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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
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