12.02.2014 Views

Radar System Engineering

Radar System Engineering

Radar System Engineering

SHOW MORE
SHOW LESS

Create successful ePaper yourself

Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.

SEC. 614] PRECISION TRACKING OF A SINGLE TARGET 207<br />

ing coverage of the tail cone without the necessity for scanning. The<br />

beam \vasconically scanned by rotating the reflector about an axis which<br />

made an angle of 2.5° ~rith its o~rn. Commutators were mounted on the<br />

shaft of the antenna rotation mechanism so that signals from the upper<br />

half of the scan collld be integrated and compared with those from the<br />

lower half; similarly, signals from the left half of the scan were compared<br />

with those from the right. The resulting error voltages were used to<br />

deflect the spot of a CRT used as an error indicator. An automatic circuit<br />

searched in range in the absence of a target, and locked on and<br />

tracked a target when an echo was encountered within the 2000-yd<br />

coverage of the set. This range circuit was used to brighten the spot<br />

only when a target was in range, in order to distinguish between correct<br />

pointing and the absence of a target. It also caused the target spot to<br />

grow horizontal “wings” whose spread increased as the range grew<br />

shorter, in order to provide an indication of range to the gunner (see<br />

Fig. 6.13).<br />

The axis of the conical scan was aligned with the guns so that only<br />

point-blank fire with no lead was possible. Thk was done because the<br />

lead required in countering the usual nightfighter approach is negligible. “<br />

The indicator was so arranged that its display was projected into the<br />

reflector sight, enabling the gunner to use the same technique for either<br />

optical or radar tracking. This equipment became available so late in<br />

the war that it had substantially no operational use, but its provingground<br />

tests indicated that its performance would have been quite satisfact<br />

ory. The attainable angular accuracy was about + 0.5°.<br />

The AN/APG-15 was unusual in that a triode, the “lighthouse”<br />

tube, was used as a pulsed oscillator. At the low pulse power used (about<br />

500 watts), this enabled transmitter, receiver, and the necessary rectifierfilter<br />

power supplies to be housed in one compact unit, shown in Fig. 6.36.<br />

Automatic Angle Tracking. -Shortcomings of the SCR-268 as a firecontrol<br />

position finder arose mainly from the use of a relatively long<br />

wavelength which resulted in broad beams from antennas of any reasonable<br />

size. When microwave radar became practicable with the development<br />

of the cavity magnetron, one of the immediate applications of the<br />

new technique was an antiaircraft position finder. The most widely used<br />

and generally successfld of the resulting equipments was the SCR-584.<br />

Before beginning precision tracking of a single target, a radar that is<br />

to serve as the only equipment of an antiaircraft battery must execute a<br />

general search in order to locate targets that are to be tracked and<br />

engaged. No auxiliarv long-wave radar search equipment was provided<br />

\vith the SC R-584. Instead, the 6-ft antenna reflector was helically<br />

scanned, and targets presented on a PPI whose maximum range was<br />

60,000 yd. A range of elevation angles up to 10° was covered by the

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!