Active electronically scanned array
An active electronically scanned array (AESA), also known as active phased array radar is a type of phased array radar whose transmitter and receiver functions are composed of numerous small solid-state transmit/receive modules (TRMs). AESA radars aim their "beam" by emitting separate radio waves from each module that interfere constructively at certain angles in front of the antenna. Advanced AESA radars can improve on the older passive electronically scanned radars by spreading their signal emissions out across a band of frequencies, which makes it very difficult to detect over background noise, allowing ships and aircraft to broadcast powerful radar signals while still remaining stealthy.
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Radar systems generally work by connecting an antenna to a powerful radio transmitter to emit a short pulse of signal. The transmitter is then disconnected and the antenna is connected to a sensitive receiver which amplifies any echos from target objects. By measuring the time it takes for the signal to return, the radar receiver can determine the distance to the object. The receiver then sends the resulting output to a display of some sort. The transmitter elements were typically klystron tubes or magnetrons, which are suitable for amplifying or generating a narrow range of frequencies to high power levels. To scan a portion of the sky, the radar antenna must be physically moved to point in different directions.
Starting in the 1960s new solid-state devices capable of delaying the transmitter signal in a controlled way were introduced. That led to the first practical large-scale passive electronically scanned array (PESA), or simply phased array radar. PESAs took a signal from a single source, split it into hundreds of paths, selectively delayed some of them, and sent them to individual antennas. The radio signals from the separate antennas overlapped in space, and the interference patterns between the individual signals was controlled to reinforce the signal in certain directions, and mute it in all others. The delays could be easily controlled electronically, allowing the beam to be steered very quickly without moving the antenna. A PESA can scan a volume of space much quicker than a traditional mechanical system. Additionally, thanks to progress in electronics, PESAs added the ability to produce several active beams, allowing them to continue scanning the sky while at the same time focusing smaller beams on certain targets for tracking or guiding semi-active radar homing missiles. PESAs quickly became widespread on ships and large fixed emplacements in the 1960s, followed by airborne sensors as the electronics shrank.
AESAs are the result of further developments in solid-state electronics. In earlier systems the transmitted signal was originally created in a klystron or traveling wave tube or similar device, which are relatively large. Receiver electronics were also large due to the high frequencies that they worked with. The introduction of gallium arsenide microelectronics through the 1980s served to greatly reduce the size of the receiver elements, until effective ones could be built at sizes similar to those of handheld radios, only a few cubic centimeters in volume. The introduction of JFETs and MESFETs did the same to the transmitter side of the systems as well. Now an entire radar, the transmitter, receiver and antenna, could be shrunk into a single "transmitter-receiver module" (TRM) about the size of a carton of milk.
The primary advantage of an AESA over a PESA is capability of the different modules to operate on different frequencies. Unlike the PESA, where the signal is generated at single frequencies by a small number of transmitters, in the AESA each module generates and radiates its own independent signal. This allows the AESA to produce numerous "sub-beams" and actively "paint" a much larger number of targets. Additionally, the solid-state transmitters are able to transmit effectively at a much wider range of frequencies, giving AESAs the ability to change their operating frequency with every pulse sent out. AESAs can also produce beams that consist of many different frequencies at once, using post-processing of the combined signal from a number of TRMs to re-create a display as if there was a single powerful beam being sent.
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AESAs add many capabilities of their own to those of the PESAs. Among these are: the ability to form multiple beams, to use each TRM for different roles concurrently, like radar detection, and, more importantly, their multiple simultaneous beams and scanning frequencies create difficulties for traditional, correlation-type radar detectors.
Low probability of intercept
Radar systems work by sending out a signal and then listening for its echo off distant objects. Each of these paths, to and from the target, is subject to the inverse square law of propagation. That means that a radar's received energy drops with the fourth power of the distance, which is why radar systems require high powers, often in the megawatt range, to be effective at long range.
The radar signal being sent out is a simple radio signal, and can be received with a simple radio receiver. It is common to use such a receiver in the targets, normally aircraft, to detect radar broadcasts. Unlike the radar unit, which must send the pulse out and then receive its reflection, the target's receiver does not need the reflection and thus the signal drops off only as the square of distance. This means that the receiver is always at an advantage over the radar in terms of range - it will always be able to detect the signal long before the radar can see the target's echo. Since the position of the radar is extremely useful information in an attack on that platform, this means that radars generally must be turned off for lengthy periods if they are subject to attack; this is common on ships, for instance.
Turning that received signal into a useful display is the purpose of the "radar warning receiver" (RWR). Unlike the radar, which knows which direction it is sending its signal, the receiver simply gets a pulse of energy and has to interpret it. Since the radio spectrum is filled with noise, the receiver's signal is integrated over a short period of time, making periodic sources like a radar add up and stand out over the random background. The rough direction can be calculated using a rotating antenna, or similar passive array using phase or amplitude comparison. Typically RWRs store the detected pulses for a short period of time, and compare their broadcast frequency and pulse repetition frequency against a database of known radars. The direction to the source is normally combined with symbology indicating the likely purpose of the radar - airborne early warning, surface to air missile, etc.
This technique is much less useful against AESA radars. Since the AESA (or PESA) can change its frequency with every pulse (except when using doppler filtering), and generally does so using a pseudo-random sequence, integrating over time does not help pull the signal out of the background noise. Moreover, AESA radars may extend the duration of the pulse and lower their peak power. This makes no difference to the total energy reflected by the target but makes the detection of the pulse by an RWR system less likely. Nor does the AESA have any sort of fixed pulse repetition frequency, which can also be varied and thus hide any periodic brightening across the entire spectrum. Older generation RWRs are essentially useless against AESA radars, which is why AESA's are also known as 'low probability of intercept radars. Modern RWRs must be made highly sensitive (small angles and bandwidths for individual antennas, low transmission loss and noise) and add successive pulses through time-frequency processing to achieve useful detection rates.
AESA radars can be much more difficult to detect that they can broadcast continually and still have a very low chance of being detected. This allows such radar systems to generate far more data than traditional radar systems, which can only receive data periodically, greatly improving overall system effectiveness.
High jamming resistance
Jamming is likewise much more difficult against an AESA. Traditionally, jammers have operated by determining the operating frequency of the radar and then broadcasting a signal on it to confuse the receiver as to which is the "real" pulse and which is the jammer's. This technique works as long as the radar system cannot easily change its operating frequency. When the transmitters were based on klystron tubes this was generally true, and radars, especially airborne ones, had only a few frequencies to choose among. A jammer could listen to those possible frequencies and select the one to be used to jam.
Most radars using modern electronics are capable of changing their operating frequency with every pulse. An AESA has the additional capability of spreading its frequencies across a wide band even in a single pulse ( within a single pulse is called chirp), which can make jamming more difficult, although it is possible to send out broadband white noise against all the possible frequencies, reducing the jammer's effectiveness. In fact, AESAs can then be switched to a receive-only mode, and use these powerful jamming signals instead to track its source, something that required a separate receiver in older platforms.
However, using a single receiving antenna only gives a direction. Obtaining a range and a target vector requires at least two physically separate passive devices for triangulation to provide instantaneous determinations. Target motion analysis can estimate these quantities by incorporating many directional measurements over time, along with knowledge of the position of the receiver and constraints on the possible motion of the target.
By integrating received signals from the targets along with a lower rate of data from its own broadcasts, an AESA radar can generate more data with less energy.
Since each element in an AESA is a powerful radio receiver, active arrays have many roles besides traditional radar. One use is to dedicate several of the elements to reception of common radar signals, eliminating the need for a separate radar warning receiver. The same basic concept can be used to provide traditional radio support, and with some elements also broadcasting, form a very high bandwidth data link. The F-35 uses this mechanism to send sensor data between aircraft in order to provide a synthetic picture of higher resolution and range than any one radar could generate. In 2007, tests by Northrop Grumman, Lockheed Martin, and L-3 Communications enabled the AESA system of a Raptor to act like a WiFi access point, able to transmit data at 548 megabits per second and receive at gigabit speed; this is far faster than the Link 16 system used by US and allied aircraft, which transfers data at just over 1 Mbit/s.
AESAs are also much more reliable than either a PESA or older designs. Since each module operates independently of the others, single failures have little effect on the operation of the system as a whole. Additionally, the modules individually operate at low powers, perhaps 40 to 60 watts, so the need for a large high-voltage power supply is eliminated.
Replacing a mechanically scanned array with a fixed AESA mount (such as on the F/A-18E/F Super Hornet) can help reduce an aircraft's overall radar cross-section (RCS), but some designs (such as the Eurofighter Typhoon) forgo this advantage in order to combine mechanical scanning with electronic scanning and provide a wider angle of total coverage.
The highest Field of View (FOV) for a flat phased array antenna is currently 120°, however this can be combined with mechanical steering as noted above.
List of existing systems
US based manufacturers of the AESA radars used in the F22 and Super Hornet include Northrop Grumman and Raytheon. These companies also design, develop and manufacture the transmit/receive modules which comprise the 'building blocks' of an AESA radar. The requisite electronics technology was developed in-house via Department of Defense research programs such as MIMIC Program.
- Northrop Grumman
- AN/APG-77, for the F-22 Raptor
- AN/APG-80, for the F-16E/F Desert Falcon
- AN/APG-81, for the F-35 Lightning II
- Multirole AESA, for the Boeing Wedgetail (AEW&C)
- AN/ASQ-236 Podded AESA Radar
- AN/ZPY-1 STARLite Small Tactical Radar - Lightweight, for manned and unmanned aircraft
- SABR, for F-16 Fighting Falcon upgrades
- AMSAR, research from the European GTDAR consortium, for Eurofighter and Rafale fighter Radar
- Captor-E CAESAR (CAPTOR Active Electronically Scanning Array Radar)
- RBE2-AA Radar à Balayage Electronique 2 - Active Array
- Mitsubishi Electric Corporation
- HPS-106, air & surface search radar, for the Kawasaki P-1 maritime patrol aircraft, four antenna arrays.
- Phazotron NIIR Zhuk-AE, for MiG-35
- Tikhomirov NIIP AESA radar, for Sukhoi T-50
- EL/M-2083 aerostat-mounted air search radar
- EL/M-2052, for fighters. Interim candidate for HAL Tejas. Also, suitable for F-15, MiG-29 & Mirage 2000
- EL/M-2075 radar for the IAI Phalcon AEW&C system
- EL/W-2085 advanced version of the radar for the EL/M-2075, used on the Gulfstream G550
- EL/W-2090 similar to the EL/W-2085, only used on the Ilyushin Il-76
- NRIET (Nanjing Research Institute of Electronic Technology/14 institute) designed radars for
Ground and Maritime based systems
- APAR (active phased array radar): Thales' multifunction radar is the primary sensor of the Royal Netherlands Navy's De Zeven Provinciën class frigates, the German Navy's Sachsen class frigates, and the Royal Danish Navy's Ivar Huitfeldt class frigates. APAR is the first active electronically scanned array multifunction radar employed on an operational warship.
- Selex EMPAR (European Multifunction Phased Array Radar)
- Northrop Grumman
- MEADS's fire control radar
- Type H/LJG-346(8) on Chinese aircraft carrier Liaoning
- Type 348 Radar on Type 052C destroyer
- AESA radar on Type 052D destroyer
- H/LJG-346 SAPARS (Predecessor to the Type 348 Radar on Type 052C destroyer)
- Type 305A Radar (Acquisition radar for the HQ-9 missile system)
- YLC-2 Radar
- THAAD system fire control radar
- Type-03 Medium Range Surface-to-Air MissileSystem (Chu-SAM,SAM-4) multifunction radar
- BAE Systems Insyte SAMPSON multifunction radar for UK Type 45 destroyers
- FCS-3 Mitsubishi Electric Corporation (Melco)
- OPS-24 Mitsubishi Electric Corporation (The world's first Naval Active Electronically Scanned Array radar)
- J/FPS-3 Japanese main ground-based air defense radar produced by Melco
- J/FPS-4 Cheaper than J/FPS-3, produced by Toshiba
- J/FPS-5 Japanese ground-based next-generation missile defense radar
- J/TPS-102 Self-propelled ground-based radar, cylindrical array antenna, NEC
- JMPQ-P13 Counter-battery radar, Toshiba
- JTPS-P14 Transportable air defence radar, Melco
- JTPS-P16 Firefinder radar, Melco
- CEAFAR CEA Technologies A 4th generation multifunction digital active phased array radar, installed on HMAS Perth and to be installed on all ANZAC class frigates.
- NNIIRT 1L119 Nebo SVU mobile AESA 3-dimensional surveillance radar
- VNIIRT Gamma DE mobile 3-dimensional solid-state AESA surveillance radar
- 50N6A multifunctional radar of the Vityaz missile system
- Multi-function radar of the KM-SAM
- The ABCs of Radar
- Page, Lewis. "F-22 superjets could act as flying Wi-Fi hotspots." The Register, 19 June 2007. Retrieved: 7 November 2009.
- F/A-18 AESA - New Technology Revolutionizes Radar Benefits
- Physical limitation of the maximum swivel angle of an AESA
- Northrop Grumman Successfully Completes F-22 Radar Flight-Test Certification
- Raytheon Company: Products & Services: AESA Technology
- A DARPA Perspective on the Future of Electronics
- http://www.ausairpower.net/APA-PLA-AWACS-Programs.html PLA-AF Airborne Early Warning & Control Programs
- http://cnair.top81.cn/J-10_J-11_FC-1.htm#j-10b Chinese Military Aviation - Fighters (Cont.)
- Jane's Navy International, August 2010, "Expanding coverage from sea to sky"
- http://www.ausairpower.net/APA-HQ-9-12-Battery-Radars.html HQ-9 and HQ-12 SAM system battery radars
- PLA Air Defence Radars