomultiplier tubes that detect the star.  This model may not be able to track stars in the daytime, but later version could.

Transit Surveying Instruments

For centuries surveyors have used the Sun and stars to determine true North.  To do this there are attachments for transits to allow imaging the Sun without damage to the users eye(s).

Leitz 115A Engineers Transit  uses the older 3" x 8 thread tripod

K&E Hand Level

This is a very early square tube unit with no optics except for a first surface mirror to view the bubble from the bottom.  I think is was build is such a way as to avoid the Locke patent 7477 hand level that K&E later offered after the patent ran out.

T. F. Randolph Level

Compact tripod mounted leveling scope with cross hairs and spirit level, with 1884 patent 297164 date. In a patented seamless leather box.


These instruments are similar to a surveyors transit except instead of mounting on a tripod they are held by a ruler.  There is no horizontal angle measuring ability, instead a ruler parallel to the line os sight is used to draw a line on the map directly in the field.  The method of Stadia is used to determine the distance to the rod.  This was the primary tool used in the U.S. to make topo maps for many years.

K&E 76 0000 Alidade - self indexing (auto leveling) and built in trig for horizontal and vertical distance based on stadia reading.

Photographic Zenith Tube (PZT)

A pool of Mercury used as a reflector so scope points straight up.  Photographic glass plates exposed four times and after developing read out on a type of coordinate measuring machine to learn the local clock error to within fractions of a second.

Replaced by the Danjon Astrolab.  An instrument that measures the time when a star crosses a number of meridians that are at an angle, not necessarily the local meridian.  The idea being to make more measurements on stars that are more convenient to measure.

StellarTime Measuring the Time for the Earth to make one  Turn.

Abram's Sun Compass

This is a Sundial that has been designed to find North when the time and location is known. It will work when mounted on vehicles and tanks whose ferrous metal content renders a normal magnetic compass useless. eBay photo
TM5-9422 Compass Universal type Abrams SC-1
BTO/3/91 may be the UK patent
It's fundamently a pole that's plumb and the tip of it's shadow falls on a flat metal plate (circular bubble level vial on plate).

Dent Meridian Instrument - Dipleidscope

Used to establish the time of meridian passage of the Sun or a star.

Chinese Sun Dial and Compass

Sextant, Aircraft



A-10A Bubble sextant used by Army Air corps Navigator in B25s during WW2



The Sun has been used to find compass directions back as far as recorded history.  There are many way this can be done with a considerable variation in the precision of the resulting "fix".  See also my Sundials web page.

Pilot Balloon Observation (Pibal) Theodolites (mirror web site)

These theodolites are used to track balloons as they rise for learning about the speed and direction of the winds aloft.
These might be a good choice for finding true North since with most designs you look in a horizontal direction and the scope objective points up using a rotary joint.
With a classical transit or theodolite it's almost impossible to look at something at a high angle since the eyepiece goes inside the base of the instrument.


1446574 Nephoscope, Mcadie Alexander, May 19, 1921, 33/284, 356/27, 33/1.00R - to track cloud movements
1743979 Sextant, Lawrence Radfordi (K&E), Feb 12, 1927, 356/146, 356/148, 362/23.1 -
1967541 Balloon theodolite, Schoute Cornelius (Zeiss Carl Fa), Mar 23, 1931, 356/251, 33/274 - classical horizontal viewing port
2651560 Observing apparatus, particularly for observing objects moving in space, Alfred Gerber (Contraves Ag), Jul 5, 1945 -

Stellar Time Keeping

Similar in concept to the Automatic Astro Compass, but instead of tracking a single known star a scanner looks at the star field and figures out either where it is or what time it is.  Was looking for information on the Danjon Astrolabe, but so far have not found any info on how it works.



This was a system operating in the frequency range around 10 to 15 kHz.  Ships at sea could keep track of their position in a "lane" defined by the phase of the signal.  System became obsolete with the deployment of GPS.


Radio Receiving Set AN/TRQ-23

Army field set for getting DF bearings covering the HF, VHF and UHF frequency ranges.  Uses antennas rotating up to 150 RPM and a CRT display.  Will provide a bearing even with a very short transmission.


38 - 55.4 MHz DF Loop Antenna


This is an H.F. radio receiver with a loop and sense vertical antenna system designed to determine the bearing to a station.

Non Directional Beacons

These are located on or near airports and send a carrier and single sideband CW ID in the 200 to 400 kHz range.  Aircraft can tune into the carrier and get an indication of the bearing to the station.


Very similar to the ARN-89.
ARM-93 Test set.
LF Automatic Radio Direction Finder Set; manufactured by Collins; used in A-37, C-2, UH-1, AH-1T, VH-3A, OH-6, P-3, S-3, OV-10, U-8F, U-21A


Vietnam era helicopter 100 to 3,000 kHz frequency coverage direction finding receiver. can use NDB, AM broadcast stations or other signals in this requency range.

Light Weight Beacon

Viet Nam era. Transmits a programmable ID on a frequency in the 265 to 535 kHz range and includes a 50 foot antenna with no part longer than 19 inches.  The complete system is in one back pack.  Most likley made for use with the ARN-89.


The post W.W.II Loran-A system operated around 1.8 MHz was replaced with the Loran-C system operating with pulsed signals on 100 kHz.  Maybe Loran-B was an idea that never was made operational?  There are a number of "chains" consisting of 3 to 5 stations with all the stations in a chain using the same Group Repetition Interval (GRI).   If a scope is triggered from a GRI generator the stations is that chain will appear as pulses with different fixed times on the horizontal axis while the pulses from stations using other GRI values will be jumping around.  Until GPS this was the most accurate system for positioning and for time transfer. 
2005 - It looks like Loran-C will be used for aviation safety providing a redundant system to support automatic landings.  Other systems like the Russian or European equivalent to GPS are not good candidates because a jammer for GPS would also take them out.

The U.S. LORAN-C system was shut down on 08 Feb 2010.
March 2012 - there is some LORAN-C acitivity in a test phase for an alternate to GPS for critical timing applications.

Table of Loarn-C Chain Stations -

Loran Patents 

Micrologic SportNav with MGRS

This hand held unit was for use in the Operation Desert Storm/Shield area by the U.S. military.


This is designed to attach to either a PRC-25 or PRC-77 back pack VHF low band transmitter receiver and report position via radio.  Also receives Loran-D which must be a temporary system that the military could put in place.
Austron 2100F LORAN-C Frequency Monitor - for precise Frequency
Austron 2100T LORAN-C Timing Receiver - for precise time
Austron 2042 LORAN-C Simulator -
Lorchron LORAN-C Timing Receiver LFT-504 - for precise timing
TI 9100 Aircraft Receiver


When Sputnik was launched in 1962 the Doppler signal was used by scientists at Princeton to determine the orbital parameters of the satellite.  They quickly realized that if a satellite was to transmit its orbital parameters then a person on the Earth could determine their position.  This was the basis for the Transit Satellite Navigation System. 


There were only a small number of satellites transmitting on 150 and 400 MHz.  A submarine whose inertial navigation system had drifted could receive the Transit pass which took maybe 15 to 30 minutes and then update their inertial system.  This system required a very high quality = expensive (atomic) clock.  When the GPS system was being developed one of the parameters was to eliminate the need for an expensive clock.
A 120 to 170 MHz eggbeater antenna would allow reception of the Transit signal on a vehicle.

"The modulation of the satellite signals was recovered in the AN/BRN-3 from whichever channel (150 or 400 MHz) was being received with the best SNR. The modulation provided 6103 bits of information every 2 min ( 50.85 bits per second) and a beep-time index every 2 min, decomposed into 156 words of 39 bits."

33 or 39 bits?

MX 4102 Satellite Navigation receiver by Magnavox

Johns Hopkins Applied Physics Lab Technical Digest January-March 1998, Volume 19, Number 1 - Transit

3172108 Method of navigation, Frank T McClure, 342/451, 701/469
                TRANSIT navigation system.

Propulsion engine with electromagnetic means to produce propellant acceleration, Kunen Alfred E, Republic Aviation Corp, May 28, 1963
Pulsed Plasma thrusters with 14 year life based on Teflon as fuel and Magneto Hydro Dynamic drive.

3529291 Synchronized sequence detector Claude W Brown (China Lake, US Navy), Dec 4, 1967,
                33 bit Barker Code Receiver (Wiki)


The GPS system has about 24 satellites in medium orbits (they are lower than geostationary) orbiting the Earth in three rings.
They transmit their orbital parameters.  By receiving the signals from four satellites a GPS receiver can figure out where it is and also the error in its clock.  If the receiver is in a known location only one GPS satellite is needed to know the time.  If more than 4 satellites are received the quality of the position fix imporves.  It may be that 1/2 of the satellites are visable at a time and that's why there are twelve channel receivers.

Stanford Telecom 5001A Navstar Test Transmitter

In order to test GPS receivers before any satellites were in orbit, Stanford Telecomunications built a small number of GPS transmitters.  They later made custom chips for military GPS receivers.
I have heard from a former STI imployee that these receivers were used to debug the large scale ICs STI made for GPS receivers.  In particular channel to channel timing skew.
AN/URN-502 Canadian Military GPS
This, large by today's standards, GPS receiver was built using different printed circuit boards for different functions and an OEM GPS receiver board made in Japan.
PSN-8 GPS receiver

Quantic Q5200/SM

This GPS Timing receiver was designed for military GPS timing and uses a couple of the Stanford Telecomunications GPS chips.  Needs a down converting antenna, if you know about the antenna, please let me know.
Garmin GPS III+
This hand held 12 channel GPS unit has a built in World map and bread crumb trail capability.  It can also average Lat and Lon but NOT altitude, mine is up to 3,051,294 averages today, and can go to 99,999,999.  This will taks some time becasue the readings are one per second. It took about 35 days to get this far. I would take over 3 years to run out the counter.
Motorola GPS Oncore VP
These are 8 channel general purpose OEM receiver boards that I have in the evaluation version boxes.  They have timing accuracy in the 30 nS area when used in the known position mode where all the variables are applied to getting a good 1 Pulse Per Second.  Unfortunately they have been discontinued and there is not a replacement with the same verycomprehensive capability. Synergy is where I purchased my VP+ units.
Motorola M12+ Timing
If the M12 has the same Motorola binary format differential correction output that is in the VP series (I most probably does) then it should be possible to place the antenna at a know location and using some math save the corrections for each satellite.  Then switch to rover mode and have those same corrections fed back into the receiver to correct it.  This is covered in a CSI patent, but they don't offer it in this format.  Note this is much different than "poor man's differential correction" since actual corrections are being made for each satellite, not just a Lat and Lon position correction.  The key limitation is the time from obtaining the differential correction and the time that most of the satellites set.  Note that GPS sats have a nominal 12 hour orbit so maybe 4 hours overhead.

PLGR Family

 - follow on after the Trimpacks, is a large hand held unit.

DAGR Family

Trimpack Family

p/n 14992-20 & 16768-20 AN/PSN-10 SLGR, Came out just in time for Desert Storm & Desert Shield, gulf wars.  Since these were L1 CA code receivers L1 was turned off for the Gulf wars, Desert Storm and Desert Shield.  Many of these can average Lat, Lon and altitude

GSM-336 GPS Test Set

 (@BPB Surplus) Anyone have info on what this set does?
 TM 11-4920-297-12 Opertion and Maintenance Intermediate for
Navigation Set Test AN/GSM-336(V)1, 685-7539-001, (NSN 6625-01-319-7118),
Navigation Test Set AN/GSM-336(V)2, 685-7540-001, (6625-01-294-1941),
Navigation Test Set AN/GSM-336(V)3, 685-7541-001, (6625-01-317-4851)
 {TO 33D7-71-51-1; NAVAIR 16-30GSM336-1}

TM 11-4920-297-12P Illustrated Parts Breakdown for
Navigation Test Set AN/GSM- (NSN 6625-01-319-7118), 685-7539-001,
Navigation Test Set AN/GSM-336(V)2, (6625-01-294-1941), 685-7540-001,
Navigation Test Set AN/GSM-336(V)4, (6625-01-347-1757), 685-7540-020,
Navigation Test Set AN/GSM-336(V)3, (6625-01-317-4851), 685-7541-001
{TO 33D7-71-51-4; NAVAIR 16-30GSM336-2}


Surveying Patents -
GPS patents
Army Space Reference Text - 7-26  Characteristics of an Ideal Pos/Nav System -
" - same thing at FAS with proper formatting
Navigation mailing list -
American Society for Photogrammetry & Remote Sensing - Grids & Datums -
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