MX 4102 Transit Satellite
Navigator
MX 4200D Differential GPS
MX 4102
Background
When Sputnik was put into orbit in 1957 some
scientists at the Johns Hopkins Applied Physics Lab came up
with the idea of using the Doppler shift measured on the
ground to solve for the 3 dimensional position of the
receiver. This required a satellite that transmits it's
orbital elements. There are a number of papers on the
JHAPL Legacy
of Transit web page. The Navy Navigation Satellite
System, as it was officially known, was designed mainly to
allow the inertial navigation system on Polaris nuclear subs
to be updated.
The very first Transit receiver took up about a dozen six foot
high rack cabinets. The
receiver for the Polaris sub was in two cabinets designed to
fit through the hatch and so were narrower than a normal relay
rack. The transistor had just come out and integrated
circuits were non existent when the Transit satellite system
went into operation. By the time Magnavox built the MX
4102 integrated circuits were common, hence it's small size
and much lower price than the very expensive early Transit
receivers.
The MX 4102 was designed by Magnavox, Torrence, CA (now Leica Geosystems Group)
for use on pleasure boats and since there can be a number of
hours between Transit fixes it includes dead reckoning to keep
the position updated. This requires external compass and
speed inputs from any number of the common types of sensors
used abroad ships and the appropriate interface options for
the MX 4102.
The MX 4102 uses a oven controlled oscillator (OCO) marked:
Electronic Research Company
Model EROS 800-MA-97
Mfg. p/n 626358-1 B
Freq 5.00 MHz
s/n 11703
Date 89-17
This is oscillator has a short term stability of 1E-10,
equivalent to rack mounted lab type standard
oscillators. A high stability oscillator is needed to
measure the Doppler curve and to set the receiver tuning
offset to account for the Doppler shift of the carrier on the
low orbiting Transit satellites.
Other Models:
Model
|
System
|
MX1102
|
400 MHz Transit
|
MX1105
|
Omega
|
MX1107
|
150 & 400 MHz
Transit
|
MX1112
|
400 MHz Transit +
features
|
MX1157
|
150/400 Transit &
Omega
|
|
|
|
|
Manuals
The Navigator's Manual and the Installation and
Service Manual are dated June 1989.
Power
The unit operates from 10 to 30 Volt Dc power with
positive going through the fuse. the current is just
over 1 amp at a cold start and decreases to about 0.8 amps
after the oscillator oven has warmed up.
Operation
By setting the approximate position, date and time
by pressing INIT repeatedly the receiver can start searching
for signals. When the signal strength at 400 Mhz gets
above some threshold the receiver starts looking for the
digital modulation. Now when there is no active
satellite or I don't have a high enough antenna gain the
receiver beeps and displays no fix (NFX). Apparently
this receiver does not use the signal at 150 Mhz, only the 400
Mhz signal. This means that the corrections for
ionosphere refraction are either approximated or not used.
The front panel has a Vacuum Fluorescent Display (VFD) with
buttons below and to the right so the VFD can act as a menu
system. In addition there are a couple of membrane
keyboards, one with specific labels related to functions and
the other with digits for numerical input.
Satellites
On 1 Jan. 1997 all the Transit satellites were
turned over to the Navy Ionospheric Monitoring System (NIMS)
and no longer use the Transit data modulation. Instead
they now use a different modulation that's a classified NIMS
format. These satellites are in a fairly high orbit and
will stay there for a very long time, i.e. they will not decay
and fall to Earth like a low orbiting satellite. But
they are all now very old and so will cease to operate
electrically when failures take them off the air.
The primary navigation frequencies are 149.985 and 399.970 and
telemetry on 136.650 MHz.
MX 4200D Differential GPS Receiver
Got a group of these on eBay and
a number of the power supplies for a low price on eBay.
The power supply puts out 12 VDC @ up to 1 Amp and may consume
up to 25 Watts.
The receiver puts out a little more than 5 VDC to the antenna
so connected it to my house antenna and after some hours (was
not paying attention) the Green LED was blinking. If the
antenna is disconnected the green LED turns off and the Yellow
LED comes on with no blink. Also, for no apparent
reason, the green LED turns off and the Yellow LED comes on.
The Magnavox MX-50R DGPS beacon receiver could have it's
output fed into the GPS receiver to mitigate the effects of
SA.
The rear panel uses a Type-F jack for the antenna connection
and a DB-25F connector for the remote interface. There's
a 1A Fuse and a switch marked Off On Remote.
A plugged hole is labeled 1 PPS Output and there's a ground
post. On the side is a flourescent orange sticker saying
Year 2000, In Process 2 Feb 99 - Maybe they found a problem?
The label on the rear panel:
Magnavox
Part No.: 707361-803 (the dash number is hand written), Serial
No.: 751, Power: % Watts 10-36 VDC, Made in U.S.A.
The DB-25F connector is labeled "Multiport Interface" implying
that there are two or more data I/O ports, i.e. Differential
corrections are input and a position/Velocity/Time data stream
is output and maybe a control input on the one or both of
these.
After being powered up for a few days the green LED is mostly
on, but blinks occasionally. There may be some type of
code associated with the green LED.
If you have any information about these GPS receivers
let me know.
Versions
MX 4200D - 6 channel
MX 9212 DGPS -12 channel
MX4818 - ? channels
25 Pin D_Sub Connector
Pin
|
Description
|
|
|
1
|
Remout
On (-)
|
|
|
2
|
Port
2 Out (+)
|
RS-422
|
Raw
Data
|
3
|
Port
2 Out (+)
|
RS-422 |
Raw
Data
|
4
|
Port
4 In (+)
|
RS-422 |
NMEA-0183
|
5
|
Port
4 Out (+)
|
RS-422 |
NMEA-0183 |
6
|
Port
3 In
|
RS-232 |
DGPS
|
7
|
Port
3 Gnd
|
|
|
8
|
Port
3 Out
|
RS-232 |
DGPS
|
9
|
|
|
|
10
|
Port
1 In
|
RS-232
|
Ctrl
Msg
|
11
|
Port
1 Out
|
RS-232 |
Ctrl
Msg |
12
|
Ext
Pwr Rtn
|
|
|
13
|
Ext
Pwr 12 V (+)
|
|
|
14
|
Port
2 In (-)
|
RS-422 |
n.a.
|
15
|
Port
2 Out (-)
|
RS-422 |
n.a.
|
16
|
Port
4 In (-)
|
RS-422 |
NMEA-0183 |
17
|
Port
4 Out (-)
|
RS-422 |
NMEA-0183 |
18
|
|
|
|
19
|
|
|
|
20
|
Event
In
|
|
|
21
|
Event
Rtn
|
|
|
22
|
|
|
|
23
|
|
|
|
24
|
Port
1 Gnd
|
|
|
25
|
Remote
On (+)
|
|
|
Panel Lights
Red - Power On
Yellow - Passed Self Test - Starting to operate
Green Flashing - receiving one or more stations
Green steady - navigating
Normal operation involves cycling between yellow, green
flashing and green steady
Transit Patents
2470787
System for determining the position or path of an object in
space, Paul
W Nosker, App: 1944-05-04, Secret, Pub: 1949-05-24, -
for locating aircraft, cited
by 54 patents, many of which have application dates
prior to Sputnik.
3063048
Discovery and location system, Frank
W Lehan, Glenn
L Brown, Space-General
Corp, 1962-11-06, -
3133352
Satellite alert,
Robert E Jasperson, 1964-05-19, - visibility
prediction calculator for low orbit satellites, see: Flight
Computer
3141167
Navigation system, Peter
C Sandretto, ITT,
App: 1959-12-07, Pub: 1964-07-14, - The idea of a satellite
and using Doppler in the receiver, not Transit details.
3172108 Method of navigation,
Frank
T Mcclure, Navy, 1965-03-02, - 150 MHz, 96 min
satellite orbit,
3191176 Method of navigation,
William
H Guier, Navy, 1965-06-22, - 2 minute data
frame, 400 & 150 MHz,
3209357
Hyperbolic position determination, Wyatt
Theodore, 1965-09-28, -
3233362
Toy satellite with radio signal generating means, Ralph
R Chapman, App: 1961-12-19, Pub: 1966-02-08, - one
transistor AM Tx.
3369236
Navigational receiver, Edwin
E Westerfield, Jerry
R Norton, Lauren
J Rueger, Malcolm
B Greenlee, Navy,
1968-02-13, - improvement over star trackers that only work
in good weather (see: MD1). Includes getting accurate
time signal from satellite. one aspect of a TRANSIT
receiver
3534378
Wide band antenna for satellite navigation and related
problems, Valor
C Smith Jr, Chu
Associates, 1970-10-13, - 150 & 400 MHz with
pattern matches to satellites in the sky
4232389 Receiver for
satellite navigational positioning system, Roger
D. Loiler, JMR
Instruments, 1980-11-04, - "...derives the actual
satellite clock directly from one of the radio frequency
carriers, rather than deriving the synthesized clock from
the demodulation products of the carrier, and its recovery
process is not dependent upon a local clock. Through the
technique of the present invention, the effects of long term
drift of the local receiver oscillator, and detector signal
to-noise ratio errors, and other sources of error in the
extraction of the two-minute time interval information from
the received satellite signals are eliminated. Any drift in
the oscillator of the satellite is recorded by the United
States Naval Observatory, and is contained in the
transmitted satellite signals. This enables the receiver to
make appropriate corrections for drifts in the satellite
clocks." patent includes many details of Transit signal.
Links
MX Marine,
Leica Geosystems Group - offers GPS, DGPS equipment for ships
Hearsat - an orginazation
with a mailing list for those listening to satellite signals,
NIMS
Center for Ionospheric Research U of Texas- Transit
Satellites -
HAARP - Slant-path
Total
Electron Content and Scintillation based on Transit
Satellites using Northwest
Research Associates, ITS10 Transit
receivers.
Transit
5B-5
der wahrscheinlich älteste aktive Satellit - BableFish
Translation - even without translation you can read the
frequencies and see the images.
YouTube: Magnavox
MX 1112 Satellite Navigator 1980 SatNav 400MHz, 40:45 -