Atactical air navigation system,commonly referred to by theacronymTACAN,is anavigationsystem initially designed for naval aircraft to acquire moving landing platforms (i.e., ships) and later expanded for use by other military aircraft. It provides the user with bearing and distance (slant-range or hypotenuse) to a ground or ship-borne station. It is, from an end-user perspective, a more accurate version of theVOR/DMEsystem that providesbearingandrangeinformation forcivil aviation.The DME portion of the TACAN system is available for civil use; atVORTACfacilities where a VOR is combined with a TACAN, civil aircraft can receive VOR/DME readings. Aircraft equipped with TACANavionicscan use this system for enroute navigation as well asnon-precision approachesto landing fields. However, a TACAN-only equipped aircraft cannot receive bearing information from a VOR-only station.
History
editThe TACAN navigation system is an evolution ofradiotranspondernavigation systems that date back to the BritishOboe systemofWorld War II.In the United States, many companies were involved with the development of TACAN for military aircraft. Hoffman Laboratories Div. of theHoffman Electronics Corp.–Military Products Division[1](now NavCom Defense Electronics)[2]was a leader in developing the present TACAN system in the US starting in the late 1950s.
Operation
editTACAN in general can be described as the military version of the VOR/DME system, though despite providing similar information as its civilian counterpart, its method of operation is significantly different. It operates in theUHFfrequencyband 962-1213MHz,utilizing a pulse-pair transponder system not dissimilar to that ofsecondary surveillance RADAR.Interrogating aircraft transmit in the 1024-1150 MHz band, split into 1 MHz channels numbered 1-126; the responding station (ground, ship, or another aircraft) is 63 MHz (63 channels) above or below the originating frequency, depending on the channel and mode of operation selected. Spacing between pulses in an individual pulse-pair is also determined by TACAN operating mode.
Ranging
editRange information is functionally identical to the method provided by civilian DME: pairs of 3.5 microsecond (μs) pulses (measured edge-to-edge at 50% modulation strength) from an aircraft are repeated by the station being interrogated, using the round-trip time to calculate slant-range distance. Randomized spacing between interrogation pulse-pairs allows the interrogator to separate its own signal from that of other aircraft, enabling multiple users to access the ranging function without mutual interference. A fixed-round trip delay time (dependent on system mode) is added to each pulse-pair when being retransmitted by its station. The interrogator will generate up to 150 pulse-pairs per second when first acquiring a station in range in "search" mode, then drop down to ≈30 per second when acquired in "track" mode. Memory circuits in the ranging function enable a track to be quickly reestablished when ranging pulses are temporarily suppressed by other TACAN functions (see below).
Bearing
editBearing information is derived fromamplitude modulation(AM) of the responding station's pulse-pair signals, the AM signal being generated via physical rotation of a station's directional antenna or electronic steering of the same signal using an antenna array. Two AM signals are generated: a fundamental AM signal at 15 Hz, and an auxiliary AM signal (implemented using fixed signal reflectors in rotating-antenna installations) at 135 Hz, the ninthharmonicof the fundamental signal. These correspond to a "coarse" and "fine" bearing signal, the latter improving the accuracy of the former. The time is compared between the point of peak positive signal strength with a reference train or "burst" of pulse-pairs of specific repetition rate and duration, timed to transmit at a specific point in the signal's sweep; these replace all other pulse types when transmitted. The civilian VOR system differs from TACAN in utilizing a single continuous-wave 30 Hz modulation signal, using the phase difference between a fixed-phase and variable phase (rotating) component to derive bearing info.
Squitter function
editTACAN stations transmit pulse-pairs at a composite rate of 3600 pairs/second: 900 of which are bearing reference bursts, and the other 2700 being composed of ranging and identification pulses. When insufficient interrogation pulses from aircraft are present, the station will use asquittercircuit to inject additional randomized pulse-pairs to maintain the desired pulse rate. This ensures that sufficient signal is present to support demodulating bearing signals.
Identification
editTACAN stations are identified byMorse code.The transmitting station periodically replaces the randomized ranging pulse-pairs with regularly spaced pairs that de-modulate to a 1350 Hz tone, keying a three-letter identification code at approximately 6-7 wpm every 40 seconds. Ranging and squitter pulses are permitted during the gaps between dots and dashes. There is no capability for voice transmission in a TACAN-only system.
Operating modes
editThere are two basic channel configurations available: X (the original implementation) and Y (added in the 1960s to expand available channels and reduce mutual interference between closely-spaced stations). These configurations differ in pulse-pair width, fixed receiver response delay, and polarity of frequency offset from the interrogation channel. TACAN interrogators can operate in four modes: receive (for bearing/identification only), transmit/receive (for bearing, range, and ID), and air-to-air versions of the previous two.
The typical TACAN onboard user panel has control switches for setting the channel (corresponding to the desired station's assigned frequency), the operation mode for either transmit/receive (T/R, to get both bearing and range) or receive only (REC, to get bearing but not range). Capability was later upgraded to include an air-to-air mode (A/A), where two airborne users can get relative slant-range information depending on specific installations,[3]though an air-to-air mode allows distance to be established between transmitters/receivers.
Channel/operating mode | Interrogator frequency (MHz)/channel | Response frequency offset (±63 MHz) | Interrogator pulse-pair width (μs) | Response delay spacing (μs) | Response pulse-pair width (μs) | Main/auxiliary reference burst length (pulse pairs) | Main/auxiliary reference burst pulse-pair spacing (μs) | Main/auxiliary reference burst synchronization point |
---|---|---|---|---|---|---|---|---|
X channels, air-to-ground | 1025-1150 (1-126) | negative (1-63) positive (64-127) |
12 | 50 | 12 | 12/6 | 12/24 | Positive peak of AM signal pointed due east when main burst triggered; auxiliary burst synchronized to same event, but suppressed during main burst transmission |
Y channels, air-to-ground | positive (1-63) negative (64-127) |
36 | 74 | 30 | 13/13 | 30/15 (both single pulse) | ||
X channels, air-to-air | 12 | 62 | single pulse | Same as air-to-ground, if supported | ||||
Y channels, air-to-air | 24 | 74 |
Performance and accuracy
editWhen initially deployed, TACAN was intended to provide a bearing accuracy of ±0.22°, based on the main bearing signal's own accuracy of ±2° and the corrections applied by the ninth-harmonic auxiliary bearing signal.[5]Theoretically a TACAN should provide a 9-fold increase inaccuracycompared to a VOR, but operational use has shown only an approximate 3-fold increase.[6]
Operational accuracy of the 135 Hz azimuth component is ±1° or ±63 m at 3.75 km.[7]
Manufacturers of TACAN sets mention the ability to track stations out to 400NM, though these systems will cap their instrumented range signals at approximately 200NM.[8]Per official FAA service volume information, reliable TACAN/DME reception can be guaranteed out to 130NM below 45,000 feet above the surface for a high-altitude certified unit.[9]
On the firstSpace Shuttleflight,CapcomJoseph P. Allenreported up to the crew that their TACANs had locked onto the Channel 111X signals atSt. Petersburg,FL at a range of 250 miles.
Benefits
editBecause the azimuth and range units are combined in one system it provides for simpler installation. Less space is required than a VOR because a VOR requires a large counterpoise and a fairly complex phased antenna system. A TACAN system theoretically might be placed on a building, a large truck, an airplane or a ship, and be operational in a short period of time. An airborne TACAN receiver can be used in air-to-air mode to provide the approximate distance between two coordinating aircraft by selecting channels with 63 channels of separation (e.g., aircraft #1 sets channel 29 into its TACAN and aircraft #2 sets channel 92 into its TACAN.). It does not provide relative bearing.
Drawbacks
editFor military usage a primary drawback is lack of the ability to control emissions (EMCON) and stealth. Naval TACAN operations are designed so an aircraft can find the ship and land. Since there is no encryption, an enemy can use the range and bearing provided to attack a ship equipped with a TACAN. Some TACANs have the ability to employ a "Demand Only" mode: only transmitting when interrogated by an aircraft on-channel. It is likely that TACAN will be replaced with a differential GPS system similar to theLocal Area Augmentation Systemcalled JPALS. TheJoint Precision Approach and Landing Systemhas a low probability of intercept to prevent enemy detection and an aircraft carrier version can be used forautolandoperations.
Some systems used in the United States modulate the transmitted signal by using a 900 RPM rotating antenna. Since this antenna is fairly large and must rotate 24 hours a day, possibly causing reliability issues. Modern systems have antennas that use electronic rotation (instead of mechanical rotation), hence no moving parts.
See also
editReferences
edit- ^Missiles and Rockets,July 20, 1959, v. 5, no. 30, p. 127.
- ^http://www.navcom.com/NavCom Defense Electronics
- ^Rockwell International (July 7, 1992)."Aircraft rendezvous using low data rate two-way TACAN information".Archived fromthe originalon June 12, 2011.
- ^"MIL-STD-291 C TACTICAL AIR NAVIGATION SIGNAL".everyspec.com.Retrieved2024-03-18.
- ^TACAN Operation - US Navy Training Film 1955,11 September 2021,retrieved2024-03-18
- ^Helfrick, Albert D. (2007).Principles of Avionics(4th ed.). Avionics Communications Inc. p. 62.ISBN978-1-885544-26-1.Retrieved2023-05-29.
- ^Department of Transportation and Department of Defense (March 25, 2002)."2001 Federal Radionavigation Systems"(PDF).RetrievedNovember 27,2005.
- ^"TACAN+ | Tactical Airborne Navigation System | L3Harris".www.l3harris.com.Retrieved2024-03-18.
- ^"Navigation Aids".Aeronautical Information Manual.Federal Aviation Administration.Retrieved2024-03-17.
External links
edit- Tactical Air Navigation- 1955 USN training film on TACAN, including information on the AN/URN-3 ground-based station
- dB Systems, Inc. - Manufacturer of mechanically scanned, electronically scanned, shipboard, man-portable, and tactical TACAN Antennas- Complete TACAN Antenna profile with datasheets and photos
- Rantec Microwave Systems - Manufacturer of non-rotating TACAN antennas- Complete with antenna internal photos and specs
- Moog Navigation and Surveillance SystemsArchived2014-11-29 at theWayback Machine- Fixed site, shipboard, mobile and man-portable TACAN systems
- Leonardo Air Traffic Management- Fixed site TACAN systems