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There are many electro-optical (EO) electronic warfare (EW) systems
which are analogous to radio frequency (RF) EW systems. These EO EW systems operate in the optical portion of the
electromagnetic spectrum. Electro-optics (EO), as the name implies, is a combination of electronics and optics. By
one definition EO is the science and technology of the generation, modulation, detection and measurement, or
display of optical radiation by electrical means. Most infrared (IR) sensors, for example, are EO systems. In the
popularly used term "EO/IR," the EO is typically used to mean visible or laser systems. The use of EO in this
context is a misnomer. Actually, almost all "EO/IR" systems are EO systems as defined above. Another often used
misnomer is referring to an EO spectrum. EO systems operate in the optical spectrum, which is from 0.01 to 1000
micrometers. EO includes lasers, photometry, infrared, and other types of visible, and UV imaging systems.
The optical spectrum is that portion of the electromagnetic spectrum from the extreme ultraviolet (UV) through
the visible to the extreme IR (between 0.01 and 1000 micrometers (μm)). Figure 1 shows the optical spectrum in
detail. Figure 2 shows the entire spectrum. The end points of the optical spectrum are somewhat arbitrary. On the
long wavelength end of the spectrum IR radiation and microwaves overlap. Similarly, x-rays and the extreme UV
overlap on the short wavelength end of the spectrum. How the division is made depends on one's point of reference.
For example, radiation having a wavelength of 1000 μm which is emitted from a very hot body and is detected by an
energy measuring device such as a super-cooled bolometer is called IR radiation. However, radiation of the same
wavelength (or 300 gigahertz) which is generated by an electric discharge and is detected by a bolometer in a
waveguide is called microwave radiation. Older texts may refer to the terms near, middle, far, and far-far IR, the
frequency limits of which differ from the newer divisions shown below. Notice that the preferred terminology no
longer uses the term "middle IR".
1. Optical Spectrum
Figure 2. Electromagnetic Radiation Spectrum
The common terms used to describe optical radiation are the source
parameters of power, radiant emittance (older term) or radiant existence (newer term), radiance, and radiant
intensity. They refer to how much radiation is given off by a body. The parameter measured by the detector (or
collecting object/surface) is the irradiance. Any of these quantities can be expressed per unit wavelength in
which case the subscript is changed from e (meaning energy derived units) to λ and the term is then called
"Spectral ...X...", i.e. Ie
is radiant intensity, while Iλ
is spectral radiant intensity. These quantities in terms of currently
preferred “Système International d’Unités” (SI units) are defined in Table 1.
Table 1. Radiometric SI Units.
In common usage, irradiance is expressed in units of watts per square centimeter and wavelengths are in μm
instead of nanometers (nm). These previously accepted units and the formerly used symbols are known as the Working
Group on Infrared Background (WGIRB) units, and are shown in Table 2. The radiant intensity is in watts per
steradian in both systems.
Table 2. Older WGIRB Radiometric Units.
Other radiometric definitions are shown in Table 3.
Table 3. Other Radiometric Definitions
Where (*) represents the appropriate quantity Q, Ψ, M, E, or L
Note (1) Radiant absorptance
should not be confused with absorption coefficient.
The processes of absorption, reflection (including
scattering), and transmission account for all incident radiation in any particular situation, and the total must
add up to one: a + ρ + τ
= 1, as shown in Figure 3.
A few words may be needed about the unit of solid angle, the steradian. Occasionally this unit is confusing when
it is first encountered. This confusion may be partly due to difficulty in visualization and partly due to
steradian being apparently a dimensionless unit (which is in itself a contradiction). Three solid angles are easy
to visualize - these are the sphere, the hemisphere, and the corner of a cube (see Figure 4). There are 4π
steradians surrounding the center of a sphere, 2π
steradians in a hemisphere, and ½
steradians in the corner of a cube (that is, the solid angle subtended by two walls and the floor of a
room is ½ π
problem of dimensions enters in calculating the steradiancy of a given area on a spherical surface. The number of
steradians intercepted by an area A on the surface of a sphere of radius R is A/R2
. If length is
measured in centimeters, the dimensions of the solid angle is cm2
. So, steradian appears
to be dimensionless. However, it is the unit, steradian, that is dimensionless (in terms of units of length), not
the solid angle itself. One steradian is the solid angle intercepted by an area of one square centimeter on a
spherical surface of one centimeter radius (or one square foot at one foot).
IR wavelengths are typically
expressed in μm, visible wavelengths in μm or nm, and UV wavelengths in nm or angstroms. Table 4 lists conversion
factors for converting from one unit of wavelength to another. The conversion is from column to row. For example,
to convert from μm to nm, multiply the value expressed in μm by 103. IR wavelengths are also sometimes expressed
in a frequency-like unit called wavenumbers or inverse centimeters. A wavenumber value can be found by dividing
10,000 by the wavelength expressed in μm. For example, 2.5 μm converts to a wavenumber of 4000 or 4000 inverse
Table 4. Wavelength Conversion Units
Whereas the radiometric quantities Ψe
, and Ee
have meaning throughout the entire electromagnetic spectrum, their
photometric counterparts Ψv
, Iv, Lv
, and Ev
are meaningful only in
the visible spectrum (0.38 μm thru 0.78 μm).
The standard candle has been redefined as the new candle or
candela (cd). One candela is the luminous intensity of 1/60th of 1 cm2 of the projected area of a blackbody
radiator operating at the temperature of the solidification of platinum (2045 ºK). The candela (by definition)
emits one lumen (lm) per steradian.
Table 5 displays the photometric quantities and units. These are used
in dealing with optical systems such as aircraft television camera systems, optical trackers, or video recording.
Table 5. Photometric SI Units.
Table 6 displays conversion factors for commonly used illuminance quantities.
Table 6. Illuminance Conversion Units
Figure 5 shows a generalized detection problem. On the left of the diagram are
the radiation sources - the sun, background, and the target of interest. In the middle is the intervening
atmosphere, which attenuates the radiation as it travels to the detection system shown on the right of the
Anything at temperatures above absolute zero radiates energy in the electromagnetic spectrum. This
radiation is a product of molecular motion, and the spectral distribution of the radiation is characterized by the
temperature of the body. The four basic laws of IR radiation are Kirchhoff's law, Planck's law, the
Stefan-Boltzmann law, and Lambert's cosine law. Kirchhoff found that a material that is a good absorber of
radiation is also a good radiator. Kirchhoff's law states that the ratio of radiated power and the absorption
coefficient: (1) is the same for all radiators at that temperature, (2) is dependent on wavelength and
temperature, and (3) is independent of the shape or material of the radiator. If a body absorbs all radiation
falling upon it, it is said to be "black." For a blackbody the radiated power is equal to the absorbed power, and
the emissivity (ratio of emitted power to absorbed power) equals one. One can also have a graybody - one which
emits with the spectral distribution of a blackbody but at a lower intensity level because it has an emissivity of
something less than one.
The radiation from a blackbody at a specific wavelength can be calculated from
Figure 6 shows the spectral radiant emittance of blackbody radiators at several temperatures as calculated
from this equation. [Wλ
is in W/cm3
so multiply by 10 to get W/cm2
Wein's displacement law takes the derivative of the Plank's law equation (above) to find the wavelength for
maximum spectral exitance (emittance) at any given temperature (or the temperature of maximum output at a given
T = 2897.8 μ°K
For example, given that T=568ºK, then λm
= 5.1μ as verified by examining Figure
Figure 6. Blackbody Spectral Radiant Emittance
According to the Stefan-Boltzmann law, the total radiant emittance of a blackbody is proportional to
the fourth power of the temperature:
This is Plank's radiation law integrated over all values of λ.
blackbody is a perfectly diffuse radiator. According to Lambert's law of cosines, the radiation emitted by a
perfectly diffuse radiator varies as the cosine of the angle between the line of sight and the normal to the
surface. As a consequence of Lambert's law, the radiance of a blackbody cavity is 1/π
times the radiant emittance (a conical blackbody cavity emits into a solid angle of π
steradians). The radiation from a flat plate is emitted into 2π
radiation pattern for these sources are shown in Figure 7. Notice that the conical cavity has the highest
radiation straight ahead, and nothing at 2 angles approaching 90º whereas the flat plate has a uniform radiation
pattern at all angles in front of the surface.
The interrelationship of the various quantities that describe source and received radiation in a
In actual practice the intervening atmosphere attenuates the radiation passing from the source to the
receiver. When atmospheric transmission is accounted for, the receiver equation becomes:
is the atmospheric transmittance.
The sources of radiation encountered outside the laboratory are
either targets or backgrounds. One person's target may be another person's background. The target is the radiation
source of interest - for example, an aircraft, a missile, a structure on the ground, or a ship at sea. The
backgrounds are the non-target sources included within the field of view of the detection system which produce
what amounts to noise - background noise. Possible background sources include the sun, clouds, terrain, the sea,
blue sky, night sky, and stars. Figure 8 shows the spectral distribution of radiation from several targets and
background sources. Spectral and spatial means are generally used to discriminate the target from the background.
Spectral discrimination can be used because the targets are often characterized by spectral line or band emissions
which yield a high signal to background ratio within a selected wavelength band. Also the target is usually small
compared to the background so spatial discrimination can be used.
NOTE: These charts show relative not absolute radiant intensity of each signature.
"amplitude" of one cannot be compared with the "amplitude" of another.
Figure 8. Spectral Distribution of Various Targets
The radiation emitted or reflected from the targets and
backgrounds must pass through the intervening atmosphere before reaching the detection system. The radiation is
absorbed and re-emitted by molecular constituents of the atmosphere and scattered into and out of the path by
various aerosol components. In the IR, atmospheric attenuation follows an exponential relationship expressed by
the following equation: I = Io-kD
, where Io
is the radiation incident on the
attenuating medium, k is the extinction coefficient, and D is the path length.
The molecules that account
for most of the absorption in the IR region are water, carbon dioxide, nitrous oxide, ozone, carbon monoxide, and
methane. Figure 9 shows the transmission of radiation over a 1 NM level path. The curve shows absorptions due to:
1) both water and carbon dioxide at 1.4 μm, 1.85 μm, and 2.7 μm; 2) due to water only at 6 μm; and 3) due to
carbon dioxide only at 4.3 μm.
Inspection of Figure 9 reveals the presence of atmospheric windows, i.e.
regions of reduced atmospheric attenuation. IR detection systems are designed to operate in these windows.
Combinations of detectors and spectral bandpass filters are selected to define the operating region to conform to
a window to maximize performance and minimize background contributions. Figure 10 shows an expanded view of the
infrared portion of the spectrum.
The transmission in a window is greatly dependent on the length and
characteristics of the path. Figure 11 shows the transmission for a 15 NM path at 10,000-foot altitude with 100%
relative humidity. As is readily apparent, the transmission in the windows is greatly reduced over the longer path
compared to the transmission for the shorter path shown in Figure 9. Since water vapor generally decreases with
altitude, transmission generally increases and path length becomes the determining factor. However, path length
does not affect transmission of all wavelengths the same.
ATTENUATION OF EM WAVES BY THE ATMOSPHERE
Figure 9. Atmospheric Transmission Over 1 NM Sea Level Path
Figure 10. Transmittance of Atmosphere Over 1 NM Sea Level Path (Infrared Region)
A detector is a transducer which transforms electromagnetic radiation into a form which can be more easily
detected. In the detectors of interest to EW the electromagnetic radiation is converted into an electrical signal.
In some systems the signal is processed entirely within the system to perform its function. In others the signal
is converted to a form to allow the human eye to be used for the final detection and signal analysis.
The physical effects by which electromagnetic radiation is converted to
electrical energy are divided into two categories: photon effects and thermal effects. EW systems primarily use
detectors dependent on photon effects. These effects can be divided into internal photo effects and external photo
effects. The external photo effect is known as photoemission. In the photoemissive effect, photons impinging on a
photocathode drive electrons from its surface. These electrons may then be collected by an external electrode and
the photocurrent thus obtained is a measure of the intensity of the received radiation.
photoeffects of interest are the photoconductive effect and the photovoltaic effect. In the photoconductive
effect, absorbed photons cause an increase in the conductivity of a semiconductor. The change is detected as a
decrease in the resistance in an electrical circuit. In the photovoltaic effect, absorbed photons excite electrons
to produce a small potential difference across a p-n junction in the semiconductor. The photovoltage thus produced
may be amplified by suitable electronics and measured directly.
pyroelectric effect is a thermal effect that is applicable to EW systems. The pyroelectric effect is a change in
polarization in a crystal due to changes in temperature. Radiation falling on such a crystal is detected by
observing the change in polarization as a build up of surface charge due to local heating. When coated with a good
black absorber, the crystal will be sensitive to a wide band of wavelengths.
Figure 12 shows the spectral
sensitivity range of typical detectors using these effects. Detector Types
Photon detectors exhibit sharp long wavelength cutoffs. The principle photoemissive detector type in EW systems is
the photomultiplier. Current amplification is obtained in photomultipliers by secondary emission. A series of
electrodes known as dynodes lie between the cathode and the anode. The structure of side-on and end-on type
photomultipliers is shown in Figure 13.
The photoelectrons from the cathode are accelerated and focused
onto the first dynode. Secondary electrons from the first dynode are accelerated and focused onto the second
dynode, which emits more secondaries. This process is continued through from 4 to 16 stages in commercial tubes.
Current gains of 10 million can be obtained with 16 stages. Typical response times (electron transit time) are
tens of nanoseconds.
Figure 13. Multiplier Phototubes
Photoconductive detectors consist of a body of semiconductor - single or arrays- having electrodes attached to
opposite ends. In operation they are used in electronic circuits as resistors whose resistance depends on the
radiation upon the sensitive surface. Typical cooled and uncooled configurations are shown in Figure 14.
Figure 14. Photoconductive Detector
Photovoltaic detector configurations are shown in Figure 15. Photoconductive and photovoltaic detectors in EW
systems are usually operated cooled for greater sensitivity. N-type material contains a large number of excess
electrons and few “holes”, while P-type material contains few electrons and many holes.
Figure 15. Photovoltaic Detector Configurations
Diode phototubes and photomultipliers are commonly used detectors for UV systems. The typical IR system uses
arrays of photoconductive or photovoltaic detectors. Many state-of-the-art IR systems use what is known as focal
plane arrays. The advantage of focal plane detectors is the ability to integrate processing electronics elements
right on the same chip as the detector elements. Most visible band systems of interest are televisions. An example
of a typical television camera tube is the vidicon (Figure 16). The vidicon is a storage type camera tube in which
a charge-density pattern is formed by the imaged scene radiation on a photoconductive surface which is then
scanned by a beam of low velocity electrons. The fluctuating voltage coupled out to a video amplifier can be used
to reproduce the scene being imaged. Pyroelectric photocathodes can be used to produce a vidicon sensitive over a
broad portion of the IR.
Another type of camera tube is the image orthicon which uses a photoemissive sensitive element (Figure 17).
Small, light weight television cameras can now be made using charge-coupled device (CCD) or charge-injection
device (CID) technology. CCD cameras are the basis of the popular hand-held camcorders.
The most common detectors used in surface-to-air and air-to-air missile seekers use compounds which
Cadmium Sulfide - CdS Lead Selenide - PbSe
Gallium Arsenide - GaAs Lead Sulfide -
Indium Antimonide - InSb
Other known detector material includes:
Germanium doped with Copper
- Ge:Cu Germanium doped with Zinc - Ge:Zn
Germanium doped with Gold - Ge:Au Indium Arsenide - InAs
Germanium doped with Mercury -
Ge:Hg Lead Telluride - PbTe
Mercury Cadmium Telluride - HgCdTe
Some detectors (such as
InSb) have multiple modes of operation, including: Photoconductive (PC), Photovoltaic (PV), or
Photoelectromagnetic (PEM) modes of operation. Typical spectral detectivity characteristics for various detectors
are shown in Figure 18.
Detector Parameters and Figures of Merit
The important parameters in
evaluating a detector are the spectral response, time constant, the sensitivity, and the noise figure. The
spectral response determines the portion of the spectrum to which the detector is sensitive. The time constant is
a measure of the speed of response of the detector. It is also indicative of the ability of the detector to
respond to modulated radiation. When the modulation frequency is equal to one over the time constant, the response
has fallen to 70.7 % of the maximum value. The time constant is related to the lifetime of free carriers in
photoconductive and photovoltaic detectors and to the thermal coefficient of thermal detectors. The time constant
in photoemissive devices is proportional to the transit time of photoelectrons between the photocathode and anode.
Figure 18. Spectral Detectivity of Various Detectors
The sensitivity of a detector is related to its responsivity. The responsivity is the ratio of the
detected signal output to the radiant power input. For photoconductive and photovoltaic detectors the responsivity
is usually measured in volts per watt -- more correctly, RMS volts per RMS watt. However, the sensitivity of a
detector is limited by detector noise. Responsivity, by itself, is not a measure of sensitivity. Detector
sensitivity is indicated by various figures of merit, which are analogous to the minimum detectable signal in
radar. Such a quantity is the noise equivalent power (NEP). The NEP is a measure of the minimum power that can be
detected. It is the incident power in unit bandwidth which will produce a signal voltage equal to the noise
voltage. That is, it is the power required to produce a signal-to-noise ratio of one when detector noise is
referred to unit bandwidth. The units of NEP are usually given as watts, but, more correctly, are watts/Hz½
Another figure of merit is the noise equivalent input (NEI). The NEI is defined
as the radiant power per unit area of the detector required to produce a signal-to-noise ratio of one. The NEI is
obtained by dividing the NEP by the sensitive area of the detector. The units of NEI are watts per square
centimeter. An NEI for photoemissive devices is commonly given in lumens.
The NEP has the disadvantage that better detectors have smaller NEP's, but the human psyche is such that a
figure of merit that increases for improvements in detector performance is preferable. A figure of merit which has
that feature is the detectivity (D), which is defined as the reciprocal of the NEP. The units of D are watts-1
A higher value of detectivity indicates an improvement in detection capability. The dependence on detector area is
removed in another detectivity measure, known as D-star (D*). D* is the detectivity measured with a bandwidth of
one hertz and reduced to a responsive area of one square centimeter. The units of D* are cm·watts-1
D* is the detectivity usually given in detector specification sheets. The spectral detectivity is the parameter
used in Figure 18.
Besides the NEI mentioned above, the quantum efficiency of the photocathode is also a
figure of merit for photoemissive devices. Quantum efficiency is expressed as a percent -- the ratio of the number
of photoelectrons emitted per quantum of received energy expressed as a percent. A quantum efficiency of 100
percent means that one photoelectron is emitted for each incident photon.
There are other figures of merit
for television cameras. The picture resolution is usually described as the ability to distinguish parallel black
and white lines and is expressed as the number of line pairs per millimeter or TV lines per picture height. The
number of pixels in the scene also defines the quality of an image. A pixel, or picture element, is a spatial
resolution element and is the smallest distinguishable and resolvable area in an image. CCD cameras with 512 x 512
elements are common. Another resolution quantity is the gray scale, which is the number of brightness levels
between black and white a pixel can have.
Noise in Detectors
The performance of a detector is limited by noise. The
noise is the random currents and voltages which compete with or obscure the signal or information content of the
radiation. Five types of noise are most prominent in detectors: thermal, temperature, shot,
generation-recombination, and 1/f noise. Thermal noise, also known as Johnson noise or Nyquist noise, is
electrical noise due to random motions of charge carriers in a resistive material. Temperature noise arises from
radiative or conductive exchange between the detector and its surroundings, the noise being produced by
fluctuations in the temperature of the surroundings. Temperature noise is prominent in thermal detectors. Shot
noise occurs due to the discreetness of the electronic charge. In a photoemissive detector shot noise is due to
thermionic emission from the photocathode. Shot noise also occurs in photodiodes and is due to fluctuations in the
current through the junction. Generation-recombination noise is due to the random generation and recombination of
charge carriers (holes and electrons) in semiconductors. When the fluctuations are caused by the random arrival of
photons impinging upon the detector, it is called photon noise. When it is due to interactions with phonons
(quantized lattice vibrations), it is called generation-recombination noise. Johnson noise is predominant at high
frequencies, shot noise predominates at low frequencies, and generation-recombination and photon noise are
predominant at intermediate frequencies. As the name implies, 1/f noise has a power spectrum which is inversely
proportional to frequency. It is dominant at very low frequencies. In photoemissive detectors it is called flicker
noise and has been attributed to variation in the emission from patches of the photocathode surface due to
variation in the work function of the surface. In semiconductors 1/f noise is also called modulation noise. Here
it is apparently due to surface imperfections and ohmic contacts (which are a form of surface imperfection).
The word laser comes from Light Amplification by Stimulated Emission of Radiation. The lasing medium may be a
solid, a gas, or a liquid. Lasing action has been achieved using atoms, ions, and molecules. The emission may be
pulsed or CW.
Figure 19 shows the spectral output of several laser types.
The first laser was a
pulsed, solid state laser, the ruby laser. In the ruby laser a xenon flash lamp is used to excite the atoms in a
ruby rod to higher energy levels. The highly polished and mirrored ends of the rod form a resonant cavity. One end
of the rod has a slightly lower reflectivity. The lamp excitation produces an inverted population of excited atoms
which are stimulated to relax to lower energy levels releasing their extra energy as photons. Repeated reflections
off the mirrored ends of the rod causes the photons to bounce back and forth through the rod stimulating further
emissions at the same wavelength and phase producing a highly coherent beam which finally passes through the lower
Figure 19. Spectral Lines / Ranges of Available Lasers
Figure 20 is a schematic representation of a ruby laser. The typical laser rangefinder uses a solid state
laser with a neodymium-YAG crystal lasing at 1.06 μm.
Figure 21. Gas
Gas lasers are of several kinds and can be pulsed or CW. The gas dynamic laser obtains its inverted population
through a rapid temperature rise produced by accelerating the gas through a supersonic nozzle. In chemical lasers
the inversion is produced by a chemical reaction. In the electric discharge laser the lasing medium is
electrically pumped. The gas can also be optically pumped. In an optically pumped gas laser the lasing medium is
contained in a transparent cylinder. The cylinder is in a resonant cavity formed by two highly reflective mirrors.
The typical configuration is shown in Figure 21.
Figure 21. Gas
Many gas lasers use carbon dioxide as the lasing medium (actually a mixture of CO2 and other gases). These
are the basis for most high energy or high power lasers. The first gas laser was an optically pumped CW
helium-neon laser. The common laser pointer is a helium-neon laser operating at 0.6328 μm. The lasing medium is a
mixture of helium and neon gas in a gas discharge or plasma tube as shown in Figure 22.
22. Helium-Neon Laser
The dye laser is an example of a laser using a liquid for the lasing medium. The lasing medium is an organic dye
dissolved in a solvent such as ethyl alcohol. Dye lasers operate from the near UV to the near IR, are optically
pumped, and are tunable over a fairly wide wavelength range.
should also be made of semiconductor or injection lasers, also known as laser diodes. The junctions of most
semiconductor diodes will emit some radiation if the devices are forward biased. This radiation is the result of
energy released when electrons and holes recombine in the junction. There are two kinds of semiconductor diode
emitters: (1) the light emitting diode (LED), which produces incoherent spontaneous emission when forward biased
and which has a broad (800 angstrom) spectral output, and (2) the laser diode, which maintains a coherent emission
when pulsed beyond a threshold current and which has a narrow spectral width (< 10 angstrom). In the laser diode
the end faces of the junction region are polished to form mirror surfaces. They can operate CW at room
temperatures, but pulsed operation is more common. Figure 23 shows a typical diode laser structure.
Q-switching is a means of obtaining short intense pulses from lasers. The Q-switch inhibits lasing until a very
large inverted population builds up. The switch can be active or passive. A passive Q-switch switches at a
predetermined level. An active Q-switch is controlled by external timing circuits or mechanical motion. The switch
is placed between the rod (or lasing medium) and the 100 percent mirror. Figure 24 shows an arrangement using a
Pockels cell as an active Q-switch.
Figure 24. Q-switch Arrangement
Fiber optic cables are the optical analogue of RF waveguides.
Transmission of radiation through an optical fiber is due to total internal reflection of the radiation from the
walls of the fiber. A plain fiber has leakage through the walls. This is controlled by coating, or cladding, the
fiber with a lower refractive index material. Fibers with the best transmission characteristics (lowest
attenuation) operate in the near infrared (out to 1.7 μm). Typical attenuations vary from two to ten dB/km in the
visible to 0.2 to 0.5 dB/km in the near infrared. Developmental fibers for use in the 2 to 20 μm wavelength range
have attenuations of hundreds of dBs/km.
Optical fibers are not used in any current EO systems. Potential applications include use with smart skins
where radiation is collected on the skin and piped by fiber optics to detectors elsewhere in the aircraft. Use of
fiber optics in a high speed data bus for EW systems will probably come first.ELECTRO-OPTICAL
A basic EO system is composed of an optical head, an electronics package, and an output unit. The optical head
consists of a window, collecting optics which gathers the incident radiation and focusses it on the detector, a
field stop to define the field of view, a reticle or chopper to modulate and encode the radiation, optical filters
to define the wavelength region of response, a detector to convert the incident radiation into an electrical
signal, and a preamplifier to increase the signal level from the detector before further handling or processing.
The system electronics consist of amplifiers, signal processors, and system controls. The output unit consists of
indicators or displays.
For most applications of EO systems in EW the detection system
is protected from the environment by a window or dome of optically transmissive material. The window operates both
as a weather seal and, in some cases, helps to define the spectral response region of the system. The transmission
bands of a representative sample of window materials is shown in Figure 25. The end points given are for the 10
percent transmission wavelengths. Not shown in Figure 25 are the various UV transmissive glasses such as Pyrex,
Corex, and Vycor.
Figure 25. Transmission of Selected Window Materials
Most optical radiation detectors have a wider
sensitivity band than desired for the particular application. To further define the system sensitivity, band
interference filters or absorption filters are used. An absorption filter is a bulk material with a sharp cut-on
or cut-off in its transmission characteristic. A cut-on and a cut-off filter can be combined to make a bandpass
filter. By selecting absorption characteristics of absorption filters combined with the response of a detector,
the desired system response can be obtained. An interference filter is composed of dielectric coatings on an
appropriate substrate combined in such a way to produced cut-on, cut-off, or bandpass filters. Interference
filters allow more control of the final response characteristics and smaller elements.
Besides bandpass filters, EO system optics often have antireflection (or AR) coatings to eliminate or greatly
reduce unwanted reflections between optical elements.Detector Coolers
Many IR detectors have to be cooled for proper operation. Most systems use closed-cycle coolers or
thermoelectric coolers. Thermoelectric coolers use the Peltier effect, which produces a reduced temperature by
passing a d-c current through a thermoelectric junction. Multi-stage coolers can cool a detector down to below
200ºK. Closed-cycle coolers typically are of the Stirling cycle design and utilize the expansion of a gas (helium)
to cool a cold finger attached to the detector. These generally operate at liquid nitrogen temperature (77ºK).
Imaging systems such Forward Looking Infrared (FLIR) systems use cathode ray tubes (CRTs) to display their
output. Future EW systems may incorporate flat panel displays of some type. Possible types are liquid crystal
displays (LCDs), LED arrays, or gas plasma displays.
EO systems of interest to EW include the following:
FLIR systems - A passive
thermal imager which typically uses the emitted radiation of a target in the 8 to 14 μm atmospheric window to
produce a picture of the scene. Figure 26 shows the configuration of a typical FLIR using the serial scan
approach. A FLIR could be used with a 10.6 μm laser target designator to determine if the proper target is being
Infrared Search and Track Systems (IRSTS) - The IRSTS is an EO analogue of a radar system. A focal plane array
detector is scanned across the field of regard, and the locations of detected targets are displayed on a CRT.
Although without direct range measuring capability, triangulation techniques can be used for passive ranging. If
combined with a laser rangefinder, an IRSTS could function just like an optical radar. An IRST provides better
angular resolution but poorer range accuracy than a RF radar system.
Missile Warning Receivers/Sets - These
may have either scanning or staring optical systems to detect and process the radiation from missile motors and
alert the pilot that the aircraft is under attack.
Laser Warning Sets - These typically have staring
optics. They detect and process received laser radiation. The pilot is alerted of the type and the direction of
the laser detected.
Infrared Countermeasure (IRCM) Systems - The EO analogue of RF jammers. They radiate a
modulated IR signal designed to confuse the detection/tracking system of an attacking IR guided missile and cause
it to miss.
Television Camera Sets - High resolution TV camera systems primarily used for the
identification friend or foe application.
Laser Rangefinders - A laser coupled with timing circuits to
measure time of travel of laser pulses to and from a target. They can give very accurate ranges.
Target Designators - Laser systems used to illuminate targets being attacked by laser guided
Table of Contents
for Electronics Warfare and Radar Engineering Handbook
Abbreviations | Decibel | Duty
Cycle | Doppler Shift | Radar Horizon / Line
of Sight | Propagation Time / Resolution | Modulation
| Transforms / Wavelets | Antenna Introduction
/ Basics | Polarization | Radiation Patterns |
Frequency / Phase Effects of Antennas |
Antenna Near Field | Radiation Hazards |
Power Density | One-Way Radar Equation / RF Propagation
| Two-Way Radar Equation (Monostatic) |
Alternate Two-Way Radar Equation |
Two-Way Radar Equation (Bistatic) |
Jamming to Signal (J/S) Ratio - Constant Power [Saturated] Jamming
| Support Jamming | Radar Cross Section (RCS) |
Emission Control (EMCON) | RF Atmospheric
Absorption / Ducting | Receiver Sensitivity / Noise |
Receiver Types and Characteristics |
General Radar Display Types |
IFF - Identification - Friend or Foe | Receiver
Tests | Signal Sorting Methods and Direction Finding |
Voltage Standing Wave Ratio (VSWR) / Reflection Coefficient / Return
Loss / Mismatch Loss | Microwave Coaxial Connectors |
Power Dividers/Combiner and Directional Couplers |
Attenuators / Filters / DC Blocks |
Terminations / Dummy Loads | Circulators
and Diplexers | Mixers and Frequency Discriminators |
Detectors | Microwave Measurements |
Microwave Waveguides and Coaxial Cable |
Electro-Optics | Laser Safety |
Mach Number and Airspeed vs. Altitude Mach Number |
EMP/ Aircraft Dimensions | Data Busses | RS-232 Interface
| RS-422 Balanced Voltage Interface | RS-485 Interface |
IEEE-488 Interface Bus (HP-IB/GP-IB) | MIL-STD-1553 &
1773 Data Bus |
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