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Pulse-Doppler radar

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216: 970: 1630: 20: 183: 873:. Non-Doppler radar systems cannot be pointed directly at the ground due to excessive false alarms, which overwhelm computers and operators. Sensitivity must be reduced near clutter to avoid overload. This vulnerability begins in the low-elevation region several beam widths above the horizon, and extends downward. This also exists throughout the volume of moving air associated with weather phenomenon. 1527: 836: 1204: 673:
Rejection speed is selectable on pulse-Doppler aircraft-detection systems so nothing below that speed will be detected. A one degree antenna beam illuminates millions of square feet of terrain at 10 miles (16 km) range, and this produces thousands of detections at or below the horizon if Doppler
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Mechanical RF components, such as wave-guide, can produce Doppler modulation due to phase shift induced by vibration. This introduces a requirement to perform full spectrum operational tests using shake tables that can produce high power mechanical vibration across all anticipated audio frequencies.
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generally appears in a circular region within a radius of about 25 miles (40 km) near ground-based radar. This distance extends much further in airborne and space radar. Clutter results from radio energy being reflected from the earth surface, buildings, and vegetation. Clutter includes weather
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Pulse-Doppler radar uses the following signal processing criteria to exclude unwanted signals from slow-moving objects. This is also known as clutter rejection. Rejection velocity is usually set just above the prevailing wind speed (10 to 100 mph or 20 to 160 km/h). The velocity threshold
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starting in the 1960s. Earlier radars had used pulse-timing in order to determine range and the angle of the antenna (or similar means) to determine the bearing. However, this only worked when the radar antenna was not pointed down; in that case the reflection off the ground overwhelmed any returns
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antenna. This is because the phase-shifter elements in the antenna are non-reciprocal and the phase shift must be adjusted before and after each transmit pulse. Spurious phase shift is produced by the sudden impulse of the phase shift, and settling during the receive period between transmit pulses
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Tracking radar systems use angle error to improve accuracy by producing measurements perpendicular to the radar antenna beam. Angular measurements are averaged over a span of time and combined with radial movement to develop information suitable to predict target position for a short time into the
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A helicopter appears like a rapidly pulsing noise emitter except in a clear environment free from clutter. An audible signal is produced for passive identification of the type of airborne object. Microwave Doppler frequency shift produced by reflector motion falls into the audible sound range for
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Search radar that include pulse-Doppler are usually dual mode because best overall performance is achieved when pulse-Doppler is used for areas with high false alarm rates (horizon or below and weather), while conventional radar will scan faster in free-space where false alarm rate is low (above
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Range and velocity cannot be measured directly using medium PRF, and ambiguity resolution is required to identify true range and speed. Doppler signals are generally above 1 kHz, which is audible, so audio signals from medium-PRF systems can be used for passive target classification.
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is adjusted to smooth the leading edge and trailing edge so that RF power is increased and decreased without an abrupt change. This creates a transmit pulse with smooth ends instead of a square wave, which reduces ringing phenomenon that is otherwise associated with target reflection.
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The pulse-Doppler radar equation can be used to understand trade-offs between different design constraints, like power consumption, detection range, and microwave safety hazards. This is a very simple form of modeling that allows performance to be evaluated in a sterile environment.
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Pulse-Doppler radar by itself can be too slow to cover the entire volume of space above the horizon unless fan beam is used. This approach is used with the AN/SPS 49(V)5 Very Long Range Air Surveillance Radar, which sacrifices elevation measurement to gain speed.
94:, they are used for discriminating aircraft from clutter. Besides the above conventional surveillance applications, pulse-Doppler radar has been successfully applied in healthcare, such as fall risk assessment and fall detection, for nursing or clinical purposes. 1496:
from mountains, buildings or wave tops can be used to detect fast moving objects otherwise blocked by solid obstruction along the line of sight. This is a very lossy phenomenon that only becomes possible when radar has significant excess sub-clutter visibility.
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system with 1024 elements provides 30.103 dB of improvement due to the type of signal processing that must be used with pulse-Doppler radar. The energy of all of the individual pulses from the object are added together by the filtering process.
915:(MTI) provide up to 25 dB sub-clutter visibility. An MTI antenna beam is aimed above the horizon to avoid an excessive false alarm rate, which renders systems vulnerable. Aircraft and some missiles exploit this weakness using a technique called 1710: 1143: 2154:
Once in track mode, pulse-Doppler radar must include a way to modify Doppler filtering for the volume of space surrounding a track when radial velocity falls below the minimum detection velocity. Doppler filter adjustment must be linked with a
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for sub-clutter visibility. Phase shifter settling time on the order of 50ns is required. Start of receiver sampling needs to be postponed at least 1 phase-shifter settling time-constant (or more) for each 20 dB of sub-clutter visibility.
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from other objects. As the ground moves at the same speed but opposite direction of the aircraft, Doppler techniques allow the ground return to be filtered out, revealing aircraft and vehicles. This gives pulse-Doppler radars "
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The signal processing enhancement of pulse-Doppler allows small high-speed objects to be detected in close proximity to large slow moving reflectors. To achieve this, the transmitter must be coherent and should produce low
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Detection range is increased proportional to the fourth root of the number of filters for a given power consumption. Alternatively, power consumption is reduced by the number of filters for a given detection range.
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Scalloping for pulse-Doppler radar involves blind velocities created by the clutter rejection filter. Every volume of space must be scanned using 3 or more different PRF. A two PRF detection scheme will have
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The earliest radar systems failed to operate as expected. The reason was traced to Doppler effects that degrade performance of systems not designed to account for moving objects. Fast-moving objects cause a
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Most antenna phase shifters operating at PRF above 1 kHz introduce spurious phase shift unless special provisions are made, such as reducing phase shifter settling time to a few dozen nanoseconds.
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Subclutter visibility involves the maximum ratio of clutter power to target power, which is proportional to dynamic range. This determines performance in heavy weather and near the earth surface.
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Tracking will cease without this feature because the target signal will otherwise be rejected by the Doppler filter when radial velocity approaches zero because there is no change in frequency.
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Pulse-Doppler antenna motion must be slow enough so that all the return signals from at least 3 different PRFs can be processed out to the maximum anticipated detection range. This is known as
831:{\displaystyle \left\vert {\frac {{\text{Doppler frequency}}\times C}{2\times {\text{transmit frequency}}}}-{\text{ground speed}}\times \cos \Theta \right\vert >{\text{velocity threshold}},} 203:
Pulse-Doppler systems measure the range to objects by measuring the elapsed time between sending a pulse of radio energy and receiving a reflection of the object. Radio waves travel at the
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capability, and pulse-Doppler is the only strategy that can satisfy this requirement. This eliminates vulnerabilities associated with the low-elevation and below-horizon environment.
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A special mode is required because the Doppler velocity feedback information must be unlinked from radial movement so that the system can transition from scan to track with no lock.
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Signal processing for a 1024-point filter improves performance by 30.103 dB, assuming compatible transmitter and antenna. This corresponds to 562% increase in maximal distance.
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In addition to this sampling limit, the duration of the transmitted pulse could mean that returns from two targets will be received simultaneously from different parts of the pulse.
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sound for the operator in track mode on some radar systems. The operator uses this sound for passive target classification, such as recognizing helicopters and electronic jamming.
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that minimizes ringing that occurs any time pulses are applied to a filter. In a digital system, this adjusts the phase and/or amplitude of each sample before it is applied to the
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Tactical missile aerodynamics, Volume 141. P17. Michael J. Hemsch, American Institute of Aeronautics and Astronautics. American Institute of Aeronautics and Astronautics, 1992
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Pulse-Doppler signal processing introduces a phenomenon called scalloping. The name is associated with a series of holes that are scooped-out of the detection performance.
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Radar systems require angular measurement. Transponders are not normally associated with pulse-Doppler radar, so sidelobe suppression is required for practical operation.
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The velocity resolution is the minimal radial velocity difference between two objects traveling at the same range before the radar can detect two discrete reflections:
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Scan time is a critical factor for some systems because vehicles moving at or above the speed of sound can travel one mile (1.6 km) every few seconds, like the
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are not appropriate because noise introduced by these devices interfere with detection performance. The only amplification devices suitable for pulse-Doppler are
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engines, and which was armed with a W40 nuclear weapon to destroy entire formations of attacking enemy aircraft. Pulse-Doppler systems were first widely used on
1199:{\displaystyle {\text{velocity resolution}}={\frac {C\times {\text{PRF}}}{2\times {\text{transmit frequency}}\times {\text{filter size in transmit pulses}}}}.} 2137:
used for that purpose, like A-scope, B-scope, C-scope, and RHI indicator. The human ear may be able to tell the difference better than electronic equipment.
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The range resolution is the minimal range separation between two objects traveling at the same speed before the radar can detect two discrete reflections:
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selectively excludes low-velocity reflections so that no detections occurs below a threshold velocity. This eliminates terrain, weather, biologicals, and
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Choppy surfaces, like waves and trees, form a diffraction grating suitable for bending microwave signals. Pulse-Doppler can be so sensitive that
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The antenna type is an important consideration for multi-mode radar because undesirable phase shift introduced by the radar antenna can degrade
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This allows the radar to separate the reflections from multiple objects located in the same volume of space by separating the objects using a
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A small fast-moving target reflection can be detected in the presence of larger slow-moving clutter reflections when the following is true:
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Similar techniques are required to develop track information for jamming signals and interference that cannot satisfy the lock criterion.
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It became possible to use pulse-Doppler radar on aircraft after digital computers were incorporated in the design. Pulse-Doppler provided
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uses variable density in the air column above the surface of the earth to bend RF signals. An inversion layer can produce a transient
141:, but more sophisticated techniques were developed that record the phase of each transmitted pulse for comparison to returned echoes. 137:, and solid state devices. Early pulse-dopplers were incompatible with other high power microwave amplification devices that are not 2537: 2364: 1844:{\displaystyle R=\left({\frac {P_{\text{t}}G_{\text{t}}A_{\text{r}}\sigma FD}{16\pi ^{2}k_{\text{B}}TBN}}\right)^{\frac {1}{4}},} 880:
Allows the radar antenna to be pointed directly at the ground without overwhelming the computer and without reducing sensitivity.
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B developed during the 1950s specifically for the purpose of operating in hurricane conditions with no performance degradation.
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indicates the difference between the two measurements is below a threshold, which can only occur with an object that satisfies
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is essential for pulse-Doppler radar operation. As the reflector moves between each transmit pulse, the returned signal has a
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is the most effective because it produces a flat processing floor with no ringing that would otherwise cause false alarms.
276:{\displaystyle {\text{Doppler frequency}}={\frac {2\times {\text{transmit frequency}}\times {\text{radial velocity}}}{C}}.} 152: 432:{\displaystyle I=I_{0}\sin \left({\frac {4\pi (x_{0}+v\Delta t)}{\lambda }}\right)=I_{0}\sin(\Theta _{0}+\Delta \Theta ),} 2509: 2156: 973:
Maximum range from reflectivity (red) and unambiguous Doppler velocity range (blue) with a fixed pulse repetition rate.
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In airborne pulse-Doppler radar, the velocity threshold is offset by the speed of the aircraft relative to the ground.
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Scan mode involves frequency filtering, amplitude thresholding, and ambiguity resolution. Once a reflection has been
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Ambiguity processing is required when target range is above the red line in the graphic, which increases scan time.
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Special consideration is required for aircraft with large moving parts because pulse-Doppler radar operates like a
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Subclutter visibility is the ratio of the smallest signal that can be detected in the presence of a larger signal.
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and moving target indicator radar, which can mask aircraft reflections. This phenomenon was adapted for use with
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of the returned signal to determine the target object's velocity. It combines the features of pulse radars and
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integrates all of the energy from all of the individual reflected pulses that enter the filter. This means a
1948: 1267: 2708: 2698: 2178: 934: 156: 1231:(PRF) from about 3 kHz to 30 kHz. The range between transmit pulses is 5 km to 50 km. 1513: 296:, from pulse to pulse. This causes the reflector to produce Doppler modulation on the reflected signal. 2316:
Proceedings of the 5th International ICST Conference on Pervasive Computing Technologies for Healthcare
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Pulse-Doppler radar has special requirements that must be satisfied to achieve acceptable performance.
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on the transmit pulse that can produce signal cancellation. Doppler has maximum detrimental effect on
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Liang, Liu; Popescu, Mihail; Skubic, Marjorie; Rantz, Marilyn; Yardibi, Tarik; Cuddihy, Paul (2011).
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capability to support air-to-air missile systems in most modern military aircraft by the mid 1970s.
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to automatically adjust Doppler rejection speed within the volume of space surrounding the track.
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Pulse-Doppler radar is generally limited to mechanically aimed antennas and active phased arrays.
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The antenna type and scan performance is a practical consideration for multi-mode radar systems.
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reduces sub-clutter visibility performance by producing apparent motion on stationary objects.
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Pulse-Doppler radar was developed during World War II to overcome limitations by increasing
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from the velocity of any precipitation in the air. Pulse-Doppler radar is also the basis of
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Pulse-Doppler radar must be multi-mode to handle aircraft turning and crossing trajectory.
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and accounting for in-band noise distribution across multiple detection filters. The value
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produce a tone. The actual size of the target can be calculated using the audible signal.
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These improvements are the reason pulse-Doppler is essential for military and astronomy.
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system that determines the range to a target using pulse-timing techniques, and uses the
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places Doppler modulation onto stationary clutter. That receive modulation corrupts the
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pose a problem with search, detection, and ambiguity resolution in pulse-Doppler radar.
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Lock eliminates the need for human intervention with the exception of helicopters and
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The received signals from multiple PRF are compared to determine true range using the
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systems, which must use reverse phase shift for Doppler compensation in the detector.
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is the angle offset between the antenna position and the aircraft flight trajectory.
2341: 2133:), which is used for target classification in addition to the kinds of conventional 2390:"Path to Nexrad, Doppler Radar Development at the National Severe Storm Laboratory" 2319: 2098: 1301: 1277: 1255: 927: 920: 59: 2523: 2040:, where Doppler velocity is compared with the range movement on successive scans. 1966: 302:
The amplitude of the successively returning pulse from the same scanned volume is
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Audible Doppler and target size support passive vehicle type classification when
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during the detection interval, and the receiver must have large instantaneous
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Pulse-Doppler provides an advantage when attempting to detect missiles and
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or lower to extend the horizon, which is very different from diffraction.
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interceptor aircraft for the United States Air Force, and later for the
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Multi-mode operation may also include continuous wave illumination for
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with a pattern of discrete ranges, each of which has a blind velocity.
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The following gives the maximum permissible settling time for antenna
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Pulse-Doppler radars exploit this phenomenon to improve performance.
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X-Fighters: USAF Experimental and Prototype Fighters, XP-59 to YF-23
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Doppler weather effects (precipitation) were also found to degrade
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is added to the standard radar range equation to account for both
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was a prototype airborne radar/combination system for the planned
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in the 1950s after declassification of some World War II systems.
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Advanced Radar Techniques and Systems edited by Gaspare Galati (
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that traps RF signals in a thin layer of air like a wave-guide.
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in radar intended to detect and report aircraft and spacecraft.
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The target Doppler signal from the detection is converted from
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The two angle error techniques used with tracking radar are
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presentation, which highlights the advantages of using the
2205:(non-pulsed, swept frequency, range and Doppler processing) 1615: 1339:
Second, the shape of the receive pulse is adjusted using a
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Increases detection range by 300% or more in comparison to
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Pulse-Doppler radar for aircraft detection has two modes.
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Doppler is incompatible with most electronically steered
2309: 54:, an American long range supersonic missile powered by 1570: 1551: 1474:= number of range samples between each transmit pulse, 1892:= effective aperture (area) of the receiving antenna, 1732: 1680: 1640: 1530: 1393: 1146: 1080: 844: 756: 688: 648: 585: 526: 499: 477: 448: 308: 233: 163:. The US's first pulse-Doppler radar, the system had 70:
Pulse-Doppler techniques also find widespread use in
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The first operational pulse-Doppler radar was in the
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Introduction to Principles and Applications of Radar
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for small object detection near terrain and weather.
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Change of wavelength caused by motion of the source
2492:"AN/SPS-49 Very Long-Range Air Surveillance Radar" 1843: 1704: 1664: 1624: 1443: 1198: 1122: 883:Fills in the vulnerability region associated with 850: 830: 740: 657: 634: 565: 508: 483: 461: 431: 275: 2648:. St. Paul, Minnesota: Motorbooks International. 1723:The theoretical range performance is as follows. 1500:Refraction and ducting use transmit frequency at 1062:The received signals are also compared using the 167:capability and could track one target at a time. 2665: 1539: 861:Surface reflections appear in almost all radar. 144:Early examples of military systems includes the 2055:needs to be satisfied during normal operation. 1918:= Doppler filter size (transmit pulses in each 930:flying near terrain, sea surface, and weather. 2584: 2446:"Subclutter Visibility and Improvement Factor" 2423:. Weather Beacon Doppler Radar. Archived from 1048:Pulse-Doppler signal processing also includes 876:Pulse-Doppler radar corrects this as follows. 2211:- the reason for ambiguous velocity estimates 1216: 1480:= maximal design pulse repetition frequency. 665:is the phase shift induced by range motion. 2643: 2060:Pulse-Doppler signal processing § Lock 1902:, or scattering coefficient, of the target, 2704:Science and technology during World War II 1965:This equation is derived by combining the 894:(MTI) by improving sub-clutter visibility. 869:Clutter creates a vulnerability region in 2187:(non-pulsed; used for navigation systems) 2121:is moving slow near terrain and weather. 2009: 1108:number of samples between transmit pulses 2324:10.4108/icst.pervasivehealth.2011.245993 1566:transmit noise, where bandwidth is  1519: 1208: 968: 214: 194: 181: 18: 2246:Modern Radar Systems by Hamish Meikle ( 210: 129:. This required the development of the 2666: 2592:"High Power L Band Fast Phase Shifter" 2094:with the exception of decoy aircraft. 1238: 1135: 2559: 2542:Massachusetts Institute of Technology 2199:(non-pulsed, pure Doppler processing) 1949:receiver bandwidth (band-pass filter) 1052:to identify true range and velocity. 1025: 223:Pulse-Doppler radar is based on the 190: 153:Hughes AN/ASG-18 Fire Control System 23:Airborne pulse-Doppler radar antenna 1069: 13: 2621:. Norhrop Grummond. Archived from 2438: 2181:(fundamentals of the radar signal) 1910:antenna pattern propagation factor 901:of about 60 dB is needed for 845: 809: 652: 649: 620: 609: 606: 548: 530: 527: 500: 420: 417: 405: 363: 74:, allowing the radar to determine 14: 2720: 2496:Federation of American Scientists 2293:"AN/APQ-174/186 Multi-Mode Radar" 2221: 1229:medium pulse repetition frequency 885:pulse-amplitude time-domain radar 871:pulse-amplitude time-domain radar 2193:(pulsed with Doppler processing) 1328:Ringing is reduced in two ways. 579:to segregate different signals: 469:is the distance radar to target, 186:Principle of pulse-Doppler radar 2636: 2608: 2530: 2516: 2502: 2484: 2088:Pulse-Doppler signal processing 1997:pulse-Doppler signal processing 1993:Pulse-Doppler signal processing 1979:pulse-Doppler signal processing 1266:Pulse-Doppler radar requires a 1032:Pulse-Doppler signal processing 516:is the time between two pulses. 2510:"Dwell Time and Hits Per Scan" 2464: 2421:"How does Doppler Radar Work?" 2413: 2382: 2357: 2348: 2303: 2285: 2276: 2108: 1983:transmitter FM noise reduction 1714: 1487: 1458:= phase shifter settling time, 1187:filter size in transmit pulses 1111: 1103: 1064:frequency ambiguity resolution 658:{\displaystyle \Delta \Theta } 423: 401: 369: 344: 1: 2269: 2146: 1295: 1227:Pulse-Doppler typically uses 964: 959:Aircraft with no moving parts 2243:course at University of Iowa 2179:Radar signal characteristics 1883:of the transmitting antenna, 1464:= sub-clutter visibility in 1317: 1261: 1022:for sub-clutter visibility. 949:sounds like a helicopter, a 935:identification friend or foe 899:Clutter rejection capability 177: 157:North American XF-108 Rapier 7: 2172: 1333:shape of the transmit pulse 1292:, and solid state devices. 1015:horizon with clear skies). 668: 10: 2725: 2616:"AWACS Surveillance Radar" 1354: 1299: 1223:Pulse repetition frequency 1220: 1217:Pulse repetition frequency 1057:range ambiguity resolution 1029: 943:pulse repetition frequency 928:low observability aircraft 127:pulse repetition frequency 97: 2232:autocorrelation technique 1861:= distance to the target, 199:Principle of pulsed radar 2567:"Dolph-Chebyshev Window" 2318:. IEEE PervasiveHealth. 2167:semi-active radar homing 2072:Weather phenomenon obey 2036:Track mode works like a 1655:CFAR detection threshold 1270:with very little noise. 1020:performance measurements 937:is not available from a 892:moving target indication 509:{\displaystyle \Delta t} 491:is the radar wavelength, 484:{\displaystyle \lambda } 80:synthetic aperture radar 2679:Radar signal processing 2538:"Side Lobe Suppression" 2524:"Side Lobe Suppression" 2354:Pace 1991, p. 152. 1941:= absolute temperature, 1282:crossed-field amplifier 957:sound like propellers. 953:sounds like a jet, and 913:moving target indicator 851:{\displaystyle \Theta } 109:moving target indicator 2694:Navigational equipment 2010:Aircraft tracking uses 1920:Fast Fourier transform 1845: 1706: 1666: 1626: 1609:receiver dynamic range 1510:over-the-horizon radar 1445: 1373:measure of performance 1349:Dolph-Chebyshev window 1345:fast Fourier transform 1200: 1124: 974: 917:flying below the radar 852: 832: 742: 659: 636: 567: 510: 485: 463: 433: 277: 220: 200: 187: 41:continuous-wave radars 24: 2684:Measuring instruments 2197:Continuous-wave radar 1846: 1707: 1695:subclutter visibility 1667: 1643:subclutter visibility 1627: 1520:Subclutter visibility 1446: 1209:Special consideration 1201: 1125: 972: 853: 833: 743: 660: 637: 568: 511: 486: 464: 462:{\displaystyle x_{0}} 434: 278: 218: 198: 185: 72:meteorological radars 22: 2689:Microwave technology 2644:Pace, Steve (1991). 2157:radar track function 1870:= transmitter power, 1730: 1678: 1638: 1528: 1391: 1144: 1078: 1050:ambiguity resolution 919:to avoid detection ( 903:look-down/shoot-down 842: 754: 686: 646: 583: 524: 497: 475: 446: 306: 231: 211:Velocity measurement 172:look-down/shoot-down 165:look-down/shoot-down 65:look-down/shoot-down 16:Type of radar system 2709:Targeting (warfare) 2699:Air traffic control 2571:Stanford University 2526:. Radartutorial.eu. 2237:Pulse-Doppler radar 2082:Newtonian mechanics 2046:Newtonian mechanics 1900:radar cross section 1385:phase shift modules 1290:traveling wave tube 1268:coherent oscillator 1239:Angular measurement 1149:velocity resolution 1136:Velocity resolution 994:air-to-air missiles 732:velocity threshold 135:traveling wave tube 92:air traffic control 29:pulse-Doppler radar 2452:on January 1, 2011 2215:Doppler sonography 2092:mechanical jamming 2067:electronic jamming 1933:Boltzmann constant 1841: 1702: 1662: 1622: 1614: 1579: 1560: 1441: 1196: 1179:transmit frequency 1120: 975: 955:propeller aircraft 939:transponder signal 848: 828: 822:velocity threshold 786:transmit frequency 738: 717:transmit frequency 678:is much lower for 655: 632: 563: 506: 481: 459: 429: 273: 253:transmit frequency 221: 201: 188: 116:conventional radar 25: 2333:978-1-936968-15-2 2115:phase-locked loop 2074:adiabatic process 2038:phase-locked loop 1835: 1821: 1808: 1774: 1764: 1754: 1697: 1696: 1693: 1684: 1657: 1656: 1653: 1644: 1610: 1601: 1593: 1578: 1577: 1574: 1567: 1559: 1558: 1555: 1534: 1436: 1433: 1418: 1414: 1323:Ringing artifacts 1191: 1188: 1180: 1167: 1150: 1115: 1109: 1098: 1084: 1026:Signal processing 909:Pulse compression 823: 798: 790: 787: 768: 767:Doppler frequency 733: 721: 718: 699: 698:Doppler frequency 627: 595: 558: 376: 268: 262: 254: 237: 236:Doppler frequency 191:Range measurement 2716: 2659: 2630: 2629: 2627: 2620: 2612: 2606: 2605: 2603: 2601: 2596: 2588: 2582: 2581: 2579: 2577: 2563: 2557: 2556: 2554: 2553: 2544:. 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Archived from 2442: 2436: 2435: 2433: 2432: 2417: 2411: 2410: 2408: 2407: 2401: 2394: 2386: 2380: 2379: 2377: 2376: 2361: 2355: 2352: 2346: 2345: 2307: 2301: 2300: 2289: 2283: 2280: 2132: 2130: 2099:frequency domain 2076:associated with 1850: 1848: 1847: 1842: 1837: 1836: 1828: 1826: 1822: 1820: 1810: 1809: 1806: 1800: 1799: 1786: 1776: 1775: 1772: 1766: 1765: 1762: 1756: 1755: 1752: 1745: 1711: 1709: 1708: 1703: 1698: 1694: 1691: 1690: 1685: 1682: 1671: 1669: 1668: 1663: 1658: 1654: 1651: 1650: 1645: 1642: 1631: 1629: 1628: 1623: 1618: 1617: 1611: 1608: 1604: 1603: 1602: 1599: 1594: 1591: 1580: 1575: 1572: 1571: 1568: 1565: 1561: 1556: 1553: 1552: 1535: 1532: 1514:troposphere duct 1479: 1473: 1463: 1457: 1450: 1448: 1447: 1442: 1437: 1435: 1434: 1431: 1420: 1419: 1412: 1411: 1401: 1302:Radar scalloping 1278:Cavity magnetron 1205: 1203: 1202: 1197: 1192: 1190: 1189: 1186: 1181: 1178: 1169: 1168: 1165: 1156: 1151: 1148: 1129: 1127: 1126: 1121: 1116: 1114: 1110: 1107: 1099: 1096: 1090: 1085: 1083:range resolution 1082: 1070:Range resolution 921:nap-of-the-earth 857: 855: 854: 849: 837: 835: 834: 829: 824: 821: 816: 812: 799: 796: 791: 789: 788: 785: 776: 769: 766: 763: 747: 745: 744: 739: 734: 731: 726: 722: 720: 719: 716: 707: 700: 697: 694: 664: 662: 661: 656: 641: 639: 638: 633: 628: 626: 612: 601: 596: 593: 572: 570: 569: 564: 559: 554: 537: 515: 513: 512: 507: 490: 488: 487: 482: 468: 466: 465: 460: 458: 457: 438: 436: 435: 430: 413: 412: 394: 393: 381: 377: 372: 356: 355: 336: 324: 323: 282: 280: 279: 274: 269: 264: 263: 260: 255: 252: 243: 238: 235: 90:and mapping. In 60:fighter aircraft 2724: 2723: 2719: 2718: 2717: 2715: 2714: 2713: 2664: 2663: 2662: 2656: 2639: 2634: 2633: 2625: 2618: 2614: 2613: 2609: 2599: 2597: 2594: 2590: 2589: 2585: 2575: 2573: 2565: 2564: 2560: 2551: 2549: 2536: 2535: 2531: 2522: 2521: 2517: 2508: 2507: 2503: 2490: 2489: 2485: 2476: 2474: 2470: 2469: 2465: 2455: 2453: 2444: 2443: 2439: 2430: 2428: 2419: 2418: 2414: 2405: 2403: 2399: 2392: 2388: 2387: 2383: 2374: 2372: 2363: 2362: 2358: 2353: 2349: 2334: 2308: 2304: 2291: 2290: 2286: 2281: 2277: 2272: 2224: 2175: 2149: 2128: 2126: 2111: 2012: 1930: 1891: 1878: 1869: 1827: 1805: 1801: 1795: 1791: 1787: 1771: 1767: 1761: 1757: 1751: 1747: 1746: 1744: 1740: 1739: 1731: 1728: 1727: 1717: 1689: 1681: 1679: 1676: 1675: 1649: 1641: 1639: 1636: 1635: 1613: 1612: 1607: 1605: 1598: 1590: 1589: 1585: 1582: 1581: 1569: 1564: 1562: 1550: 1543: 1542: 1531: 1529: 1526: 1525: 1522: 1490: 1477: 1471: 1461: 1455: 1430: 1410: 1406: 1405: 1400: 1392: 1389: 1388: 1357: 1341:window function 1320: 1304: 1298: 1264: 1241: 1225: 1219: 1211: 1185: 1177: 1170: 1164: 1157: 1155: 1147: 1145: 1142: 1141: 1138: 1106: 1095: 1094: 1089: 1081: 1079: 1076: 1075: 1072: 1034: 1028: 967: 843: 840: 839: 820: 795: 784: 777: 765: 764: 762: 761: 757: 755: 752: 751: 730: 715: 708: 696: 695: 693: 689: 687: 684: 683: 671: 647: 644: 643: 613: 602: 600: 592: 584: 581: 580: 577:spread spectrum 538: 536: 525: 522: 521: 498: 495: 494: 476: 473: 472: 453: 449: 447: 444: 443: 408: 404: 389: 385: 351: 347: 337: 335: 331: 319: 315: 307: 304: 303: 292:difference, or 286:Radial velocity 261:radial velocity 259: 251: 244: 242: 234: 232: 229: 228: 213: 193: 180: 100: 84:radar astronomy 17: 12: 11: 5: 2722: 2712: 2711: 2706: 2701: 2696: 2691: 2686: 2681: 2676: 2661: 2660: 2654: 2640: 2638: 2635: 2632: 2631: 2628:on 2009-02-27. 2607: 2583: 2558: 2529: 2515: 2501: 2483: 2463: 2437: 2412: 2381: 2356: 2347: 2332: 2302: 2284: 2274: 2273: 2271: 2268: 2267: 2266: 2255: 2244: 2239:handouts from 2234: 2223: 2222:External links 2220: 2219: 2218: 2212: 2206: 2200: 2194: 2188: 2182: 2174: 2171: 2148: 2145: 2125:human beings ( 2110: 2107: 2063: 2062: 2053:lock criterion 2023: 2022: 2019: 2011: 2008: 1971:noise equation 1967:radar equation 1963: 1962: 1952: 1942: 1936: 1928: 1923: 1913: 1903: 1893: 1889: 1884: 1876: 1871: 1867: 1862: 1852: 1851: 1840: 1834: 1831: 1825: 1819: 1816: 1813: 1804: 1798: 1794: 1790: 1785: 1782: 1779: 1770: 1760: 1750: 1743: 1738: 1735: 1716: 1713: 1701: 1688: 1661: 1648: 1621: 1616: 1606: 1597: 1588: 1584: 1583: 1563: 1549: 1548: 1546: 1541: 1538: 1521: 1518: 1489: 1486: 1482: 1481: 1475: 1469: 1459: 1440: 1429: 1426: 1423: 1417: 1409: 1404: 1399: 1396: 1356: 1353: 1319: 1316: 1312:detection gaps 1300:Main article: 1297: 1294: 1263: 1260: 1240: 1237: 1221:Main article: 1218: 1215: 1210: 1207: 1195: 1184: 1176: 1173: 1163: 1160: 1154: 1137: 1134: 1119: 1113: 1105: 1102: 1093: 1088: 1071: 1068: 1030:Main article: 1027: 1024: 966: 963: 896: 895: 888: 881: 863:Ground clutter 847: 827: 819: 815: 811: 808: 805: 802: 794: 783: 780: 775: 772: 760: 737: 729: 725: 714: 711: 706: 703: 692: 670: 667: 654: 651: 631: 625: 622: 619: 616: 611: 608: 605: 599: 591: 588: 562: 557: 553: 550: 547: 544: 541: 535: 532: 529: 518: 517: 505: 502: 492: 480: 470: 456: 452: 428: 425: 422: 419: 416: 411: 407: 403: 400: 397: 392: 388: 384: 380: 375: 371: 368: 365: 362: 359: 354: 350: 346: 343: 340: 334: 330: 327: 322: 318: 314: 311: 272: 267: 258: 250: 247: 241: 225:Doppler effect 212: 209: 205:speed of light 192: 189: 179: 176: 161:Lockheed YF-12 99: 96: 88:remote sensing 37:Doppler effect 15: 9: 6: 4: 3: 2: 2721: 2710: 2707: 2705: 2702: 2700: 2697: 2695: 2692: 2690: 2687: 2685: 2682: 2680: 2677: 2675: 2672: 2671: 2669: 2657: 2655:0-87938-540-5 2651: 2647: 2642: 2641: 2624: 2617: 2611: 2593: 2587: 2572: 2568: 2562: 2548:on 2012-03-31 2547: 2543: 2539: 2533: 2525: 2519: 2511: 2505: 2497: 2493: 2487: 2473: 2467: 2451: 2447: 2441: 2427:on 2012-03-31 2426: 2422: 2416: 2402:on 2012-03-21 2398: 2391: 2385: 2371:on 2012-03-31 2370: 2366: 2360: 2351: 2343: 2339: 2335: 2329: 2325: 2321: 2317: 2313: 2306: 2298: 2294: 2288: 2279: 2275: 2264: 2263:0-86341-172-X 2260: 2256: 2253: 2252:1-58053-294-2 2249: 2245: 2242: 2238: 2235: 2233: 2229: 2228:Doppler radar 2226: 2225: 2216: 2213: 2210: 2207: 2204: 2201: 2198: 2195: 2192: 2191:Weather radar 2189: 2186: 2185:Doppler radar 2183: 2180: 2177: 2176: 2170: 2168: 2163: 2160: 2158: 2152: 2144: 2141: 2138: 2136: 2135:radar display 2122: 2120: 2116: 2106: 2104: 2100: 2095: 2093: 2089: 2085: 2083: 2079: 2075: 2070: 2068: 2061: 2058: 2057: 2056: 2054: 2049: 2047: 2043: 2039: 2034: 2032: 2028: 2020: 2017: 2016: 2015: 2007: 2004: 2001: 1998: 1994: 1990: 1986: 1984: 1980: 1976: 1972: 1968: 1960: 1956: 1953: 1950: 1946: 1943: 1940: 1937: 1934: 1927: 1924: 1921: 1917: 1914: 1911: 1907: 1904: 1901: 1897: 1894: 1888: 1885: 1882: 1875: 1872: 1866: 1863: 1860: 1857: 1856: 1855: 1838: 1832: 1829: 1823: 1817: 1814: 1811: 1802: 1796: 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825: 817: 813: 806: 803: 800: 792: 781: 778: 773: 770: 758: 748: 735: 727: 723: 712: 709: 704: 701: 690: 681: 680:weather radar 675: 674:is not used. 666: 629: 623: 617: 614: 603: 597: 589: 586: 578: 573: 560: 555: 551: 545: 542: 539: 533: 503: 493: 478: 471: 454: 450: 442: 441: 440: 426: 414: 409: 398: 395: 390: 386: 382: 378: 373: 366: 360: 357: 352: 348: 341: 338: 332: 328: 325: 320: 316: 312: 309: 300: 297: 295: 291: 287: 283: 270: 265: 256: 248: 245: 239: 226: 217: 208: 206: 197: 184: 175: 173: 168: 166: 162: 158: 154: 149: 147: 142: 140: 136: 132: 128: 123: 121: 120:weather radar 117: 112: 110: 106: 95: 93: 89: 85: 81: 77: 73: 68: 66: 61: 57: 53: 52:CIM-10 Bomarc 48: 46: 42: 38: 34: 30: 21: 2645: 2637:Bibliography 2623:the original 2610: 2598:. Retrieved 2586: 2574:. Retrieved 2561: 2550:. Retrieved 2546:the original 2532: 2518: 2504: 2486: 2475:. Retrieved 2466: 2454:. Retrieved 2450:the original 2440: 2429:. Retrieved 2425:the original 2415: 2404:. Retrieved 2397:the original 2384: 2373:. Retrieved 2369:the original 2359: 2350: 2315: 2305: 2287: 2278: 2240: 2164: 2161: 2153: 2150: 2142: 2139: 2123: 2112: 2096: 2086: 2071: 2064: 2052: 2050: 2041: 2035: 2024: 2013: 2005: 2002: 1991: 1987: 1974: 1964: 1959:noise figure 1954: 1944: 1938: 1925: 1915: 1905: 1895: 1886: 1873: 1864: 1858: 1853: 1722: 1718: 1683:target power 1673: 1633: 1523: 1499: 1491: 1483: 1382: 1378: 1368:phased-array 1365: 1361: 1358: 1338: 1330: 1327: 1321: 1311: 1308: 1305: 1276: 1265: 1256:conical scan 1249: 1245: 1242: 1233: 1226: 1212: 1139: 1131: 1073: 1061: 1054: 1047: 1035: 1017: 1013: 1002: 998: 979: 976: 932: 925: 916: 907: 897: 875: 868: 862: 860: 797:ground speed 749: 676: 672: 594:target speed 574: 519: 301: 298: 293: 284: 222: 202: 169: 150: 143: 124: 113: 101: 69: 49: 28: 26: 2576:January 29, 2456:January 29, 2203:Fm-cw radar 2109:Helicopters 2103:time domain 1715:Performance 1600:filter size 1592:sample bits 1576:filter size 1557:noise power 1494:diffraction 1488:Diffraction 1331:First, the 1272:Phase noise 1039:phase noise 294:phase shift 105:phase-shift 45:electronics 2668:Categories 2552:2011-09-06 2477:2024-03-15 2431:2011-09-04 2406:2011-09-04 2375:2011-09-04 2270:References 2147:Multi-mode 2119:helicopter 2101:back into 1506:Refraction 1296:Scalloping 1005:dwell time 965:Detriments 947:helicopter 76:wind speed 2600:August 2, 1969:with the 1793:π 1778:σ 1428:× 1422:× 1318:Windowing 1262:Coherency 1252:monopulse 1183:× 1175:× 1162:× 1101:× 1066:process. 1059:process. 941:. Medium 846:Θ 810:Θ 807:⁡ 801:× 793:− 782:× 771:× 713:× 702:× 653:Θ 650:Δ 621:Δ 618:π 610:Θ 607:Δ 604:λ 556:λ 549:Δ 543:π 531:Θ 528:Δ 501:Δ 479:λ 421:Θ 418:Δ 406:Θ 399:⁡ 374:λ 364:Δ 342:π 329:⁡ 257:× 249:× 178:Principle 146:AN/SPG-51 2342:14786782 2297:Raytheon 2209:Aliasing 2173:See also 2131: Hz 2080:and not 2078:air mass 2031:resolved 2027:detected 1286:klystron 1247:future. 669:Benefits 139:coherent 131:klystron 82:used in 1355:Antenna 990:Kitchen 986:Harpoon 98:History 2652:  2340:  2330:  2261:  2250:  1854:where 1502:L-band 1451:where 1347:. The 992:, and 982:Exocet 838:where 642:where 439:where 133:, the 56:ramjet 2674:Radar 2626:(PDF) 2619:(PDF) 2595:(PDF) 2400:(PDF) 2393:(PDF) 2338:S2CID 2127:20–20 2021:Track 290:phase 33:radar 31:is a 2650:ISBN 2602:2011 2578:2011 2458:2011 2328:ISBN 2259:ISBN 2248:ISBN 2051:The 2042:Lock 2029:and 2018:Scan 1981:and 1881:gain 1687:> 1508:for 1280:and 1254:and 911:and 818:> 728:> 151:The 2320:doi 2129:000 1573:PRF 1540:min 1478:PRF 1462:SCV 1432:PRF 1413:SCV 1166:PRF 1097:PRF 1009:MTI 951:jet 804:cos 520:So 396:sin 326:sin 2670:: 2569:. 2540:. 2494:. 2336:. 2326:. 2314:. 2295:. 2169:. 2069:. 1985:. 1957:= 1947:= 1931:= 1922:), 1908:= 1898:= 1879:= 1789:16 1466:dB 1416:20 1387:. 1288:, 1258:. 1045:. 1011:. 988:, 984:, 682:. 86:, 47:. 27:A 2658:. 2604:. 2580:. 2555:. 2498:. 2480:. 2460:. 2434:. 2409:. 2378:. 2344:. 2322:: 2299:. 2265:) 2254:) 1975:D 1961:. 1955:N 1951:, 1945:B 1939:T 1935:, 1929:B 1926:k 1916:D 1912:, 1906:F 1896:σ 1890:r 1887:A 1877:t 1874:G 1868:t 1865:P 1859:R 1839:, 1833:4 1830:1 1824:) 1818:N 1815:B 1812:T 1807:B 1803:k 1797:2 1784:D 1781:F 1773:r 1769:A 1763:t 1759:G 1753:t 1749:P 1742:( 1737:= 1734:R 1700:. 1660:. 1647:= 1620:. 1596:+ 1587:2 1545:{ 1537:= 1472:S 1468:, 1456:T 1439:, 1425:S 1408:e 1403:1 1398:= 1395:T 1194:. 1172:2 1159:C 1153:= 1118:. 1112:) 1104:( 1092:C 1087:= 826:, 814:| 779:2 774:C 759:| 736:. 724:| 710:2 705:C 691:| 630:, 624:t 615:4 598:= 590:= 587:v 561:. 552:t 546:v 540:4 534:= 504:t 455:0 451:x 427:, 424:) 415:+ 410:0 402:( 391:0 387:I 383:= 379:) 370:) 367:t 361:v 358:+ 353:0 349:x 345:( 339:4 333:( 321:0 317:I 313:= 310:I 271:. 266:C 246:2 240:=

Index


radar
Doppler effect
continuous-wave radars
electronics
CIM-10 Bomarc
ramjet
fighter aircraft
look-down/shoot-down
meteorological radars
wind speed
synthetic aperture radar
radar astronomy
remote sensing
air traffic control
phase-shift
moving target indicator
conventional radar
weather radar
pulse repetition frequency
klystron
traveling wave tube
coherent
AN/SPG-51
Hughes AN/ASG-18 Fire Control System
North American XF-108 Rapier
Lockheed YF-12
look-down/shoot-down
look-down/shoot-down

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