06.02.2013 Views

FINAL REPORT - Stakeholders - Ofcom

FINAL REPORT - Stakeholders - Ofcom

FINAL REPORT - Stakeholders - Ofcom

SHOW MORE
SHOW LESS

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

3.2.2.4 Antenna Systems<br />

For most ATC applications, the antenna is required to produce a fan beam in the vertical<br />

cross section. This shape of beam ensures that optimum distribution of energy occurs<br />

with the upper limit of coverage set by the maximum altitude required and the lower limit<br />

set to minimise the energy transmitted into the ground. As the antenna rotates, it<br />

describes a coverage volume with the characteristics of a flat cylinder with the antenna at<br />

the centre. As already noted, the horizontal beamwidth is set to maximise angular<br />

resolution of targets. Typical beam widths are in the range 1 to 2 degrees which gives an<br />

indication of the directivity. Such beam widths equate to an antenna gain in the range 30<br />

to 35 dB<br />

This type of radar is only capable of defining target positions in two dimensions – range<br />

and bearing. Using modern phased arrays it is possible to “steer” the beam under<br />

computer control in two or three dimensions. Such techniques are very costly and have<br />

not been generally applied to ATC surveillance radars to date.<br />

Generally ATC radar antennas are horizontally polarised (i.e. with the electric field in the<br />

horizontal plane) which gives maximum response from aircraft targets. Circular<br />

polarisation is used as an option to improve the detection of targets in rain.<br />

3.2.2.5 Transmitters<br />

Radar transmitters are divided into two main types: driven and self-oscillating. This<br />

terminology refers to the nature of the output device. In a self-oscillating system, the<br />

output tube is simply switched on and off at intervals corresponding to the radar pulse<br />

width. The transmission frequency is determined by the tube itself. In a driven system the<br />

output device is a high power amplifier with the pulse pattern and transmission<br />

frequencies determined at low level by the drive circuits. Driven systems provide better<br />

control of the transmitted spectrum.<br />

The only self oscillating tube widely used in ATC radar is the magnetron. The magnetron<br />

is physically small and uses relatively lower voltages (typically 15 to 25kV). It is used<br />

where compact dimensions and low costs are at a premium. Typical applications include<br />

low cost airport radars and in aircraft where space is a problem. It is also widely used in<br />

marine radar applications. However, as a self oscillating device, it has poor spectral<br />

characteristics and stability.<br />

The klystron is widely used in ATC radars. It is used in high power applications and<br />

requires high voltages (typically 80 to 100kV). It therefore requires X ray shielding and<br />

numerous safety interlocks.<br />

The travelling wave tube can provide a wide bandwidth, which is necessary to transmit<br />

short pulses or permit frequency diversity operation. The cost of TWT’s is high, but this is<br />

usually offset by a long in-service life.<br />

Solid state devices operate with low voltages and have a long life expectancy. They are<br />

well suited to feeding conventional rotating antennas as well as planar array applications<br />

where they provide a distributed power source. They are also much better suited to pulse<br />

compression applications and generate pulses with good spectral characteristics. In<br />

applications where they are used to drive a conventional antenna, a power combining<br />

network must be provided.<br />

Page 38

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

Saved successfully!

Ooh no, something went wrong!