Secondary Surveillance Radar SSR)

Secondary Surveillance Radar

Principle of Secondary Surveillance Radar (SSR)

  • SSR provides positive identification of aircraft in the line of sight on the UHF band frequencies with active co-operation of target
  • Secondary Surveillance Radar detects aircrafts at higher range using lower power on the principle of interrogation and response

SSR Ground Based Interrogator

  • Interrogator of SSR is a ground-based equipment transmitting on 1030 MHz in horizontal plane in a specified direction
  • SSR Interrogator has a flat directional antenna mounted on top of primary radar antenna to synchronise with primary radars
  • The Interrogation Message is contained between two framing pulses called P1 and P3
  • Interrogator can transmit in Mode A for a duration 8 micro seconds or Mode C with duration of 21 micro seconds
  • Interrogator receives the aircraft’s response on 1090 MHz in the horizontal plane

SSR Transponder in the Aircraft

  • SSR transponder replies to the ground interrogator using an omni-directional pulses on 1090 MHz after a delay of 50 micro seconds
  • The reply consists of a unique 4-digit code set on the aircraft transponder and connected to flight plan of every aircraft
  • The reply code is received on ground providing display of aircraft call-sign, track and height on radar scope

Side Lobe Suppression

  • Ground based Interrogator transmits unwanted side-lobes that has to be identified and not replied by aircraft
  • Interrogator transmits an additional framing pulse P2 in all directions from a separate ariel for side-lobe suppression
  • P2 pulse is transmitted 2 microseconds after the first framing pulse P1 with a strength lesser than P1 but exceeds the side lobe strength
  • If P2 is stronger than P1, it is considered as a side-lobe and the aircraft would not respond to this side-lobe interrogation

Reply of Aircraft Transponder

  • Aircraft transponder replies to the interrogation by a message enclosed between two framing pulses called F1 and F2 spaced 20.3 micro seconds apart
  • The information is contained in three pulses for each digit of SSR code making a total of 12 information pulses
  • Code relayed by information pulses by three digits for each number of the code
  • For example, 7 is relayed as 1+2+4, 3 is relayed as 1+1+1 and 6 is relayed as 2+2+2
  • The maximum value of code is 7777 which results in a combination of 4096 codes

Special Position Identification

  • When ATC requests Squawk Ident, Special Position Identification or Ident spring-loaded button is pressed
  • Ident button activates an Ident pulse transmission 4.35 micro seconds after F2 for 20 seconds
  • ATC can identify the aircraft by a ring around the return on the radar screen

SSR Mode A and C

  • Mode A transponders replies provide Identification, Bearing and Range with pulses train of 8 micro second spacing
  • Mode C interrogation pulses are at 20.5 micro second spacing for transmitting height referenced to 1013 HPa using an encoder altimeter
  • Mode C is activated through an ALT button providing an accuracy of 50 feet with an overall accuracy on the radar scope is 100 ft

Reserved Codes in SSR

  • Special Codes are reserved in SSR for Emergency, Communication Failure, Hijack and Code not Allotted st departure
  • 7700 indicates Emergency, 7600 indicates Communication Failure, 7500 indicates Hijack, 2000 indicates code not allotted and 7000 is the Default code

Advantages and Disadvantages of SSR

  • SSR requires lesser power and the range can extend to 200 NM, ensuring positive identification of aircraft
  • SSR is clutter free and not dependent on returning pulses due to aircraft aspect or echo area
  • In addition to raw position calculated Speed, Track and Altitude are displayed to the Radar Controller
  • SSR mode A or C provides for only 4096 Codes which is grossly insufficient due to increase in civil aviation

Garbling and Fruiting

  • Garbling is caused by overlapping replies from two aircrafts when aircraft transponders are within 1.7 NM apart
  • Fruiting is the result of interference at one interrogator (ground) by replies from transponder (aircraft) to another interrogator

Mode S SSR

  • Mode S overcomes disadvantages of normal SSR by selective addressing using 16,700,000 codes incorporated during manufacture
  • Data link in Mods S SSR helps in transmitting written message when supported by ground data network
  • Uplink and downlink over the horizon are possible facilitating ground to air and air to ground data exchange
  • Mode S SSR continuously transmit every second without interrogation reducing radio communication while under radar control
  • SSR Mode S also operates on 1030 and 1090 MHz frequencies providing height to an accuracy of 25 Ft
  • Mode S SSR interrogates on All Call, Broadcast, Selective and Inter Mode
  • All Call mode is used to interrogate all mode S transponders (aircraft)
  • Broadcast mode is used to transmit information to all transponders
  • Selective mode is used to get response only from selected transponders
  • Inter-mode is used to interact with mode A and C transponders
  • If Mode A or C ground station interrogates mode S transponder, the aircraft will reply in Mode A or C using 4096 codes

Benefits of Mode S SSR

  • SSR Mode S enables Unique Aircraft Identification by Unique Address incorporated during manufacture
  • Selective Calling facility in addition to All-call facility provides Integrity of Identification with reduced Garbling and Fruiting in SSR Mode S
  • Mode S provides Simplified Aircraft Identification and improved Air Picture and Tracking in Horizontal and Vertical direction
  • More aircrafts can be accommodated by large number of addresses improving Short Term Conflict Alert
  • Mode S reduces Radio Transmission and provides an altitude Accuracy of 25 Ft with a display accuracy of 100 Ft

Best of luck