In telecommunications, identification, friend or foe (IFF) is an identification system designed for command and control. It enables military and national (civilian-located ATC) interrogation systems to identify aircraft, vehicles or forces as friendly and to determine their bearing and range from the interrogator. IFF may be used by both military and civilian aircraft.
IFF was first developed during World War II. The term is something of a misnomer, as IFF can positively identify friendly targets but not hostile ones. If an IFF interrogation receives no reply or an invalid reply, the object cannot be identified as friendly but is not positively identified as a foe.
There are many reasons for friendly aircraft not to reply to IFF, such as battle damage or equipment failure, loss of encryption keys, and wrong encryption keys. Terrain-hugging aircraft are very often poor candidates for microwave line-of-sight systems such as the IFF system. Microwaves cannot penetrate terrain, and very often atmospheric effects (referred to as anomalous propagation) cause timing, range, and azimuth issues.
History[edit | edit source]
The world's first IFF, FuG 25a "Erstling" (English: "Debut"), was developed in Germany in 1940. It received the radar frequencies on 125 MHz (Freya radar) and 550-580 MHz (Würzburg radar). To start the identification procedure, the ground operator switched the pulse frequency of his radar from 3,750 Hz to 5,000 Hz.
The airborne receiver decoded that and started to transmit its code. Before departure, two mechanical keys of ten bits each were inserted into the shown reader. The IFF transmitter worked on 168 MHz with a power of 400 Watt (PEP). Unfortunately for the Germans, British military scientists designed and built their own IFF transmitter called "Perfectos", which was designed to trigger a response from any FuG 25a systems in the vicinity. When mounted in an RAF Mosquito, the "Perfectos" device revealed the position of any German nightfighters fitted with an FuG 25a. As a result, the British "Perfectos" device severely compromised German use of the FuG 25a.
The IFF of World War II and Soviet military systems (1946 to 1991) used coded radar signals (called Cross-Band Interrogation, or CBI) to automatically trigger the aircraft's transponder in an aircraft illuminated by the radar. Radar-based IFF is also called secondary radar, with primary radar bouncing an RF pulse off of the aircraft to determine position. George Charrier, working for RCA, filed for a patent for such an IFF device in 1941 that required the operator to perform several adjustments to the radar receiver in order to suppress the image of the natural echo on the radar receiver in order to visually examine the IFF signal. By 1943, Donald Barchok filed a patent for a radar system using the acronym IFF in his text with only parenthetic explanation, indicating that this acronym had become an accepted term. In 1945, Emile Labin and Edwin Turner filed patents for radar IFF systems where the outgoing radar signal and the transponder's reply signal could each be independently programmed with a binary codes by setting arrays of toggle switches; this allowed the IFF code to be varied from day to day or even hour to hour.
Early 21st century systems[edit | edit source]
An IFF system must obviously be standardised so that all allied users can recognise each other.
NATO[edit | edit source]
The United States and other NATO countries started using a system called Mark XII in the late twentieth century; Britain had not until then implemented an IFF system compatible with that standard, but then developed a program for a compatible system known as successor IFF (SIFF).
The systems used in the early twenty-first century by NATO and allied powers use a separate specialized transponder beacon which can operate without radar. They are referred to as cross-band beacon or transponders.
IFF is used by both military and civilian aircraft. Modes 1, 2, 4 and 5 are for military use only. Modes 1, 2 and 3/A are collectively known as Selective Identification Feature (SIF) modes. Civilian aircraft use modes 3/A, C and S. Mode C which includes barometric pressure altitude information is often used in conjunction with mode 3/A. Mode S is a new civilian mode developed to replace both mode 3/A and C.
An IFF transponder receives interrogation pulses at one frequency, and sends the reply pulses at a different frequency (1030 MHz and 1090 MHz in the MK XII system.). In modes 1, 2, 3/A, and C, the interrogator challenge is composed of two pulses spaced apart by a different amount for each mode, with the transponder reply being a long series of bits; in the encrypted military mode 4, the IFF interrogation is instead a long series of bits that contains the encrypted message and parity, and the reply is just three pulses.
If no encrypted mode 4 or 5 reply is received from the IFF transponder, the nature of the target continues to be unknown. The IFF system does not definitively declare a target hostile if it does not reply correctly: pilots may have the wrong code (encryption key) selected, or be using an expired code. They will have an audible and visual alarm every time they are interrogated by IFF; if they cannot clear the alarm they have a defined pre-briefed safe passage procedure to follow.
Modes[edit | edit source]
Mode 1 – provides 2-digit octal mission code. (military only – can be changed in flight)
Mode 2 – provides 4-digit octal unit code. (military only – can't be changed in flight)
Mode 3/A – provides a 4-digit octal identification code for the aircraft, assigned by the air traffic controller. (military and civilian)
Mode 4 – provides a 3-pulse reply to crypto coded challenge. (military only)
Mode 5 – provides a cryptographically secured version of Mode S and ADS-B GPS position. (military only) Mode 5 is divided into two levels. Both are crypto-secure with Enhanced encryption, Spread Spectrum Modulation, and Time of Day Authentication. Level 1 is similar to Mode 4 information but enhanced with an Aircraft Unique PIN. Level 2 is the same as Mode 5 level one but includes additional information such as Aircraft Position and Other Attributes.
Mode C – provides 4-digit octal code for aircraft's pressure altitude. (military and civilian)
Mode S – provides multiple information formats to a selective interrogation. Typically aircraft are assigned a unique 24-bit Mode S address. The Mode S address is partitioned and a group of address ranges are allocated to each country. Some countries change the assigned address for security reasons, and thus it might not be a unique address. (military and civilian)
Modes 4 and 5 are designated for use by NATO forces.
See also[edit | edit source]
- Automatic target recognition
- List of World War II electronic warfare equipment
- Secondary surveillance radar
References[edit | edit source]
- George M. Charrier, Recognition System for Pulse Echo Radio Locators, U.S. Patent 2,453,970, granted Nov. 16, 1948.
- Donald Barchok, Means for Synchronizing Detection and Interrogation Systems, U.S. Patent 2,515,178, granted July 18, 1950.
- Emile Labin, Magnetostrictive Time-Delay Device, U.S. Patent 2,495,740, granted Jan. 31, 1950.
- Edwin E. Turner, Coded Impulse Responsive Secret Signalling System, U.S. Patent 2,648,060, granted Aug. 4, 1953.
- NATO STANAG 4193
- This article incorporates public domain material from the General Services Administration document "Federal Standard 1037C".
- This article incorporates public domain material from the United States Department of Defense document "Dictionary of Military and Associated Terms".
[edit | edit source]
- The short film STAFF FILM REPORT 66-27A (1966) is available for free download at the Internet Archive [more]
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