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FINAL REPORT - Stakeholders - Ofcom

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3.3.3 Technology Description<br />

3.3.3.1 Introduction<br />

Secondary Surveillance Radars consist of a ground interrogator and an airborne<br />

transceiver (which detects the interrogation and produces a reply that is synchronous with<br />

the interrogation). All SSR installations operate on 1030MHz for the ground-air<br />

interrogations and 1090MHz for the air-ground reply. The use of different frequencies for<br />

uplink and downlink ensures that any reflections or echoes to the interrogation signal will<br />

not interfere with the aircraft’s reply. This overcomes one of the main technical limitations<br />

of PSR, and explains why SSR has a much better performance than PSR. However, note<br />

that unlike primary radar, SSR is a dependent system (reliant on airborne equipage of<br />

transponders), and therefore cannot ‘see’ unequipped airborne traffic.<br />

The interrogation and control transmissions (on 1030MHz) must have tolerances within<br />

0.2MHz of the carrier frequency for Mode A/C and ± 0.1MHz for Mode S. The frequency<br />

tolerance for the reply transmission shall be ±3MHz for Mode A/C and ±1MHz for Mode S.<br />

SSR is used as a stand-alone system, or co-located and synchronised with primary radar<br />

(particularly in en-route areas, where all the UK’s primary en-route radars are co-located<br />

and frequency paired with SSR). It is used in en-route, TMA and on the airport surface<br />

(normally as part of a multilateration solution).<br />

3.3.3.2 Technical Description<br />

The ground interrogator transmits a signal, which is responded to by the aircraft’s<br />

transponder. The ground then measures the round trip delay of the received signal, and<br />

extracts data from the aircraft transponder reply. Azimuth is measured from the position of<br />

the rotating radar antennae.<br />

Figure 3-6 below shows a basic schematic for the operation of SSR.<br />

Figure 3-6: Secondary Surveillance Radar, showing the pulse data transfer<br />

The interrogations for Mode A/C can be seen in Fig 3-7 – P1 and P3 are the interrogation<br />

pulses, with P2 being the control pulse. The P2 pulse is used for sidelobe suppression –<br />

the P2 pulse is constant, and thus other pulses can be measured against it to ensure that<br />

the target will only reply when in the main P1/P3 beam. If the P2 pulse returns a higher<br />

signal level than the P1 or P3 pulse, the target is outside the main beam and will not<br />

reply.<br />

Page 63

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