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Fighter Combat - Tactics and Maneuvering

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FIGHTER WEAPONS<br />

The various forms of horning guidance generally offer improved capability<br />

against airborne targets, especially highly maneuverable targets. More<br />

efficient trajectories <strong>and</strong> better guidance accuracy in the critical terminal<br />

phase of the intercept are often available. Each guidance method, however,<br />

has some advantage over the others in certain situations, so combination<br />

systems are sometimes employed. An example is the use of preset or<br />

comm<strong>and</strong> guidance during the early portion of a long-range shot to get the<br />

missile close enough to the target to allow passive or active homing.<br />

Advances in solid-state electronics technology have made it practical to<br />

place more sophisticated guidance <strong>and</strong> sensor capability in small, lightweight<br />

missile packages.<br />

Missile Seekers<br />

The seeker system of a missile is responsible for sensing <strong>and</strong> tracking the<br />

target <strong>and</strong> providing the information necessary for performance of the<br />

guidance system. Preset <strong>and</strong> comm<strong>and</strong> guidance do not require a seeker in<br />

the missile, since the tracking function is accomplished by the launching/guidance<br />

platform. Beam-rider missiles usually have a receiver in the<br />

tail to collect information from the host guidance/tracking beam. Passive<br />

missiles generally require a sensor receiver in the nose, as do semi-active<br />

homers; but semi-active homers may also include a rear receiver for<br />

interception of information directly from the illuminating platform which<br />

can be compared to the reflected energy received by the forward sensor to<br />

derive additional guidance data. Active homers require both a transmitter<br />

<strong>and</strong> a receiver, generally located forward.<br />

The maximum range of its seeker operation often limits the effective<br />

range of a missile system. Passive seekers have an inherent advantage here,<br />

because their received power is inversely proportional to the square of the<br />

target range, while the max-range of active <strong>and</strong> semi-active systems varies<br />

inversely with the fourth power. Several other factors also are involved.<br />

For passive systems these include the intensity of the target radiation in<br />

the direction of the sensor, the type of radiation (which determines the rate<br />

of signal attenuation by the atmosphere), <strong>and</strong> the seeker sensitivity. For<br />

active <strong>and</strong> semi-active systems maximum range depends on, in addition to<br />

transmitted power <strong>and</strong> receiver sensitivity, the reflective characteristics of<br />

the target relative to the type of illumination used. These reflective characteristics<br />

are usually sensitive to target size, <strong>and</strong> also to the target's construction<br />

material, shape, surface contours, <strong>and</strong> aspect, all of which may<br />

combine to increase or decrease reflectivity.<br />

The most common passive seeker now in use is the heat seeker. This<br />

device contains a material (the detector) which is sensitive to heat (infrared—IR—radiation)<br />

that is produced primarily by the target's propulsion<br />

system. The detector is often cryogenically cooled to eliminate<br />

internally generated thermal "noise" <strong>and</strong> allow detection of even very<br />

small amounts of IR energy coming from an external source. The seeker<br />

must still have the capability to discriminate between target radiation <strong>and</strong><br />

background radiation, however. Such differentiation is essential for all<br />

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