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By

                                                     Sharad Saurabh
                                      3rd year, Dept. of Instrumentation & Control
                                                      SRM University




                                       &


              Sayan Chakrabarty
3rd year, Dept. of Instrumentation & Control
               SRM University

                                                                                     1
   Ad-hoc literally means Something ‘created or done for a
    specific purpose only’.
   Ad-hoc network is a dynamic network which can be
    created anywhere with just two basic nodes and does
    not require any centralized infrastructure.
   Each node has a certain range of communication in
    which it can transmit or receive data.
   If it needs to communicate to a node which is outside
    its range, it may do so by sending the data to a node
    which is within its range. That node will transmit to
    the next and so on till it reaches its designated
    destination.
   Data is transmitted in the form of small packets.
                                                              2
Devices such as laptops, PDAs, mobile phones, MP3 players etc,
can be made to interact using Ad-hoc networking




In fact this is being used in technologies such as Bluetooth and Wi-Fi
to connect various devices. Now-a-days, most of the above
mentioned devices come with in built facilities to support ad hoc
networking.
                                                                    3
Contemporary communication means in aircrafts include :
 Radio Communication from ground (TIS-B)
 RADAR (Radio Detection and Ranging):

                Air Traffic Control (ATC) Radars
                Secondary Surveillance Radar (SSR) (Airport Surveillance Radar)
                Ground Control Approach (GCA) Radars
                PAR Systems
           Distance Measuring Equipment (DME)
           Radio Beacons
           Identification Friend or Foe (IFF) Systems
                IFF Interrogator
                IFF Transponder
           •Altimeter (AL) Radar Systems
           •Terrain-Following Radar (TFR) Systems
                                                                                   4
5
Automatic Dependent Surveillance-Broadcast (ADS-B)


 Data is broadcast in the form of discrete packets.

 Since the mid-1990s, FAA has focused on two different ADS-B
frequencies-
        1. 978 MHz Universal Access Transceiver – used by the General
Aviation (GA).
        2. 1090 MHz Extended Squitter (ES) – used by airliners and
other large aircraft.

 The 1090ES is selected for its international interoperability, whereas
the UAT link is for its weather graphics up-link capacity and low cost.


                                                                       6
7
•   Accuracy does not seriously degrade with range, atmospheric
    conditions, or target altitude.
•    Update intervals do not depend on the rotational speed or
    reliability of mechanical antennas.
•   Accuracy is unaffected by the range to the aircraft.
•    Also operable in lower altitudes and mountainous regions.
•   Relatively inexpensive technology, with costs for equivalent
    radar coverage running in the 0.1 to 0.05 range.
•   A single Mode S 1090ES ADS-B ground station can cost
    anywhere from $150,000 - $300,000 USD, including
    installation.

                                                                   8
Mode S 1090ES ADSB               Sample Mode S Multilateration and 1090ES ADS-B Ground
and Multilateration Ground       Station Installation for FAA ASDE-X Program.
Stations Deployed On Oil
Platforms In Gulf of Mexico For
Helicopter and En Route Tracking                                                   9
   Airbus has stated its intent to
    begin equipping all new
    transport class aircraft it
    produces with Mode S 1090ES as
    a standard feature.

   UPS, a US freight carrier, is in
    the process of installing Mode S
    1090ES ADS-B avionics on all
    107 Boeing 757s and 767s it
    operates.

   Australia, Japan, China and
    some parts of Europe & Africa
    have also opted for ADS-B and
    plan to implement it soon.         # Map showing European airports
                                       with ADS-B compatibility
                                                                    10
   Essentially a single-node operation scheme.

   Range is limited to the direct transmission range of the airborne Antenna.

   The 1090ES is likely to support ADS-B applications that do not require
    air-to-air ranges exceeding 80km when used in the highest density airspace
    and will provide ranges of 180 km in lower traffic density airspace. This is
    too short for longer range applications and flight-path-conflict resolutions.

   Research is on to implement an airborne ADS-B architecture that will
    readily accommodate a second ADS-B link in addition to the 1090ES.

   However, these additions can be too expensive and problematic, especially
    when in India, we are yet to realise the full potential benefits of even one
    digital link of the single-node system.
                                                                            11
Fig illustrates the main drawback of ADS-B
                                             12
13
   Multiple-hop means an ad hoc network where the data
    exchange is not limited to just a single pair but it includes a
    number of nodes.

   The nodes not only transmit their own data but also those
    received from neighbouring nodes.

   One aircraft can be made to broadcast not only its own state
    information periodically, but also the state information it
    receives about neighbouring aircrafts.

   Clusters can be disjoint from, or overlapped with each other.
                                                                  14
Fig. shows a cluster of planes forming a multiple hop network

                                                                15
   Possible to select more useful
    information over a larger area
    for cockpit display and
    onboard automation systems.

   Pilot can virtually see other
    aircrafts beyond its
    transmission range.

   Live data can be sent in a
    reliable and timely manner.

   Can provide a collision-free
    and extended traffic coverage.
                                     16
17
   The transmitted Protocol specifies
        The maximum number of hops the state information
    will be relayed
        How often the state information is broadcast
        What state information to broadcast
        The mix of own aircraft information vs. information
    of other aircraft, etc.
   The protocol should also specify a transmission rate
    such that it is ample to handle the data that it receives
    and transmits, i.e. the processing rate of the information
    should be synchronised with frequency with which data
    is received.


                                                                 18
Fig shows an example of five node network with link delivery probabilities.
                                                                              21
Future Achievability
Extensive research on the following issues is required for future usage :

 Security needs to be dealt with, as the data is open to all receivers.

 A proper protocol needs to be devised which will address the points
mentioned before.

 Testing needs to be done using real-time simulations to test the
effectiveness.

 Issues such as information reachability and effect of signal interference
need testing.

 Priority should also be specified, so that information about the nearest
aircraft is processed first before moving to data from farther aircrafts.


                                                                              20
•   www.ads-b.com
•   www.faa.gov
•   www.wikipedia.com
•   www.howstuffworks.com
•   www.springerlink.com
•   www.sciencedirect.com


•   M. S. Nolan, “Fundamentals of Air Traffic Control”, 2nd Edition, Wadsworth
    Publishing Company.

•   J. D. Anderson, “Introduction to Flight”, 4th Edition, McGraw-Hill.

•   Charles E. Perkins, “Ad-Hoc Networking”, 1st Edition, Addison and Wesley
    Publishing Company.

•   “Aviation Today” Magazines.

                                                                            21
22
23

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Air Traffic Control Using Ad Hoc Networking

  • 1. By Sharad Saurabh 3rd year, Dept. of Instrumentation & Control SRM University & Sayan Chakrabarty 3rd year, Dept. of Instrumentation & Control SRM University 1
  • 2. Ad-hoc literally means Something ‘created or done for a specific purpose only’.  Ad-hoc network is a dynamic network which can be created anywhere with just two basic nodes and does not require any centralized infrastructure.  Each node has a certain range of communication in which it can transmit or receive data.  If it needs to communicate to a node which is outside its range, it may do so by sending the data to a node which is within its range. That node will transmit to the next and so on till it reaches its designated destination.  Data is transmitted in the form of small packets. 2
  • 3. Devices such as laptops, PDAs, mobile phones, MP3 players etc, can be made to interact using Ad-hoc networking In fact this is being used in technologies such as Bluetooth and Wi-Fi to connect various devices. Now-a-days, most of the above mentioned devices come with in built facilities to support ad hoc networking. 3
  • 4. Contemporary communication means in aircrafts include :  Radio Communication from ground (TIS-B)  RADAR (Radio Detection and Ranging): Air Traffic Control (ATC) Radars Secondary Surveillance Radar (SSR) (Airport Surveillance Radar) Ground Control Approach (GCA) Radars PAR Systems Distance Measuring Equipment (DME) Radio Beacons Identification Friend or Foe (IFF) Systems IFF Interrogator IFF Transponder •Altimeter (AL) Radar Systems •Terrain-Following Radar (TFR) Systems 4
  • 5. 5
  • 6. Automatic Dependent Surveillance-Broadcast (ADS-B)  Data is broadcast in the form of discrete packets.  Since the mid-1990s, FAA has focused on two different ADS-B frequencies- 1. 978 MHz Universal Access Transceiver – used by the General Aviation (GA). 2. 1090 MHz Extended Squitter (ES) – used by airliners and other large aircraft.  The 1090ES is selected for its international interoperability, whereas the UAT link is for its weather graphics up-link capacity and low cost. 6
  • 7. 7
  • 8. Accuracy does not seriously degrade with range, atmospheric conditions, or target altitude. • Update intervals do not depend on the rotational speed or reliability of mechanical antennas. • Accuracy is unaffected by the range to the aircraft. • Also operable in lower altitudes and mountainous regions. • Relatively inexpensive technology, with costs for equivalent radar coverage running in the 0.1 to 0.05 range. • A single Mode S 1090ES ADS-B ground station can cost anywhere from $150,000 - $300,000 USD, including installation. 8
  • 9. Mode S 1090ES ADSB Sample Mode S Multilateration and 1090ES ADS-B Ground and Multilateration Ground Station Installation for FAA ASDE-X Program. Stations Deployed On Oil Platforms In Gulf of Mexico For Helicopter and En Route Tracking 9
  • 10. Airbus has stated its intent to begin equipping all new transport class aircraft it produces with Mode S 1090ES as a standard feature.  UPS, a US freight carrier, is in the process of installing Mode S 1090ES ADS-B avionics on all 107 Boeing 757s and 767s it operates.  Australia, Japan, China and some parts of Europe & Africa have also opted for ADS-B and plan to implement it soon. # Map showing European airports with ADS-B compatibility 10
  • 11. Essentially a single-node operation scheme.  Range is limited to the direct transmission range of the airborne Antenna.  The 1090ES is likely to support ADS-B applications that do not require air-to-air ranges exceeding 80km when used in the highest density airspace and will provide ranges of 180 km in lower traffic density airspace. This is too short for longer range applications and flight-path-conflict resolutions.  Research is on to implement an airborne ADS-B architecture that will readily accommodate a second ADS-B link in addition to the 1090ES.  However, these additions can be too expensive and problematic, especially when in India, we are yet to realise the full potential benefits of even one digital link of the single-node system. 11
  • 12. Fig illustrates the main drawback of ADS-B 12
  • 13. 13
  • 14. Multiple-hop means an ad hoc network where the data exchange is not limited to just a single pair but it includes a number of nodes.  The nodes not only transmit their own data but also those received from neighbouring nodes.  One aircraft can be made to broadcast not only its own state information periodically, but also the state information it receives about neighbouring aircrafts.  Clusters can be disjoint from, or overlapped with each other. 14
  • 15. Fig. shows a cluster of planes forming a multiple hop network 15
  • 16. Possible to select more useful information over a larger area for cockpit display and onboard automation systems.  Pilot can virtually see other aircrafts beyond its transmission range.  Live data can be sent in a reliable and timely manner.  Can provide a collision-free and extended traffic coverage. 16
  • 17. 17
  • 18. The transmitted Protocol specifies The maximum number of hops the state information will be relayed How often the state information is broadcast What state information to broadcast The mix of own aircraft information vs. information of other aircraft, etc.  The protocol should also specify a transmission rate such that it is ample to handle the data that it receives and transmits, i.e. the processing rate of the information should be synchronised with frequency with which data is received. 18
  • 19. Fig shows an example of five node network with link delivery probabilities. 21
  • 20. Future Achievability Extensive research on the following issues is required for future usage :  Security needs to be dealt with, as the data is open to all receivers.  A proper protocol needs to be devised which will address the points mentioned before.  Testing needs to be done using real-time simulations to test the effectiveness.  Issues such as information reachability and effect of signal interference need testing.  Priority should also be specified, so that information about the nearest aircraft is processed first before moving to data from farther aircrafts. 20
  • 21. www.ads-b.com • www.faa.gov • www.wikipedia.com • www.howstuffworks.com • www.springerlink.com • www.sciencedirect.com • M. S. Nolan, “Fundamentals of Air Traffic Control”, 2nd Edition, Wadsworth Publishing Company. • J. D. Anderson, “Introduction to Flight”, 4th Edition, McGraw-Hill. • Charles E. Perkins, “Ad-Hoc Networking”, 1st Edition, Addison and Wesley Publishing Company. • “Aviation Today” Magazines. 21
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