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Radar System Engineering

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SEC,9.17] STABILIZATION OF THE BEAM 305<br />

devise means of compensating for the angular motions of such vehicles,<br />

and this mactice is known as stabilization.’ The techniaue falls into<br />

two broad divisions, depending on whether the beam of radiation is<br />

stabilized, or the data displayed on the indicator are stabilized or corrected<br />

for the distortions caused by a tilting vehicle.<br />

In general there is no choice between the two types of stabilization.<br />

If the vehicle rolls or pitches to such an extent that its search radar no<br />

longer scans the desired part of the field of view, beam stabilization is<br />

necessary. This will prevent targets from fading from the indicator; if<br />

they are then indicated, but at a false position, data stabilization becomes<br />

a concurrent need. If the vehicle momentarily changes heading (yaws)<br />

while on a certain course, the relative azimuth of targets will momentarily<br />

ah er; the consequent aberration of the display can be, and has been, corrected<br />

by either type of stabilization. Either sort of stabilization<br />

requires the vehicle to carry gyroscopes or other devices which are sensitive<br />

to direction in space and “know” the direction of north or up.<br />

There are several ways of more or less completely mechanizing the<br />

stabilization of the beam. The most obvious and perhaps the most<br />

elegant is to provide a stable base for the scanner. This may be a platform<br />

mounted on gimbals and controlled automatically to compensate<br />

the pitching and rolling of the vehicle. If the vehicle rolls much but<br />

pitches little, the pitch-gimbal axis may be omitted, and the stable-base<br />

stabilization degenerates into roll stabilization.<br />

A very different method of beam stabilization is possible in a scanner<br />

having its main axis always perpendicular to the floor of the vehicle.<br />

Use is made of the tilt axis of the antenna to the end that the antenna is<br />

automatically directed toward the horizon, or to whatever angle above or<br />

below the horizon is desired. The line of sight is thereby stabilized.<br />

9.17. Stabilization of the Beam. Airborne Antenna Stabilization. 2—<br />

Antenna stabilization for airborne radar is a scheme to preserve the same<br />

conditions of radiation illumination in ponlevel flight as in level flight.<br />

This is necessary to prevent (1) uneven illumination of the area being<br />

scanned, (2) loss of radar range, or (3) distortion of the PPI presentation.<br />

Stabilization equipment must be designed and constructed to stabilize<br />

the beam of radiation, whether it be pencil or fan, against any maneuver<br />

of the aircraft such as a climb, a glide, or any combination thereof. This<br />

must be accomplished with components that are not affected by the<br />

various accelerations, attitudes, or vibrations which might be encountered<br />

in turns, climbs, glides, or banks.<br />

A stabilizer may generally be broken down into three main components:<br />

the gyroscope lvith its potentiometer or synchro take-offs, the<br />

1‘~he theorv and Inethods of stabilization me discussedin Vol. 26 of this series<br />

2By F. B. Lincoln.

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