Loran-C

Loran-Cis ahyperbolicradio navigationsystem that allows a receiver to determine its position by listening tolow frequencyradio signals that are transmitted by fixed land-basedradio beacons.Loran-C combined two different techniques to provide a signal that was both long-range and highly accurate, features that had been incompatible. Its disadvantage was the expense of the equipment needed to interpret the signals, which meant that Loran-C was used primarily by militaries after it was introduced in 1957.

A Loran-C receiver for use on merchant ships

Loran-C sound as received on an AM receiver at 100 kHz

By the 1970s, the cost, weight and size of electronics needed to implement Loran-C had been dramatically reduced because of the introduction ofsolid-state electronicsand, from the mid-1970s, earlymicrocontrollersto process the signal. Low-cost and easy-to-use Loran-C units became common from the late 1970s, especially in the early 1980s, and the earlierLORANsystem was discontinued in favor of installing more Loran-C stations around the world. Loran-C became one of the most common and widely-used navigation systems for large areas of North America, Europe, Japan and the entire Atlantic and Pacific areas. TheSoviet Unionoperated a nearly identical system,CHAYKA.

The introduction of civiliansatellite navigationin the 1990s led to a rapid drop-off in Loran-C use. Discussions about the future of Loran-C began in the 1990s; several turn-off dates were announced and then cancelled. In 2010, the US and Canadian systems were shut down, along with Loran-C/CHAYKA stations that were shared with Russia.Several other chains remained active; some were upgraded for continued use. At the end of 2015, navigation chains in most of Europe were turned off.In December 2015 in the United States, there was also renewed discussion of funding aneLoransystem,andNISToffered to fund development of a microchip-sized eLoran receiver for distribution of timing signals.

The National Timing Resilience and Security Act of 2017, proposed resurrecting Loran as a backup for the United States in case of a GPS outage caused byspace weatheror attack.

History

Loran-A

Main article:LORAN

The original LORAN was proposed in 1940 byAlfred Lee Loomisat a meeting of the U.S. Army's Microwave Committee. TheArmy Air Corpswere interested in the concept for aircraft navigation, and after some discussion they returned a requirement for a system offering accuracy of about 1 mile (1.6 km) at a range of 200 miles (320 km), and a maximum range as great as 500 miles (800 km) for high-flying aircraft. The Microwave Committee, by this time organized into what would become theMIT Radiation Laboratory,took up development asProject 3.During the initial meetings, a member of the UK liaison team,Taffy Bowen,mentioned that he was aware the British were also working on a similar concept, but had no information on its performance.

The development team, led by Loomis, made rapid progress on the transmitter design and tested several systems during 1940 before settling on a 3 MHz design. Extensive signal-strength measurements were made by mounting a conventional radio receiver in astation wagonand driving around the eastern states.However, the custom receiver design and its associatedcathode-ray tubedisplays proved to be a bigger problem. In spite of several efforts to design around the problem, instability in the display prevented accurate measurements as the output shifted back and forth on the face of the oscilloscope.

By this time the team had become much more familiar with the BritishGeesystem, and were aware of their related work on "strobes", atime base generatorthat produced well-positioned "pips" on the display that could be used for accurate measurement. This meant that inaccuracy of the positioning on the display had no effect: any inaccuracy in the position of the signal was also in the strobe, so the two remained aligned. The Project 3 team met with the Gee team in 1941, and immediately adopted this solution. This meeting also revealed that Project 3 and Gee called for almost identical systems, with similar performance, range and accuracy, but Gee had already completed basic development and was entering into initial production, making Project 3 superfluous.

In response, the Project 3 team told the Army Air Force to adopt Gee, and instead, at the behest of the British team, realigned their efforts to provide long-range navigation on the oceans where Gee was not useful. This led toUnited States Navyinterest, and a series of experiments quickly demonstrated that systems using the basic Gee concept, but operating at a lower frequency around 2 MHz would offer reasonable accuracy on the order of a few miles over distances on the order of 1,250 miles (2,010 km), at least at night when signals of this frequency range were able to skip off theionosphere.Rapid development followed, and a system covering the western Atlantic was operational in 1943. Additional stations followed, first covering the European side of the Atlantic, and then a large expansion in the Pacific. By the end of the war, there were 72 operational LORAN stations and as many as 75,000 receivers.

In 1958 the operation of the LORAN system was handed over to theUnited States Coast Guard,which renamed the system "Loran-A", the lower-case name being introduced at that time.

LF LORAN

There are two ways to implement the timing measurements needed for a hyperbolic navigation system, pulse timing systems like Gee and LORAN, and phase-timing systems like theDecca Navigator System.

The former requires sharp pulses of signal, and their accuracy is generally limited to how rapidly the pulses can be turned on and off, which is a function of thecarrier frequency.There is an ambiguity in the signal; the same measurements can be valid at two locations relative to the broadcasters, but in normal operation, they are hundreds of kilometres apart, so one possibility can be eliminated.

The second system uses constant signals ( "continuous wave" ) and takes measurements by comparing the phase of two signals. This system is easy to use even at very low frequencies. However, its signal is ambiguous over the distance of a wavelength, meaning there are hundreds of locations that will return the same signal. Decca referred to these ambiguous locations ascells.This demands some other navigation method to be used in conjunction to pick which cell the receiver is within, and then using the phase measurements to place the receiver accurately within the cell.

Numerous efforts were made to provide some sort of secondary low-accuracy system that could be used with a phase-comparison system like Decca in order to resolve the ambiguity. Among the many methods was a directional broadcast system known asPOPI,and a variety of systems combining pulse-timing for low-accuracy navigation and then using phase-comparison for fine adjustment. Decca themselves had set aside one frequency, "9f", for testing this combined-signal concept, but did not have the chance to do so until much later. Similar concepts were also used in the experimentalNavarhosystem in the United States.

It was known from the start of the LORAN project that the same CRT displays that showed the LORAN pulses could, when suitably magnified, also show the individual waves of theintermediate frequency.This meant that pulse-matching could be used to get a rough fix, and then the operator could gain additional timing accuracy by lining up the individual waves within the pulse, like Decca. This could either be used to greatly increase the accuracy of LORAN, or alternately, offer similar accuracy using much lower carrier frequencies, and thus greatly extend the effective range. This would require the transmitter stations to be synchronized both in time and phase, but much of this problem had already been solved by Decca engineers.

The long-range option was of considerable interest to the Coast Guard, who set up an experimental system known asLF LORANin 1945. This operated at much lower frequencies than the original LORAN, at 180 kHz, and required very long balloon-borne antennas. Testing was carried out throughout the year, including several long-distance flights as far asBrazil.The experimental system was then sent to Canada where it was used duringOperation Muskoxin the Arctic. Accuracy was found to be 150 feet (46 m) at 750 miles (1,210 km), a significant advance over LORAN. With the ending of Muskox, it was decided to keep the system running under what became known as "Operation Musk Calf", run by a group consisting of theUnited States Air Force,Royal Canadian Air Force,Royal Canadian Navyand the UKRoyal Corps of Signals.The system ran until September 1947.

This led to another major test series, this time by the newly-formed United States Air Force, known as Operation Beetle. Beetle was located in the far north, on the Canada-Alaska border, and used new guy-stayed 625 feet (191 m) steel towers, replacing the earlier system's balloon-lofted cable antennas. The system became operational in 1948 and ran for two years until February 1950. Unfortunately, the stations proved poorly sited, as the radio transmission over thepermafrostwas much shorter than expected and synchronization of the signals between the stations using ground waves proved impossible. The tests also showed that the system was extremely difficult to use in practice; it was easy for the operator to select the wrong sections of the waveforms on their display, leading to significant real-world inaccuracy.

CYCLAN and Whyn

In 1946 theRome Air Development Centersent out contracts for longer-ranged and more-accurate navigation systems that would be used for long-range bombing navigation. As theUnited States Army Air Forceswere moving towards smaller crews, only three in theBoeing B-47 Stratojetfor instance, a high degree of automation was desired. Two contracts were accepted;Sperry Gyroscopeproposed theCYCLANsystem (CYCLe matching LorAN) which was broadly similar to LF LORAN but with additional automation, and Sylvania proposedWhynusing continuous wave navigation like Decca, but with additional coding usingfrequency modulation.In spite of great efforts, Whyn could never be made to work, and was abandoned.

CYCLAN operated by sending the same LF LORAN-like signals on two frequencies, LF LORAN's 180 kHz and again on 200 kHz. The associated equipment would look for a rising amplitude that indicated the start of the signal pulse, and then use sampling gates to extract the carrier phase. Using two receivers solved the problem of mis-aligning the pulses, because the phases would only align properly between the two copies of the signal when the same pulses were being compared. None of this was trivial; using the era's tube-based electronics, the experimental CYCLAN system filled much of asemi-trailer.

CYCLAN proved highly successful, so much so that it became increasingly clear that the problems that led the engineers to use two frequencies were simply not as bad as expected. It appeared that a system using a single frequency would work just as well, given the right electronics. This was especially good news, as the 200 kHz frequency was interfering with existing broadcasts, and had to be moved to 160 kHz during testing.

Through this period the issue of radio spectrum use was becoming a major concern, and had led to international efforts to decide on a frequency band suitable for long-range navigation. This process eventually settled on the band from 90 to 100 kHz. CYCLAN appeared to suggest that accuracy at even lower frequencies was not a problem, and the only real concern was the expense of the equipment involved.

Cytac

The success of the CYCLAN system led to a further contract with Sperry in 1952 for a new system with the twin goals of working in the 100 kHz range while being equally accurate, less complex and less expensive. These goals would normally be contradictory, but the CYCLAN system gave all involved the confidence that these could be met. The resulting system was known as Cytac.

To solve the complexity problem, a new circuit was developed to properly time the sampling of the signal. This consisted of a circuit to extract the envelope of the pulse, another to extract the derivative of the envelope, and finally another that subtracted the derivative from the envelope. The result of this final operation would become negative during a very specific and stable part of the rising edge of the pulse, and this zero-crossing was used to trigger a very short-time sampling gate. This system replaced the complex system of clocks used in CYCLAN. By simply measuring the time between the zero-crossings of the master and secondary, pulse-timing was extracted.

The output of the envelope sampler was also sent to a phase-shifter that adjusted the output of a local clock that locked to the master carrier using aphase-locked loop.This retained the phase of the master signal long enough for the secondary signal to arrive. Gating on the secondary signal was then compared to this master signal in aphase detector,and a varying voltage was produced depending on the difference in phase. This voltage represented the fine-positioning measurement.

The system was generally successful during testing through 1953, but there were concerns raised about the signal power at long range and the possibility of jamming. This led to further modifications of the basic signal. The first was to broadcast a series of pulses instead of just one, broadcasting more energy during a given time and improving the ability of the receivers to tune in a useful signal. They also added a fixed 45° phase shift to every pulse, so simple continuous-wave jamming signals could be identified and rejected.

The Cytac system underwent an enormous series of tests across the United States and offshore. Given the potential accuracy of the system, even minor changes to the groundwave synchronization were found to cause errors that could be eliminated — issues such as the number of rivers the signal crossed caused predictable delays that could be measured and then factored into navigation solutions. This led to a series ofcorrection contoursthat could be added to the received signal to adjust for these concerns, and these were printed on the Cytac charts. Using prominent features on dams as target points, a series of tests demonstrated that the uncorrected signals provided accuracy on the order of 100 yards, while adding the correction contour adjustments reduced this to the order of ten yards.

Loran-B and -C

It was at this moment that the United States Air Force, having taken over these efforts while moving from theUnited States Army Air Forces,dropped their interest in the project. Although the reasons are not well recorded, it appears the idea of a fully automated bombing system using radio aids was no longer considered possible.The AAF had been involved in missions covering about 1000 km (the distance from London to Berlin) and the Cytac system would work well at these ranges, but as the mission changed to trans-polar missions of 5,000 km or more, even Cytac did not offer the range and accuracy needed. They turned their attention to the use ofinertial platformsandDoppler radarsystems, cancelling work on Cytac as well as a competing system known as Navarho.

Around this period the United States Navy began work on a similar system using combined pulse and phase comparison, but based on the existing LORAN frequency of 200 kHz. By this time the United States Navy had handed operational control of the LORAN system to the Coast Guard, and it was assumed the same arrangement would be true for any new system as well. Thus, the United States Coast Guard was given the choice of naming the systems, and decided to rename the existing system Loran-A, and the new system Loran-B.

With Cytac fully developed and its test system on the east coast of the United States mothballed, the United States Navy also decided to re-commission Cytac for tests in the long-range role. An extensive series of tests across the Atlantic were carried out by theUSCGCAndroscogginstarting in April 1956. Meanwhile, Loran-B proved to have serious problems keeping their transmitters in phase, and that work was abandoned.Minor changes were made to the Cytac systems to further simplify it, including a reduction in the pulse-chain spacing from 1200 to 1000 μs, the pulse rate changed to 20ppsto match the existing Loran-A system, and the phase-shifting between pulses to an alternating 0, 180-degree shift instead of 45 degrees at every pulse within the chain.

The result was Loran-C. Testing of the new system was intensive, and over-water flights aroundBermudademonstrated that 50% of fixes lay within a circle of 260 ft (79 m) radius,a dramatic improvement over the original Loran-A, meeting the accuracy of the Gee system, but at much greater range. The first chain was set up using the original experimental Cytac system, and a second one in the Mediterranean in 1957. Further chains covering the North Atlantic and large areas of the Pacific followed. At the time global charts were printed with shaded sections representing the area where a 3-mile (4.8 km) accurate fix could be obtained under most operational conditions. Loran-C operated in the 90 to 110 kHz frequency range.

Improving systems

Loran-C had originally been designed to be highly automated, allowing the system to be operated more rapidly than the original LORAN's multi-minute measurement. It was also operated in "chains" of linked stations, allowing a fix to be made by simultaneously comparing two secondaries to a single master. The downside of this approach was that the required electronic equipment, built using 1950s-era tube technology, was very large. Looking for companies with knowledge of seaborne, multi-channel phase-comparison electronics led, ironically, to Decca, who built the AN/SPN-31, the first widely used Loran-C receiver. The AN/SPN-31 weighed over 100 pounds (45 kg) and had 52 controls.

Airborne units followed, and an adapted AN/SPN-31 was tested in anAvro Vulcanin 1963. By the mid-1960s, units with some transistorization were becoming more common, and a chain was set up inVietnamto support the United States'war effortsthere. A number of commercial airline operators experimented with the system as well, using it for navigation on thegreat circleroute between North America and Europe. However,inertial platformsultimately became more common in this role.

In 1969, Decca sued the United States Navy for patent infringement, producing ample documentation of their work on the basic concept as early as 1944, along with the "missing" 9f frequencyat 98 kHz that had been set aside for experiments using this system. Decca won the initial suit, but the judgement was overturned on appeal when the Navy claimed "wartime expediency".

Loran-D and -F

When Loran-C became widespread, the United States Air Force once again became interested in using it as a guidance system. They proposed a new system layered on top of Loran-C to provide even higher accuracy, using the Loran-C fix as the coarse guidance signal in much the same way that Loran-C extracted coarse location from pulse timing to remove the ambiguity in the fine measurement. To provide an extra-fine guidance signal,Loran-Dinterleaved another train of eight pulses immediately after the signals from one of the existing Loran-C stations, folding the two signals together. This technique became known as "Supernumary Interpulse Modulation" (SIM). These were broadcast from low-power portable transmitters, offering relatively short-range service of high accuracy.

Loran-D was used only experimentally during war-games in the 1960s from a transmitter set in the UK. The system was also used in a limited fashion during theVietnam War,combined with the Pave Spotlaser designatorsystem, a combination known as Pave Nail. Using mobile transmitters, the AN/ARN-92 LORAN navigation receiver could achieve accuracy on the order of 60 feet (18 m), which the Spot laser improved to about 20 feet (6.1 m).The SIM concept later became a system for sending additional data.

At about the same time,Motorolaproposed a new system using pseudo-random pulse-chains. This mechanism ensures that no two chains within a given period (on the order of many seconds) will have the same pattern, making it easy to determine if the signal is a groundwave from a recent transmission or a multi-hop signal from a previous one. The system,Multi-User Tactical Navigation Systems(MUTNS) was used briefly but it was found that Loran-D met the same requirements but had the added advantage of being a standard Loran-C signal as well. Although MUTNS was unrelated to the Loran systems, it was sometimes referred to asLoran-F.

Decline

In spite of its many advantages, the high cost of implementing a Loran-C receiver made it uneconomical for many users. Additionally, as military users upgraded from Loran-A to Loran-C, large numbers of surplus Loran-A receivers were dumped on the market. This made Loran-A popular in spite of being less accurate and fairly difficult to operate. By the early 1970s the introduction ofintegrated circuitscombining a complete radio receiver began to greatly reduce the complexity of Loran-A measurements, and fully automated units the size of astereo receiverbecame common. For those users requiring higher accuracy, Decca had considerable success with their Decca Navigator system, and produced units that combined both receivers, using Loran to eliminate the ambiguities in Decca.

The same rapid development of microelectronics that made Loran-A so easy to operate worked equally well on the Loran-C signals, and the obvious desire to have a long-range system that could also provide enough accuracy for lake and harbour navigation led to the "opening" of the Loran-C system to public use in 1974. Civilian receivers quickly followed, and dual-system A/C receivers were also common for a time. The switch from A to C was extremely rapid, due largely to rapidly falling prices which led to many users' first receiver being Loran-C. By the late 1970s the Coast Guard decided to turn off Loran-A, in favour of adding additional Loran-C stations to cover gaps is its coverage. The original Loran-A network was shut down in 1979 and 1980, with a few units used in the Pacific for some time. Given the widespread availability of Loran-A charts, many Loran-C receivers included a system for converting coordinates between A and C units.

One of the reasons for Loran-C's opening to the public was the move from Loran to new forms of navigation, includinginertial navigation systems,TransitandOMEGA,meant that the security of Loran was no longer as stringent as it was as a primary form of navigation. As these newer systems gave way to GPS through the 1980s and 90s, this process repeated itself, but this time the military was able to separate GPS's signals in such a way that it could provide both secure military and insecure civilian signals at the same time. GPS was more difficult to receive and decode, but by the 1990s the required electronics were already as small and inexpensive as Loran-C, leading to rapid adoption that has become largely universal.

Loran-C in the 21st century

Although Loran-C was largely redundant by 2000, it has not universally disappeared as of 2014due to a number of concerns. One is that the GPS system can be jammed through a variety of means. Although the same is true of Loran-C, the transmitters are close-at-hand and can be adjusted if necessary. More importantly, there are effects that might cause the GPS system to become unusable over wide areas, notablyspace weatherevents and potentialEMPevents. Loran, located entirely under the atmosphere, offers more resilience to these issues. There has been considerable debate about the relative merits of keeping the Loran-C system operational as a result of such considerations.

In November 2009, theUnited States Coast Guardannounced that Loran-C was not needed by the U.S. for maritime navigation. This decision left the fate of LORAN and eLoran in the United States to the Secretary of theDepartment of Homeland Security.Per a subsequent announcement, the US Coast Guard, in accordance with the DHS Appropriations Act, terminated the transmission of all U.S. Loran-C signals on 8 February 2010.On 1 August 2010 the U.S. transmission of the Russian American signal was terminated,and on 3 August 2010 all Canadian signals were shut down by the USCG and the CCG.

TheEuropean Unionhad decided that the potential security advantages of Loran are worthy not only of keeping the system operational, but upgrading it and adding new stations. This is part of the widerEurofixsystem which combines GPS,Galileoand nine Loran stations into a single integrated system.

In 2014, Norway and France both announced that all of their remaining transmitters, which make up a significant part of the Eurofix system, would be shut down on 31 December 2015.The two remaining transmitters in Europe (Anthorn,UK andSylt,Germany) would no longer be able to sustain a positioning and navigation Loran service, with the result that the UK announced its trial eLoran service would be discontinued from the same date.

Description

Hyperbolic navigation

A crude diagram of the LORAN principle—the difference between the time of reception of synchronized signals from radio stations A and B is constant along each hyperbolic curve; when demarcated on a map, such curves are known as "TD lines". "TD" stands for "Time Difference".

In conventional navigation, measuring one's location, ortaking a fix,is accomplished by taking two measurements against well known locations. In optical systems this is typically accomplished by measuring the angle to two landmarks, and then drawing lines on anautical chartat those angles, producing an intersection that reveals the ship's location. Radio methods can also use the same concept with the aid of aradio direction finder,but due to the nature of radio propagation, such instruments are subject to significant errors, especially at night. More accurate radio navigation can be made using pulse timing or phase comparison techniques, which rely on the time-of-flight of the signals. In comparison to angle measurements, these remain fairly steady over time, and most of the effects that change these values are fixed objects like rivers and lakes that can be accounted for on charts.

Timing systems can reveal the absolute distance to an object, as is the case inradar.The problem in the navigational case is that the receiver has to know when the original signal was sent. In theory, one could synchronize an accurate clock to the signal before leaving port, and then use that to compare the timing of the signal during the voyage. However, in the 1940s no suitable system was available that could hold an accurate signal over the time span of an operational mission.

Instead, radio navigation systems adopted themultilaterationconcept which is based on the difference in times (or phase) instead of the absolute time. The basic idea is that it is relatively easy to synchronize two ground stations, using a signal shared over a phone line for instance, so one can be sure that the signals received were sent at exactly the same time. They will not be received at exactly the same time, however, as the receiver will receive the signal from the closer station first. Timing the difference between two signals can be easily accomplished, first by physically measuring them on a cathode-ray tube, or simple electronics in the case of phase comparison.

The difference in signal timing does not reveal the location by itself. Instead, it determines a series of locations where that timing is possible. For instance, if the two stations are 300 km apart and the receiver measures no difference in the two signals, that implies that the receiver is somewhere along a line equidistant between the two. If the signal from one is received exactly 100 μs after, then the receiver is 30 kilometres (19 mi) closer to one station than the other. Plotting all the locations where one station is 30 km closer than the other produces a curved line. Taking a fix is accomplished by making two such measurements with different pairs of stations, and then looking up both curves on a navigational chart. The curves are known aslines of positionor LOP.

In practice, radio navigation systems normally use achainof three or four stations, all synchronized to amastersignal that is broadcast from one of the stations. The others, thesecondaries,are positioned so their LOPs cross at acute angles, which increases the accuracy of the fix. So for instance, a given chain might have four stations with the master in the center, allowing a receiver to pick the signals from two secondaries that are currently as close to right angles as possible given their current location. Modern systems, which know the locations of all the broadcasters, can automate which stations to pick.

LORAN method

LORAN pulse

In the case of LORAN, one station remains constant in each application of the principle, theprimary,being paired up separately with two othersecondarystations. Given two secondary stations, the time difference (TD) between the primary and first secondary identifies one curve, and the time difference between the primary and second secondary identifies another curve, the intersections of which will determine ageographicpoint in relation to the position of the three stations. These curves are referred to asTD lines.

In practice, LORAN is implemented in integrated regionalarrays,orchains,consisting of oneprimarystation and at least two (but often more)secondarystations, with a uniformgroup repetition interval(GRI) defined inmicroseconds.The amount of time before transmitting the next set of pulses is defined by the distance between the start of transmission of primary to the next start of transmission of primary signal.

The secondary stations receive this pulse signal from the primary, then wait a preset number ofmilliseconds,known as thesecondary codingdelay,to transmit a response signal. In a given chain, each secondary's coding delay is different, allowing for separate identification of each secondary's signal. (In practice, however, modern LORAN receivers do not rely on this for secondary identification.)

LORAN chains (GRIs)

LORAN Station Malone,Malone, FloridaGreat Lakes chain (GRI 8970)/Southeast U.S. chain (GRI 7980)

Every LORAN chain in the world uses a unique Group Repetition Interval, the number of which, when multiplied by ten, gives how many microseconds pass between pulses from a given station in the chain. In practice, the delays in many, but not all, chains are multiples of 100 microseconds. LORAN chains are often referred to by this designation,e.g.,GRI 9960, the designation for the LORAN chain serving theNortheastern United States.

Due to the nature of hyperbolic curves, a particular combination of a primary and two secondary stations can possibly result in a "grid" where the grid lines intersect at shallow angles. For ideal positional accuracy, it is desirable to operate on a navigational grid where the grid lines are closer to right angles (orthogonal) to each other. As the receiver travels through a chain, a certain selection of secondaries whose TD lines initially formed a near-orthogonal grid can become a grid that is significantly skewed. As a result, the selection of one or both secondaries should be changed so that the TD lines of the new combination are closer to right angles.In practice, nearly all chains provide at least three, and as many as five, secondaries.

LORAN charts

This nautical chart ofNew YorkHarbor includes LORAN-A TD lines. Note that the printed lines do not extend into inland waterway areas.

Where available, common marinenautical chartsinclude visible representations of TD lines at regular intervals over water areas. The TD lines representing a given primary-secondary pairing are printed with distinct colors, and note the specific time difference indicated by each line. On a nautical chart, the denotation for each Line of Position from a receiver, relative to axis and color, can be found at the bottom of the chart. The color on official charts for stations and the timed-lines of position follow no specific conformance for the purpose of theInternational Hydrographic Organization(IHO). However, local chart producers may color these in a specific conformance to their standard. Always consult the chart notes, administrations Chart1 reference, and information given on the chart for the most accurate information regarding surveys, datum, and reliability.

There are three major factors when considering signal delay andpropagationin relation to LORAN-C:

1. Primary Phase Factor (PF) – This allows for the fact that the speed of the propagated signal in the atmosphere is slightly lower than in a vacuum.
2. Secondary Phase Factor (SF) – This allows for the fact that the speed of propagation of the signal is slowed when traveling over the seawater because of the greater conductivity of seawater compared to land.
3. Additional Secondary Factors (ASF) – Because LORAN-C transmitters are mainly land based, the signal will travel partly over land and partly over seawater. ASF may be treated as land and water segments, each with a uniform conductivity depending on whether the path is over land or water.

The chart notes should indicate whether ASF corrections have been made (Canadian Hydrographic Service (CHS) charts, for example, include them). Otherwise, the appropriate correction factors must be obtained before use.

Due to interference and propagation issues suffered from land features and artificial structures such as tall buildings, the accuracy of the LORAN signal can be degraded considerably in inland areas (seeLimitations). As a result, nautical charts will not show TD lines in those areas, to prevent reliance on LORAN-C for navigation.

Traditional LORAN receivers display the time difference between each pairing of the primary and one of the two selected secondary stations, which is then used to find the appropriate TD line on the chart. Modern LORAN receivers display latitude and longitude coordinates instead of time differences, and, with the advent of time difference comparison and electronics, provide improved accuracy and better position fixing, allowing the observer to plot their position on a nautical chart more easily. When using such coordinates, thedatumused by the receiver (usuallyWGS84) must match that of the chart, or manual conversion calculations must be performed before the coordinates can be used.

Timing and synchronization

Cesium atomic clocks

Each LORAN station is equipped with a suite of specialized equipment to generate the precisely timed signals used to modulate / drive the transmitting equipment. Up to three commercial cesiumatomic clocksare used to generate 5 MHz andpulse per second(or 1 Hz) signals that are used by timing equipment to generate the various GRI-dependent drive signals for the transmitting equipment.

While each U.S.-operated LORAN station is supposed to be synchronized to within 100 ns ofCoordinated Universal Time(UTC), the actual accuracy achieved as of 1994 was within 500 ns.

Transmitters and antennas

LORAN transmitter bank

LORAN-C transmitters operate at peak powers of 100–4,000 kilowatts, comparable tolongwavebroadcasting stations. Most use 190–220 metre tall mast radiators, insulated from ground. The masts are inductively lengthened and fed by aloading coil(see:electrical length). A well known-example of a station using such an antenna isRantum.Free-standingtower radiatorsin this height range are also used.Carolina Beachuses a free-standing antenna tower. Some LORAN-C transmitters with output powers of 1,000 kW and higher used extremely tall412-metremast radiators (see below). Other high power LORAN-C stations, likeGeorge,used four T-antennas mounted on four guyed masts arranged in a square.

All LORAN-C antennas are designed to radiate an omnidirectional pattern. Unlike longwave broadcasting stations, LORAN-C stations cannot use backup antennas because the exact position of the antenna is a part of the navigation calculation. The slightly different physical location of a backup antenna would produce Lines of Position different from those of the primary antenna.

Limitations

• 
  Atlantic Ocean LORAN coverage (2006)
• 
  Pacific Ocean LORAN coverage (2006)

LORAN suffers from electronic effects of weather and the ionospheric effects of sunrise and sunset. The most accurate signal is thegroundwavethat follows the Earth's surface, ideally over seawater. At night the indirectskywave,bent back to the surface by theionosphere,is a problem as multiple signals may arrive via different paths (multipath interference). The ionosphere's reaction to sunrise and sunset accounts for the particular disturbance during those periods.Geomagnetic stormshave serious effects, as with any radio based system.

LORAN uses ground-based transmitters that only cover certain regions. Coverage is quite good in North America, Europe, and the Pacific Rim.

The absolute accuracy of LORAN-C varies from 0.10 to 0.25nmi(185 to 463 m). Repeatable accuracy is much greater, typically from 60 to 300ft(18 to 91 m).

LORAN Data Channel (LDC)

LORAN Data Channel (LDC) is a project underway between theFAAandUnited States Coast Guardto send low bit rate data using the LORAN system. Messages to be sent include station identification, absolute time, and position correction messages. In 2001, data similar toWide Area Augmentation System(WAAS)GPScorrection messages were sent as part of a test of the Alaskan LORAN chain. As of November 2005, test messages using LDC were being broadcast from several U.S. LORAN stations.

In recent years, LORAN-C has been used in Europe to send differential GPS and other messages, employing a similar method of transmission known as EUROFIX.

A system called SPS (Saudi Positioning System), similar to EUROFIX, is in use in Saudi Arabia.GPS differential corrections and GPS integrity information are added to the LORAN signal. A combined GPS/LORAN receiver is used, and if a GPS fix is not available it automatically switches over to LORAN.

Future

As LORAN systems are maintained and operated by governments, their continued existence is subject to public policy. With the evolution of other electronic navigation systems, such assatellite navigationsystems, funding for existing systems is not always assured.

Critics, who have called for the elimination of the system, state that the LORAN system has too few users, lacks cost-effectiveness, and thatGlobal Navigation Satellite System(GNSS) signals are superior to LORAN.Supporters of continued and improved LORAN operation note that LORAN uses a strong signal, which is difficult to jam, and that LORAN is an independent, dissimilar, and complementary system to other forms of electronic navigation, which helps ensure availability of navigation signals.

On 26 February 2009, the U.S. Office of Management and Budget released the first blueprint for theFiscal Year 2010 budget.This document identified the LORAN-C system as "outdated" and supported its termination at an estimated savings of $36 million in 2010 and $190 million over five years.

On 21 April 2009 the U.S. Senate Committee on Commerce, Science and Transportation and the Committee on Homeland Security and Governmental Affairs released inputs to the FY 2010 Concurrent Budget Resolution with backing for the continued support for the LORAN system, acknowledging the investment already made in infrastructure upgrades and recognizing the studies performed and multi-departmental conclusion that eLoran is the best backup to GPS.

SenatorJay Rockefeller,Chairman of the Committee on Commerce, Science and Transportation, wrote that the committee recognized the priority in "Maintaining LORAN-C while transitioning to eLORAN" as means of enhancing the national security, marine safety and environmental protection missions of the Coast Guard.

Senator Collins, the ranking member on the Committee on Homeland Security and Governmental Affairs wrote that the President's budget overview proposal to terminate the LORAN-C system is inconsistent with the recent investments, recognized studies and the mission of the U.S. Coast Guard. The committee also recognizes the $160 million investment already made toward upgrading the LORAN-C system to support the full deployment of eLoran.

Further, the Committees also recognize the many studies which evaluated GPS backup systems and concluded both the need to back up GPS and identified eLoran as the best and most viable backup. "This proposal is inconsistent with the recently released (January 2009) Federal Radionavigation Plan (FRP), which was jointly prepared by DHS and the Departments of Defense (DOD) and Transportation (DOT). The FRP proposed the eLoran program to serve as a Position, Navigation and Timing (PNT) backup to GPS (Global Positioning System)."

On 7 May 2009, President Barack Obama proposed cutting funding (approx. $35 million/year) for LORAN, citing its redundancy alongside GPS.In regard to the pending Congressional bill, H.R. 2892, it was subsequently announced that "[t]he Administration supports the Committee's aim to achieve an orderly termination through a phased decommissioning beginning in January 2010, and the requirement that certifications be provided to document that the LORAN-C termination will not impair maritime safety or the development of possible GPS backup capabilities or needs."

Also on 7 May 2009, the U.S. General Accounting Office (GAO), the investigative arm of Congress, released a report citing the very real potential for the GPS system to degrade or fail in light of program delays which have resulted in scheduled GPS satellite launches slipping by up to three years.

On 12 May 2009 the March 2007 Independent Assessment Team (IAT) report on LORAN was released to the public. In its report the ITA stated that it "unanimously recommends that the U.S. government complete the eLoran upgrade and commit to eLoran as the national backup to GPS for 20 years." The release of the report followed an extensive Freedom of Information Act (FOIA) battle waged by industry representatives against the federal government. Originally completed 20 March 2007 and presented to the co-sponsoring Department of Transportation and Department of Homeland Security (DHS) Executive Committees, the report carefully considered existing navigation systems, including GPS. The unanimous recommendation for keeping the LORAN system and upgrading to eLoran was based on the team's conclusion that LORAN is operational, deployed and sufficiently accurate to supplement GPS. The team also concluded that the cost to decommission the LORAN system would exceed the cost of deploying eLoran, thus negating any stated savings as offered by the Obama administration and revealing the vulnerability of the U.S. to GPS disruption.

In November 2009, the U.S. Coast Guard announced that the LORAN-C stations under its control would be closed down for budgetary reasons after 4 January 2010 provided the Secretary of the Department of Homeland Security certified that LORAN is not needed as a backup for GPS.

On 7 January 2010, Homeland Security published a notice of the permanent discontinuation of LORAN-C operation. Effective 2000 UTC 8 February 2010, the United States Coast Guard terminated all operation and broadcast of LORAN-C signals in the United States. The United States Coast Guard transmission of the Russian American CHAYKA signal was terminated on 1 August 2010. The transmission of Canadian LORAN-C signals was terminated on 3 August 2010.

United Kingdom eLoran implementation

On 31 May 2007, the UK Department for Transport (DfT), via thegeneral lighthouse authorities,awarded a 15-year contract to provide a state-of-the-art Enhanced LORAN service to improve the safety of mariners in the UK and Western Europe. The service contract was to operate in two phases, with development work and further focus for European agreement on eLoran service provision from 2007 through 2010, and full operation of the eLoran service from 2010 through 2022. The first eLoran transmitter was situated atAnthorn Radio StationCumbria, UK, and was operated byBabcock International(previously Babcock Communications).

The UK government granted approval for seven differential eLoran ship-positioning technology stations to be built along the south and east coasts of the UK to help counter the threat of jamming of global positioning systems. They were set to reach initial operational capability by summer 2014.The general lighthouse authorities of the UK and Ireland announced 31 October 2014 the initial operational capability of UK maritime eLoran. Seven differential reference stations provided additional position, navigation, and timing (PNT) information via low-frequency pulses to ships fitted with eLoran receivers. The service was to help ensure they could navigate safely in the event of GPS failure in one of the busiest shipping regions in the world, with expected annual traffic of 200,000 vessels by 2020.

Despite these plans, in light of the decision by France and Norway to cease Loran transmissions on 31 December 2015, the UK announced at the start of that month that its eLoran service would be discontinued on the same day.However to allow for further research and PNT development, the eLoran timing signal is still active from the government facility inAnthorn.

List of LORAN-C transmitters

Map of LORAN stations.

A list of LORAN-C transmitters. Stations with an antenna tower taller than 300metres(984 feet) are shown in bold.

Station	Country	Chain	Coordinates	Remarks
Afif	Saudi Arabia	Saudi Arabia South (GRI 7030) Saudi Arabia North (GRI 8830)	23°48′36.66″N42°51′18.17″E	400 kW
Al Khamasin	Saudi Arabia	Saudi Arabia South (GRI 7030) Saudi Arabia North (GRI 8830)	20°28′2.34″N44°34′51.9″E	dismantled
Al Muwassam	Saudi Arabia	Saudi Arabia South (GRI 7030) Saudi Arabia North (GRI 8830)	16°25′56.87″N42°48′6.21″E	dismantled
Angissoq	Greenland	shut down	59°59′17.348″N45°10′26.91″W	shut down31 December 1994; used a 411.48 metre tower until 27 July 1964,demolished
Anthorn	United Kingdom	Lessay (GRI 6731)	54°54′41.949″N3°16′42.58″W	Master and Slave on 9 January 2016. Replacement for transmitter RugbyeLoran timing signal remains active.
Ash Shaykh Humayd	Saudi Arabia	Saudi Arabia South (GRI 7030) Saudi Arabia North (GRI 8830)	28°9′15.87″N34°45′41.36″E
Attu Island	United States	North Pacific (GRI 9990) Russian-American (GRI 5980) shut down	52°49′44″N173°10′49.7″E	demolishedAugust 2010
Balasore	India	Calcutta (GRI 5543)	21°29′11.02″N86°55′9.66″E
Barrigada	Guam	shut down	13°27′50.16″N144°49′33.4″E	demolished
Baudette	United States	shut down North Central U.S. (GRI 8290)Great Lakes (GRI 8970)	48°36′49.947″N94°33′17.91″W	dismantled
Berlevåg, Finnmark	Norway	Bø (GRI 7001) shut down	70°50′43.07″N29°12′16.04″E	shut down31 December 2015
Bilimora	India	Bombay (GRI 6042)	20°45′42.036″N73°2′14.48″E
Boise City	United States	shut down Great Lakes (GRI 8970) South Central U.S. (GRI 9610)	36°30′20.75″N102°53′59.4″W
Bø, Vesterålen	Norway	Bø (GRI 7001) Eiði (GRI 9007) shut down	68°38′6.216″N14°27′47.35″E	shut down31 December 2015,demolishedOctober 2016.
Cambridge Bay	Canada	shut down	69°6′52.840″N105°0′55.95″W	shut down;free-standing lattice tower still in use for anon-directional beacon,demolished
Cape Race	Canada	shut down Canadian East Coast (GRI 5930) Newfoundland East Coast (GRI 7270)	46°46′32.74″N53°10′28.66″W	used a 411.48 metre tall tower until 2 February 1993, now uses a 260.3 metre tall tower. The latter however, was shut down in 2012.Demolished
Caribou, Maine	United States	shut down Canadian East Coast (GRI 5930) Northeast U.S. (GRI 9960)	46°48′27.305″N67°55′37.15″W	demolished
Carolina Beach	United States	shut down Southeast U.S. (GRI 7980) Northeast US (GRI 9960)	34°3′46.208″N77°54′46.10″W	demolished
Chongzuo	China	China South Sea (GRI 6780)	22°32′35.8″N107°13′19″E
Comfort Cove	Canada	shut down Newfoundland East Coast (GRI 7270)	49°19′53.65″N54°51′43.2″W	demolished
Dana	United States	shut down Great Lakes (GRI 8970) Northeast US (GRI 9960)	39°51′7.64″N87°29′10.71″W
Dhrangadhra	India	Bombay (GRI 6042)	23°0′16.2″N71°31′37.64″E
Diamond Harbor	India	Calcutta (GRI 5543)	22°10′20.42″N88°12′15.8″E
Eiði	Faroe Islands	shut down Eiði (GRI 9007)	62°17′59.69″N7°4′25.59″W	demolished
Estaca de Vares	Spain	NATO "C" shut down	43.786348°N 7.679095°W/43.786348; -7.679095
Estartit	Spain	Mediterranean Sea (GRI 7990) shut down	42°3′36.63″N3°12′16.08″E	demolished
Fallon	United States	shut down U.S. West Coast (GRI 9940)	39°33′6.77″N118°49′55.6″W
Fox Harbour	Canada	shut down Canadian East Coast (GRI 5930) Newfoundland East Coast (GRI 7270)	52°22′35.29″N55°42′28.68″W	demolished
George	United States	shut down Canadian West Coast (GRI 5990) U.S. West Coast (GRI 9940)	47°3′48.096″N119°44′38.97″W
Gesashi	Japan	shut down North West Pacific (GRI 8930) East Asia (GRI 9930)	26°36′25.09″N128°8′56.94″E	demolished
Gillette	United States	shut down North Central U.S. (GRI 8290) South Central U.S. (GRI 9610)	44°0′11.21″N105°37′24″W
Grangeville	United States	shut down Southeast U.S. (GRI 7980) South Central U.S. (GRI 9610)	30°43′33.24″N90°49′43.01″W	dismantled
Havre	United States	shut down North Central U.S. (GRI 8290)	48°44′38.58″N109°58′53.3″W
Hellissandur	Iceland	shut down	64°54′14.793″N23°54′47.83″W	shut down31 December 1994; 411.48 metre tall tower now used forRÚVlongwavebroadcast on 189 kHz
Helong	China	China North Sea (GRI 7430)	42°43′11″N129°6′27.07″E
Hexian	China	China South Sea (GRI 6780)	23°58′3.21″N111°43′9.78″E
Iwo Jima	Japan	shut down	24°48′26.262″N141°19′34.76″E	shut downSeptember 1993;dismantled;used a 411.48 metre tall tower
Jan Mayen	Norway	Bø (GRI 7001) Ejde (GRI 9007) shut down	70°54′51.478″N8°43′56.52″W	shut down31 December 2015;demolishedOctober 2017.
Johnston Island	United States	shut down	16°44′43.82″N169°30′30.9″W	shut down, demolished
Jupiter	United States	shut down Southeast U.S. (GRI 7980)	27°1′58.49″N80°6′52.83″W	demolished
Kargaburun	Turkey	Mediterranean Sea (GRI 7990) shut down	40°58′20.51″N27°52′1.89″E	demolished
Kwang Ju	South Korea	East Asia (GRI 9930)	35°2′23.69″N126°32′27.2″E
Lampedusa	Italy	Mediterranean Sea (GRI 7990) shut down	35°31′22.11″N12°31′31.06″E	shut down
Las Cruces	United States	shut down South Central U.S. (GRI 9610)	32°4′18.1″N106°52′4.32″W
Lessay	France	Lessay (GRI 6731) Sylt (GRI 7499) shut down	49°8′55.27″N1°30′17.03″W	shut down31 December 2015,demolished
Loop Head	Ireland	Lessay (GRI 6731) Eiði (GRI 9007) never built	never built	250 kW;never built
Malone	United States	shut down Southeast U.S. (GRI 7980) Great Lakes (GRI 8970)	30°59′38.87″N85°10′8.71″W	dismantled
Middletown	United States	shut down U.S. West Coast (GRI 9940)	38°46′57.12″N122°29′43.9″W	demolished
Minami-Tori-shima	Japan	shut down North West Pacific (GRI 8930)	24°17′8.79″N153°58′52.2″E	used a 411.48 metre tall tower until 1985 demolished
Nantucket	United States	shut down Canadian East Coast (GRI 5930) Northeast U.S. (GRI 9960)	41°15′12.42″N69°58′38.73″W	demolished
Narrow Cape	United States	shut down 0) North Pacific (GRI 9990)	57°26′20.5″N152°22′10.2″W
Niijima	Japan	shut down North West Pacific (GRI 8930) East Asia (GRI 9930)	34°24′12.06″N139°16′19.4″E	demolished
Patapur	India	Calcutta (GRI 5543)	20°26′50.627″N85°49′38.67″E
Pohang	South Korea	North West Pacific (GRI 8930) East Asia (GRI 9930)	36°11′5.33″N129°20′27.4″E
Port Clarence	United States	Gulf of Alaska (GRI 7960) North Pacific (GRI 9990) shut down	65°14′40.372″N166°53′11.996″W	demolished28 April 2010; used a 411.48 metre tall tower
Port Hardy	Canada	shut down Canadian West Coast (GRI 5990)	50°36′29.830″N127°21′28.48″W	demolished
Rantum (Sylt)	Germany	Lessay (GRI 6731) Sylt (GRI 7499 ) shut down	54°48′29.94″N8°17′36.9″E	shut down31 Dec 2015
Raymondville	United States	shut down Southeast U.S. (GRI 7980) South Central U.S. (GRI 9610)	26°31′55.17″N97°49′59.52″W	dismantled
Raoping	China	China South Sea (GRI 6780) China East Sea (GRI 8390)	23°43′26.02″N116°53′44.7″E
Rongcheng	China	China North Sea (GRI 7430) China East Sea (GRI 8390)	37°03′51.765″N122°19′25.95″E
Rugby	United Kingdom	Experimental (GRI 6731) shut down	52°21′57.893″N1°11′27.39″W	shut downJuly 2007,demolished
Saint Paul	United States	shut down North Pacific (GRI 9990)	57°9′12.35″N170°15′6.06″W	demolished
Salwa	Saudi Arabia	Saudi Arabia South (GRI 7030) Saudi Arabia North (GRI 8830)	24°50′1.46″N50°34′12.54″E
Searchlight	United States	shut down South Central U.S. (GRI 9610) U.S. West Coast (GRI 9940)	35°19′18.305″N114°48′16.88″W	demolished
Sellia Marina	Italy	Mediterranean Sea (GRI 7990) shut down	38°52′20.72″N16°43′6.27″E	shut down
Seneca	United States	shut down Great Lakes (GRI 8970) Northeast U.S. (GRI 9960)	42°42′50.716″N76°49′33.30″W	dismantled
Shoal Cove	United States	shut down Canadian West Coast (GRI 5990) Gulf of Alaska (GRI 7960)	55°26′20.940″N131°15′19.09″W	dismantled
Soustons	France	Lessay (GRI 6731) shut down	43°44′23.21″N1°22′49.63″W	shut down31 December 2015,demolished
Tok	United States	shut down Gulf of Alaska (GRI 7960)	63°19′42.884″N142°48′31.34″W	demolished
Tokachibuto	Japan	shut down Eastern Russia Chayka (GRI 7950) North West Pacific (GRI 8930)	42°44′37.2″N143°43′10.5″E	dismantled
Upolo Point	United States	shut down	20°14′51.12″N155°53′4.34″W	shut down
Værlandet	Norway	Sylt (GRI 7499) Ejde (GRI 9007) shut down	61°17′49.49″N4°41′47.05″E	shut down31 December 2015; demolished 19 Sep 2017
Veraval	India	Bombay (GRI 6042)	20°57′09.316″N70°20′11.73″E
Williams Lake	Canada	shut down Canadian West Coast (GRI 5990) North Central U.S. (GRI 8290)	51°57′58.78″N122°22′1.55″W	dismantled
Xuancheng	China	China North Sea (GRI 7430) China East Sea (GRI 8390)	31°4′8.3″N118°53′8.78″E
Yap	Federated States of Micronesia	shut down	9°32′44.76″N138°9′53.48″E	shut down1987;demolished;used a 304.8 metre tower

See also

• Alpha (navigation),the Russian counterpart of the OMEGA Navigation System, still in use as of 2006.
• CHAYKA,the Russian counterpart of LORAN
• Decca Navigator System,a British system that usedphasedifference instead of time difference.
• Gee (navigation)
• Gee-H (navigation)
• Global Positioning System
• Local positioning system
• Oboe (navigation)
• Omega (navigation system),the Western counterpart of the Alpha Navigation System, no longer in use.
• SHORAN
• Tactical air navigation system
• Trilateration
• VHF omnidirectional range

References

Bibliography

• Department of Transportation and Department of Defense (February 2006)."2005 Federal Radionavigation Plan"(PDF).Archived fromthe original(PDF)on 9 May 2013.Retrieved26 February2006.
• Hefley, Gifford (1972).The Development of Loran-C Navigation and Timing.National Bureau of Standards.
• Blanchard, W. F. (September 1991). "Hyperbolic Airborne Radio Navigation Aids".Journal of Navigation:285–315.doi:10.1017/S0373463300010092.S2CID130079994.
• L. E. Gatterer"The Development of Loran-C Navigation and Timing",National Bureau of Standards, October 1972
• Conant, Jennet (2002).Tuxedo Park: A Wall Street tycoon and the secret palace of science that changed the course of World War II.New York: Simon & Schuster. pp.231–232.ISBN0-684-87287-0.
• Halford, John Alvin; Davidson, D.; Waldschmitt, J. A. (1948)."History of LORAN"(PDF).In Pierce, John Alvin; McKenzie, Alexander Anderson; Woodward, Richard Horace (eds.).LORAN: Long Range Navigation.Office of Scientific Research and Development, National Defence Research Committee. MIT Radiation Laboratory Series. Vol. 4. New York: McGraw Hill. pp. 19–51.

External links

• United States National Institute of Standards and Technology Site- Using LORAN C for time-keeping.
• European Loran-C network website
• LORAN-C Transmitter (Rantum)atStructurae
• Hellissandur Transmission ToweratStructurae:former LORAN-C transmitter mast, now used for longwave broadcasting
• LORAN-C facility antenna (Gillette, Wyoming)atStructurae
• LORAN-C facility antenna (Port Clarence, Alaska)atStructurae
• Jerry Proc, VE3FAB:Hyperbolic Radionavigation Systems:
  • In-depth discussion of the Loran-A system.Archived5 August 2009 at theWayback Machine
  • Histories of Loran-B, -D, and -F
  • Loran-C Introduction: eLoran
• Integrated GPS/Loran Prototypes for Aviation Applications
• The Migration to Enhanced or eLoran
• GNSS/eLoran for Timing and Frequencyby Locus, Inc.
• Loran's Capability to Mitigate the Impact of a GPS Outage on GPS Position, Navigation, and Time Applicationsby Locus, Inc.
• New Potential of Low-Frequency Radionavigation in the 21st CenturyPhD dissertation
• LORAN-C chains in serviceArchived6 February 2012 at theWayback Machine
• List of active LORAN-C transmitters
• SDR in action: The last LORAN-C receiveris a technical description of using asoftware-defined radioto decode LORAN-C signals
• New UK eLORAN service provision news articleNews article re: UK leading the way in eLORAN service provision.
• eLORAN vs Loran-CArchived7 October 2010 at theWayback MachineatInside GNSS—Short article describing the innovations in eLoran
• History of LORAN
• Dr. G. Linn Roth (October 1998)."The Case for Loran".International Loran Association. Archived fromthe originalon 27 January 2010.Retrieved18 July2010.