by Monte L. Stuck
Assembly Room, A. K. Smiley Public Library
January 7, 2010
There I was at 40,000 feet in a United States Air Force flight suit, helmet and oxygen mask. We were headed east over the Atlantic, and it
was dark. I was part of the 6-man crew aboard a B-52 bomber of the Strategic Air Command, loaded with nuclear weapons. I was the navigator. And I knew
where we were. I had just plotted a good three-star position fix, so I had a little time to relax --- and I began to think about the people who
developed the science of navigation which allowed the six of us to fly into the night with such solid confidence. Confidence that we would safely reach
our appointed destination --- on target and on time.
“At this time, in the early 1960s, the Strategic Air Command had control of more than 2,000 nuclear-laden bombers. Along with the bombers,
there were large fleets of in-flight refueling tankers. Both of these aircraft fleets required navigators and/or navigator-bombardiers.” [1]
“During the Second World War, the Army Air Force trained more than 45,000 navigators and 50,000 bombardiers.” [2] And anyone trained by the Air Force as a navigator knew how this science developed.
While the basic definition of navigation is “the art of finding the way from one place to another,” most early navigation was not
navigation at all in the true sense of the word, but piloting.
Early mariners used piloting, the practice of remaining close to shore so they could use geographic landmarks such as prominent rocks and
cliffs to guide them. True navigation skills came into play when these mariners ventured into open water away from sight of shore. “The Greeks and
Phoenicians made great strides in navigation and developed techniques that remained in use for thousands of years. By some accounts, the Phoenicians
were the first to use the Pole star --- Polaris --- for maritime navigation and the first to circumnavigate Africa. Polaris, which remains fixed above
the North Pole, was critical for early navigation because it allowed navigators in the Northern Hemisphere to gauge their latitude by measuring its
height.”[3]
Many times as a navigator I would use Polaris as an excellent latitude check. If the sextant read a height of 35 degrees 20 minutes, you
were at latitude 35 degrees 20 minutes --- give or take a mile or so for the wobble of the earth around its axis.
Perhaps the best of the early navigators were the Pacific Islanders who navigated thousands of miles between islands by using their
intimate knowledge of the effect of the various winds --- which they gave specific names for their direction and force --- along with the sea currents,
and migrating seabirds.
They also developed extensive star charts using the bearing of selected stars to guide them to their destinations --- these stars were
usually named the same as the islands they sought. Of course, one wonders how many of these trips were unsuccessful. An unexpected storm taking those
navigators more than a dozen miles off course on a 2200- mile voyage would result in their passing by their destination unobserved.
The first piece of technical equipment to aid the early navigator was the magnetized needle compass “first used in China in 1100; and then
appeared in Europe eight or nine decades later.” [4] Sir Francis Bacon, the renaissance author of the
1600s, wrote that the three greatest innovations of change in the world until that time were gunpowder, the printing press, and the compass. A slightly
refined version of the Chinese magnet of 900 years ago, hanging on a silk thread, is a part of every military aircraft’s instrument package today. It
is nicknamed the “whiskey compass,” because its magnetized compass card floats in a small enclosed container of alcohol. Today in an aircraft, if all
electrical power fails, and all other electronic navigation aids are useless, the whisky compass can always point the way home.
Just a side note: early mariners had some problems with this simple “compass thing” because it did not always point at the Pole Star. This
is because they didn’t understand that earth’s magnetic north pole is not exactly at the actual North Pole. It lies in northern Canada at approximately
74 degrees north latitude --- about 1000 miles from true North Pole. And while there was little variation between true north and magnetic north
throughout the Greek’s and Phoenicians’ Mediterranean, the difference at the tip of Africa was significant: up to 30 degrees variation, which also
changed year-to-year because the Earth’s magnetic field shifts over time.
So while other tools of navigation were practically non-existent for hundreds of years to mariners plying the earth’s waters, sail them
they did.
“Half a century ago, most schoolchildren were taught that Christopher Columbus discovered America while searching for a shorter route to
India and that he accomplished this remarkable feat because he was one of few people who understood that the earth was round. He simply blindly sailed
west, not fearing that he would fall off the flat world. As Samuel Morrison points out in his Pulitzer Prize-winning ‘Admiral of the OceanSea,’
however, no capable sea captain of Columbus’ era thought the earth was flat, and Columbus was a capable captain and an exceptional dead-reckoning
navigator. Celestial navigation was not widely understood, and Columbus’ tools, knowledge, and skills were meager, but he knew how to maintain a track.
He crossed an ocean unknown to him, found his way home, and found his way back again. He kept track of course and speed with a simple compass and a
floating block.” [5]
The floating wood block, commonly called a “chiplog,” was used to estimate the ship’s speed. “This small float was affixed to a “rope
knotted at intervals of 47 and ¼ feet.
Navigators threw the float off the boat and counted the number of knots played out as they sailed on by. “The navigators timed their count,
using a 28-second sandglass to ensure consistency. The number of knots that ran out in 28 seconds equaled the boat’s speed in nautical miles. The term
knot, meaning one nautical mile per hour, originated with the chip log. If the first knot appeared as the sand ran out, the boat’s speed equaled one
nautical mile per hour, or one knot.” [6]
The next navigation advancement of significance after the wide-spread use of the magnetic compass was the slow development of the sextant.
Initially, the sole purpose of the early sextant was to measure the angle of the Pole Star.
Among the first angle measuring devices was the mariner’s quadrant, simply a wood or brass quarter-circle plate marked in degrees from 0 to
90 with a short plumb-bob to establish a vertical line of reference and two fixed sights to aim at Polaris. Columbus probably made use of a quadrant.
A more sophisticated device resembling the quadrant was the astrolabe. The astrolabe had no plumb-bob, but was the plumb-bob itself, having
a circular metal frame hanging from a top ring. A rotatable center arm carried the sighting holes, and when aligned with the star, the angle observed
could be read on the circular metal frame.
A more simple sighting device developed next was the cross-staff, two calibrated sticks resembling a Christian cross. The short arm called
the transom slid up and down on the longer staff so that the star could be sighted over the upper end of the transom while the horizon was aligned with
the bottom edge.
These instruments were in use for more than 250 years, primarily providing the navigator a reasonable estimate of his latitude.
But these sighting instruments had drawbacks: the plumb bob of the quadrant and swinging astrolabe were hard to use on a rolling deck, and
with the cross-staff, the navigator had to look in two directions at once -- at the top of the transom to the star, and at the bottom of the transom to
the horizon. “Thus, toward the end of the 1600s and into the 1700s, the more inventive instrument makers were shifting their focus to optical systems
based on mirrors and prisms that could be used to observe the nighttime celestial bodies.” [7]
“The critical development was made independently and almost simultaneously by John Hadley in England and by Thomas Godfrey, a Philadelphia
glazier, about 1731. The fundamental idea is to use two mirrors to make a doubly reflecting instrument --- the forerunner of the modern sextant.” [8]
The sextant was easy to use: simply swing an index arm holding the index mirror while observing a celestial body until that body appears to
rest on the horizon of the horizon mirror. And since this was now an optical sighting instrument, refinements soon came in the form of sighting scopes
using various optical magnification powers and in filters which enabled direct viewing of the sun, for very accurate measurements.
By this time, astronomers had developed methods of determining longitude from the sun, moon, planets and select stars, but the calculations
and celestial observations were highly dependent on the time at the astronomers’ base of Greenwich, England, or zero degrees longitude designated as
the “Prime Meridian.” “Even some of the best clocks of the early eighteenth century could lose as much as 10 minutes per day, which translates into a
computational error of 150 miles or more.” [9]
One technique used by navigators in the early 1700s to celestially correct their timepieces involved a long and complicated series of
calculations. “Astronomers had developed a method for predicting the angular distance between the moon and the sun, the planets or selected stars.
Using this technique, the navigator at sea could measure the angle between the moon and a celestial body, calculate the time at which the moon and the
celestial body would be precisely at that angular distance and then compare the ship’s chronometer to the time back at the national observatory.
Knowing the correct time, the navigator would now determine longitude.” [10]
The longitude problem was so great to mariners that in 1714 England established a “Board of Longitude,” and offered a reward of 20,000
pounds sterling to whoever could resolve it. In 1764, British clockmaker John Harrison invented the seagoing chronometer which lost less than one
second per day during long sea voyages.
“In 1779, British naval officer and explorer Captain James Cook used Harrison’s chronometer to navigate the globe. When he returned, his
(final) calculations of longitude based on the chronometer proved correct within eight miles. From information he gathered on his voyage, Cook
completed many detailed charts of the world that completely changed the nature of navigation.” [11]
“In 1884, at the height of the British Empire, Greenwich, England, was established as the world’s Prime Meridian. Previously, each major
nation established its own prime meridian and local time; the promulgation of Greenwich Mean Time did away with these, and thus standardized
navigational readings throughout the globe.” [12]
And so it was until the early 1900s. “That century opened with the first transatlantic radio transmission by Marconi in 1901, followed by
the first airplane flight by the Wright Brothers in 1903. These two events would soon become closely linked, in navigational terms. The rapid
acceptance of the airplane necessitated navigational improvements. By the 1920s, the development of radio navigation was underway. Radio direction
finding thus became the standard for aircraft navigation, eliminating the need for celestial techniques.” [13] Except for the military. A direction-giving radio station could always be turned off, or its
signal jammed -- whereas the stars are silent, yet dependable aids.
In 1907, the gyroscopic compass, or gyro compass, was introduced. This heading indicator, once set to any direction and unslaved to a
free-running mode, is unaffected by the Earth’s --- or the plane’s --- magnetic fields. Once set to true north, it always points to true north (give or
take a small amount of instrument precession, which the navigator periodically corrects.
Gyro compasses are universally used today, even now as standard equipment in the smallest civilian aircraft. The last thing prior to
take-off even a Cessna 150 pilot does is quickly set and unslave the gyrocompass to runway heading before advancing the throttle.
An unslaved gyro not affected by the earth’s magnetic north also has other advantages. At polar latitudes, the very large variations
between true north and magnetic north are difficult to reconcile in a fast-moving aircraft --- especially near 101 degrees West longitude above 74
degrees North latitude where true north is actually in the direction of magnetic south. Another problem for navigators in Polar Regions is the way
longitude meridians are represented on maps. At the equator, the distance between one degree of longitude is approximately 69 miles, but this distance
decreases rapidly as one approaches either pole.
So, an Air Force navigator who anticipates flying over the pole solves both the magnetic compass problem and the longitude convergence
problem simply by asking the pilot to unslave the gyro and set the indicator to an artificial “grid” heading. The navigator pulls out a grid map which
is simply a series of straight-ruled longitude and latitude lines, superimposed over a conformal projection, with a constant grid north, which is
aligned in parallel with 20 degrees east longitude.
From experience using grid, I can tell you that the navigator is happy with this arrangement, although I have on occasion detected a degree
of apprehension on the part of the pilots, who are looking at a heading instrument which seems “sideways” with their “reality.”
In the early 1900s, advances in radio receivers and transmitters were a boon to peace-time aircraft navigation. RDF, or radio
direction-finding equipped planes could home in on ground-transmitted signals or navigators could plot radio bearings from various stations on a chart
to obtain a position. This is the form of navigation used by Amelia Earhart and her navigator, Fred Noonan, that fateful day of July 1st,
1937, as they searched for their destination of Howland Island, north of the Solomons. Like many early forms of navigation, when using the first radio
direction finding equipment, the navigator needed to have a good approximation of his position to be successful. These early RDF bearings could either
be toward a transmitter, or on the reciprocal of that bearing, flying away from a station.
By the early 1950s, a new radio navigation aid called the VOR, short for VHF Omni-directional Radio Range, had replaced the older radio
beacon system. “This became a world-wide land-based network of ‘air highways,’ known in the U.S. as Victor Airways (below 18,000 feet) and ‘jet routes’
(at and above 18,000 feet).” [14] This network of VOR stations allowed pilots to not only fly from one
station to another simply by keeping a course pointer centered on the VOR display, but they could instantly read their position from any VOR station
from 1 to 360 degrees. And the “to the station” or “from the station” ambiguity had also been solved, with the VOR indicator prominently displaying the
words “To” or “From” on the indicator itself.
All this was possible by rotating the ground based transmitting antennas at a rate of 30 times per second, along with simultaneously
transmitting a reference-phase signal. The two signals are detected at the receiver and then compared to determine the phase difference, and thus the
direction, or radial, from the station to the aircraft. “In the ‘50s, transmitters were vacuum tube, and the antennas rotated mechanically. By the
1960s, these systems were being replaced by solid state electronics and the antenna “rotation” was accomplished electronically, achieving an equivalent
result with no moving parts.” [15]
The next evolution in this type of radio navigation was the co-location of DME equipment (distance measuring equipment) at VOR stations.
This allowed a one-station position fix by knowing both the radial from the station, and the distance from that station. The military stations
providing both azimuth and distance were named TACAN stations, for “Tactical Air Navigation.” Coupled VORS and DMES and VORS and TACANS (called
VORTACS) are all accessible to both military and civilian equipment. And those Victor Airways and Jet routes over the United States today are not
limited to flying from one VOR to the next, but now are often defined by a VOR radial and a DME distance.
For the navigator, another type of radio navigation system called a hyperbolic signal system was developed during the Second World War. It
also used fixed ground-based transmitters.
“The theory behind the operation of hyperbolic radio navigation systems was known in the late 1930s, but it took the urgency of World War
II to speed development of the system into practical use. By early 1942, the British had an operating hyperbolic system in use designed to aid in long
range bomber navigation. This system, named Gee, employed ‘master’ and ‘slave’ transmitters spaced approximately 100 miles apart.” [16]
“The Americans were not far behind the British in development of their own system. By 1943, the U.S. Coast Guard was operating a chain of
hyperbolic navigation transmitters that became Loran A (The term Loran is the acronym for Long Range Navigation). By the end of the war, the network
consisted of over 70 transmitters providing coverage over approximately 30 percent of the earth’s surface.
The theory of operation for this type of radio navigation was that the master and secondary Loran stations transmit radio pulses at precise
time intervals. “The aircraft receiver measures the time differences between when it receives the master signal and when it receives each of the
secondary signals. When this elapsed time is converted to distance, the locus of points having the time difference between the master and each
secondary forms the hyperbolic line of position. The intersection of two or more of these line of positions plotted on special charts overprinted with
a Loran time-delay lattice consisting of special hyperbolic time difference lines, produces a fix of the aircraft’s position.” [17]
“In the late 1940s and early 1950s, experiments in low frequency Loran produced a longer range, more accurate system, and Loran developed
into a 24-hour-a-day, all-weather radio navigation system named Loran C. The United States continued to operate Loran C in a number of areas around
the world, including Europe, Asia, the Mediterranean Sea, and parts of the Pacific Ocean until the mid-1990s when it began closing its overseas Loran C
stations or transferring them to the governments of the host countries.” [18] Currently Loran
continues to serve the 48 contiguous states, their coastal areas and most of Alaska.
However, the President’s Fiscal Year 2010 Budget, publicly announced by the Office of Management and Budget in February 2009 “suggests the
termination of outdated system such as terrestrial-based, long-range radio navigation (LORAN-C) operated by the Coast Guard, resulting in an offset of
$36 million in 2010 and $180 million over five years.” [19]
Since I was never assigned to LORAN-equipped aircraft, except at basic navigation school, I personally have no sympathetic feelings
regarding the up-coming loss of this system which assisted navigators for more than 60 years. I do have a lot of feeling, however, for a navigation
system that was developed on the same time-frame as Loran. And that is radar (short for “radio detection and ranging”).
After six months of Air Force navigator training, leaving the basics of maps and map-reading, plotting time and distance, using
driftmeters, astro-compasses, and bubble-averaging sextants, we finally graduated to radar. “Well, here it is,” we all said, “an electronic reflection
of what is on the ground --- how difficult can this really be?” Granted, at first, the confusing patterns of electronic “blips” lighting the radar
screen were difficult to decipher, but like everything else, hours of practice brought high levels of understanding.
Wind the clock ahead 10 years. I no longer filled the navigator position on B-52 bombers, but had upgraded to the radar-bombardier position
of this aircraft.
It was a cold night in February, and we were flying about 300 feet off the ground in this eight-engine aircraft, originally designed to fly
strategically at high altitudes. The display on the 10-inch-diameter radar scope directly in front of me danced with changing patterns of black and
white. The black areas were shadows behind hills and ridges we had yet to crest. The bright areas flickering and morphing as we passed were reflected
radar returns of those ridges in this remote area of northern New York State.
This was an important mission. Scoring our weapons release to within 10-feet at the end of this 30-minute low-level run would be a ground
crew from Air Force Strategic Air Command Headquarters. This was our Wing’s annual ORI, or Operational Readiness Inspection. All aspects of the Wing’s
mission would be inspected --- not just our flying and bombing ability. The crews standing alert had already been tested on nuclear weapon procedures
and safety, and aircraft ordnance crews were observed for safety during actual weapons download operations. All our alert aircraft nuclear weapons were
downloaded, since these same aircraft were required to fly--without receiving any additional maintenance--exactly in the configuration they were when
the inspection team arrived. And the safe handling of the nuclear weapons was critical to pass the inspection. Those were the days when “nuclear bombs
were the standard bombs of the cold war and production peaked in 1962 at six warheads a day, with the U.S. inventory of nuclear weapons eventually
reaching over 30,000.” [20]
So there we were, completing the last 100 miles of this low-level route, the navigator directing us left, right, up, and down over the
terrain. Successfully hitting imaginary targets at the conclusion of this route very likely would make the difference between a number of people being
promoted, or their status changed to “never promote again.”
The coordinates of the target had been selected by the Strategic Air Command Headquarters, which required our local Wing Bomb-Nav shop to
evaluate the target area and select an offset aiming point for the Wing’s bombardiers. They had to select, based solely on a space photo of the area,
some ground feature that would consistently radar-reflect during the bomb run. After much study of terrain-masking based upon the planned bomb-run
direction and altitude, the Bomb-Nav shop selected a farmer’s barn as the final aiming point, as they concluded it had a metal roof that would reflect
properly.
So, over the next ridge and I would get a radar look at the barn in the valley. I switched the radar from full-scan mode to tracking mode
and we popped over the ridge. And there were two small, separate returns where there should have been one. Which one? Quick, think. The return
on the left was directly below the highpoint of the next ridge. This was the pointer I needed to make the choice. But was this ridge showing
correctly? Decision. Cross-hairs on the left return, offset switch number one in, and with 40 seconds to go I called the pilot to give me “second
station.” The bombing computer was now in control of the aircraft, and as I moved the cross-hairs slowly to refine their placement, I could feel the
bomber respond. Twenty seconds. Scoring tone on. Tracking well --- don’t touch anything. Ten seconds --- the return to the right is still booming in;
no time to wonder what it is --- then we are on to the next target.
Well, we were told later that the return on the right was the farmer’s tractor, which he had taken out of the barn and driven down the road
to begin spring plowing. I was still in good standing with my crew, the squadron commander, the Wing commander, and as far as I knew, General Power
(CINCSAC himself), and God. During these missions I talked to God often, but never to General Thomas Sarsfield Power.
My next Air Force assignment--one for which I had applied and personally interviewed--was a school assignment at the University of Southern
California to receive a master’s degree in motion picture production. After graduation from that 18-month vacation from navigating, I was called to fly
the back seat of F-4 fighter-bombers during the Vietnam conflict as a “weapons systems officer.” Now, the Air Force version of the F-4 Phantom was
configured for two pilots, with full aircraft controls in the second cockpit. But what was remarkable is that this back-seater was provided an
automatic navigation system: inertial navigation. While the WSO (Weapon System Operator) had plenty of flight duties to keep him busy, navigation
certainly was not one of them. The navigation effort was simply: turn the inertial system on, wait four minutes until it has spun up to speed and
stabilized, set the base latitude and longitude coordinates and unslave the unit. It would then track the position of the aircraft in changing latitude
and longitude read-outs for the duration of the flight.
All the early inertial systems used a three-gimbal system.
“The gimbals have a bearing at each end. Each has a motor, built around one of the bearings, and at the other end a synchro (an
electromagnetic angle-measuring device). No matter how the vehicle maneuvers, the innermost gimbal maintains its orientation in inertial space. The
synchro on the innermost gimbal thus measures azimuth (or heading), the synchro on the middle gimbal measures pitch, and that on the outer gimbal
measures roll. The innermost gimbal can be thought of as a ‘stable platform’ on which are mounted the gyros and accelerometers. The whole arrangement
is generally called a ‘gimbaled platform’.” [21]
The military now uses inertial navigation in many applications because the system is impossible to (electronically) jam or sabotage from
outside using existing military technology. As early as 1958, U.S. submarines used inertial navigation to guide them under Arctic ice to the North
Pole. “Today, inertial navigation is required safety equipment in passenger aircraft making international flights. However, inertial guidance systems
are too expensive for widespread public use.” [22]
What has become quite inexpensive for civilian use is the GPS (Global Positioning System) developed and maintained by the military
and now available for general public use at no cost. “GPS was conceived in the 1970s by the Department of Defense for ballistic missile submarines to
accurately determine their position before launching missiles.” [23] Other systems were too
inaccurate, too complicated, or subject to electronic jamming.
The initial GPS system consisting of 24 solar-powered NAVSTAR satellites in high orbit cost $12 billion. As of May of 2009, there were 34
satellites, each with an estimated average life span of 7 ½ years, and maintained by the GPS Wing of the Air Force Space Command, in Los Angeles,
California. The satellites are arranged so that anytime, anywhere on Earth, there are at least four “visible” in the sky.
The system works by comparing the “lag time” in nanoseconds from a signal sent from the satellite to the synchronized clock of the
receiver. The length of the delay is equal to the signal’s travel time, and thus the distance from the satellite’s known position. That is, the
satellite’s signal speed (186,000) miles/second) times the delay time it takes to receive that signal (usually around eight hundredths of a second)
equals the distance (generally 12,000 to 15,000 miles) to the satellite.
The GPS receiver surveys all the satellite signals available to it in a similar manner, resolves these distances for a single position, and
displays that location electronically on a display screen.
When measuring delays in signals that travel at the speed of light (186,000 miles per second), it immediately becomes obvious that the
clocks in both the satellites and receiver need to be perfectly synchronized.
“To make a satellite positioning system using only synchronized clocks, you would need to have atomic clocks not only on all the
satellites, but also in the receiver itself. But atomic clocks cost somewhere between $50,000 and $100,000, which makes them just a bit too expensive
for everyday consumer use.
“The Global Positioning System has a clever, effective solution to this problem. Every satellite contains an expensive atomic clock, but
the receiver itself uses an ordinary quartz clock, which is constantly reset. In a nutshell, the receiver looks at incoming signals from four or more
satellites and gauges its own inaccuracy. In other words, there is only one value for the ‘current time’ that the receiver can use. The correct time
value will cause all of the signals that the receiver is receiving to align at a single point in space. That time value is the time value held by the
atomic clocks in all of the satellites. So the receiver sets its clock to that time value, and it then has the same time value that all the atomic
clocks in all of the satellites have. The GPS receiver gets atomic clock accuracy ‘for free’.” [24]
The last required element in this system is for the GPS receiver to know exactly where all the satellites are at all times. They travel in
very high, predictable orbits that circle the Earth twice each day. “The GPS receiver simply stores an almanac that tells it where every satellite
should be at any given time. The Satellites do change positions slightly due to minor gravitational pull from the sun and moon.” [25] “The Department of Defense tracks all the satellites by radar, and transmits any errors in
position back up to the satellites themselves, then each includes this revised position information in the signal it broadcasts.” [26]
A person might guess that the small errors observed in a GPS position are the result of clock error or orbit error. While a few feet, on
average, are the result of clock and orbit errors, the major GPS error --- when there is one --- results in changes in the speed of light. The speed of
light is not constant, except in a vacuum. The signals from satellites are often slightly slowed when traversing through charged particles in the
ionosphere, and to a very small degree by water vapor in the troposphere.
And for navigators who have GPS units that read out a position in degrees and minutes of latitude and longitude, they must make sure that
the maps they are using match the same geodetic datum as the GPS. “Geodetic datums are mathematical descriptions of the Earth used to construct maps.
Very early datums assumed the Earth was a perfect sphere. Older maps are based on the North American Datum of 1927. GPS uses the World Geodetic Systems
1984 datum.” [27]
A very significant accuracy upgrade to the basic GPS system in the United States was the development of WAAS (Wide Area Augmentation
System) in mid-year 2000. WAAS uses additional geostationary satellites (not the regular GPS satellites) and numerous ground stations providing signal
corrections which increases GPS accuracy from 60 feet to 6 feet or less, 95 percent of the time.
Free Flight Systems of Waco, Texas, advertises their aircraft cargo utility GPS navigator receiver as being 6 inches x 7 ½ x 3 inches,
weighing three pounds. It reports a new position accurate within five meters every second. It measures aircraft speed within a tenth of a knot,
instantaneously calculates and displays bearing and distance to destinations, with a running ETA and course deviation indicator, and with a quick
access search to the 20 nearest airports (not including the Hudson River).
What a navigator! But what about those real flesh-and-blood navigators who spent their careers answering the question “Are we there yet?”
Those thousands who trained by learning memory jogs such as “East is least and West is best” to know whether to add or subtract magnetic variation from
a true heading to obtain a magnetic heading; or if “Ho is Mo it’s toward,” to plot a celestial line of position toward the assumed position if the
height of the body observed (Ho) is higher (Mo, or more) than the height calculated for that assumed position.
Today, the Air Force no longer trains navigators. Through a joint service agreement, a few are still being trained by the Navy. The title
“navigator” is gradually being replaced with “combat systems officers,” as the navigator’s traditional duties are eliminated with each new aircraft
model or systems up-grade.
What would Capt James Cook have thought? But then again, how he would have loved a GPS unit!
Background of the Author:
Monte Stuck graduated from Michigan State University with a bachelor’s degree in Communication Arts, majoring in Technical Writing. He then spent the next 26 years in the Air Force, flying as a B-52 Navigator and Bombardier and later as a Weapon Systems Officer in F-4 Phantom jets, with 184 combat missions in Vietnam.
He received his master’s degree in Motion Picture Production at the University of Southern California while still in the service, and
subsequently held many Air Force management positions in film production, including Squadron Commander of a Photographic Squadron, Director of
Joint-Interest Film Procurement for the Department of Defense (at the Pentagon) and Assistant Deputy of Operations for the Department of Defense
Audiovisual Agency.
Upon retirement, Monte worked for Riverside County Department of Building and Safety, first as a building inspector, then as a plans
examiner, and finally retiring in 2000 as a Deputy Director of Building and Safety for Riverside County.
He is currently Secretary of the Board of Air Force Village West, a continuing care retirement community of 600 residents in Riverside.
Footnote References:
[5]
Egbert, Robert I. and King, Joseph E., The GPS Handbook, (Burford Books, 2003) p.52
[23]
Egbert, Robert I. and King, Joseph E., The GPS Handbook, (Burford Books, 2003) p.9
[26]
Egbert, Robert I. and King, Joseph E., The GPS Handbook, (Burford Books, 2003) p.14