Air traffic surveillance and communication system

• US 5,459,469 A
• Filed: 02/04/1994
• Issued: 10/17/1995
• Est. Priority Date: 02/04/1994
• Status: Expired due to Term

• Current Assignee: Exelis Incorporated (L3Harris Technologies, Inc.)
• Original Assignee: Stanford Telecommunications, Inc. (Nokia Corporation)
• Inventors: Schuchman, Leonard, Greenberg, Steve, Bruno, Ronald C., Zakrzewski, Edward J., Kefaliotis, John
• Primary Examiner(s): Lobo, Ian J.
• Application Number:
  US08/192,327
• Time in Patent Office: 620 Days
• Field of Search: 342/29, 342/32, 342/36, 342/37, 342/43, 342/38
• US Class Current: 342/37
• CPC Class Codes: G01S 13/765 with exchange of information between interrogator and responder
• CPC Class Codes: G01S 13/767 Responders; Transponders teaching or practice apparatus for gun-aiming or gun-laying using reflecting targets or active targets F41G3/26
• CPC Class Codes: G01S 13/86 Combinations of radar systems with non-radar systems, e.g. sonar, direction finder
• CPC Class Codes: G01S 13/91 for traffic control G01S13/93 takes precedence
• CPC Class Codes: G01S 19/15 Aircraft landing systems
• CPC Class Codes: G01S 19/35 Constructional details or hardware or software details of the signal processing chain
• CPC Class Codes: G01S 7/003 Transmission of data between radar, sonar or lidar systems and remote stations
• CPC Class Codes: H04B 7/18506 Communications with or from aircraft, i.e. aeronautical mobile service

Abstract

An air traffic surveillance and communication system for air traffic controllers, includes a plurality of ground based first radio transceivers located in specific geographic sectors, respectively, and having a first frequency channel for supporting party-line digital voice and a second frequency channel dedicated to supporting a digital data channel for down-linking dependent surveillance data and for both up-link and down-link data communications. The first and second frequency channels are paired such that each time a frequency change is commanded by the ground both the first and second frequency channels will be automatically tuned to a new air-ground frequency paid. The system also includes a plurality of aircraft based second digital radio transceivers, one located in each aircraft. Each second radio transceiver has corresponding first and second frequency channels and a navigational data source on each aircraft. The navigational data source incorporates triply redundant GPS receivers for producing highly accurate aircraft navigation data selected from aircraft latitude, longitude, altitude, speed, heading and glide data which is coupled to the respective aircraft transceiver for transmission on said second channel to at least one of the plurality of ground based first radio transceivers. Each ground based first radio transceiver has a communication controller for formatting up-link data and separating down-linked surveillance data and disseminating same to air traffic controllers in the sectors of said aircraft. In a preferred embodiment, in a TDMA format with digital radio transceiver operates with a 12.5 kHz spacing, differential QPSK signal modulation is used and each broadcast is by short transmission bursts having a guard band signal preamble and a management/user data field.

Claims

1. Air traffic surveillance and communication system for air traffic controllers, comprising:

a plurality of ground based first digital radio transceiver means, each first digital radio transceiver means being located in specific geographic sectors, respectively, and having a first frequency channel for supporting party-line digital voice, and a second frequency channel dedicated to supporting a digital data channel for down-linking surveillance data and for both up-link and down-link data communications, said first and second frequency channels being paired such that each time a frequency change is commanded by the ground both the first and second frequency channels will be simultaneously and automatically tuned to a new air-ground frequency pair,

a plurality of aircraft based second digital radio transceiver means, one located in each aircraft, each second radio transceiver having further paired first and second frequency channels which correspond to the paired first and second frequency channels in said plurality of ground based first digital radio transceiver means, a navigational data source on each aircraft, said navigational data source including GPS receiver means for producing aircraft navigation data selected from aircraft latitude, longitude, altitude, speed, heading and glide, and means coupling said navigational data source to the respective aircraft transceiver for transmission on said second channel to at least one of said plurality of ground based first radio transceiver means,

each said ground based first radio transceiver means having a communication controller for formatting up-link data and separating down-linked surveillance data and disseminating same to air traffic controllers in the sectors of said aircraft.

2. The air traffic surveillance and communication system defined in claim 1 wherein each said digital radio transceiver means includes means for causing said digital radio transceiver to operate with a 12.5 kHz spacing.

3. The air traffic surveillance and communication system defined in claim 1 wherein said GPS receiver means includes triply redundant GPS receivers and majority voting means to ensure high accuracy of said navigational data.

4. The air traffic surveillance and communication system defined in claim 1 wherein each said digital radio transceiver incorporates differential QPSK signal modulation.

5. The air traffic surveillance and communication system defined in claim 2 wherein each radio transceiver broadcast is by short transmission bursts having a guard band signal preamble and a management/user data field.

6. The air traffic surveillance and communication system defined in claim 1 wherein said system includes means for causing each said digital radio transceiver to operate in a time division multiple access (TDMA) mode having super-frames with multiple subframes within each super-frame.

7. The air traffic surveillance and communication system defined in claim 6 wherein each said subframe has guard band and a synchronizing preamble followed by a predetermined data format.

8. The air traffic surveillance and communication system defined in claim 1 wherein said aircraft-based second digital radio transceiver means is adapted to receive all other aircraft-based transceiver transmission bursts in its vicinity and provide signals indicative of the latitude, longitude, altitude, speed heading and glide of other aircraft in said vicinity.

9. Air traffic surveillance and communication method for air traffic controllers, comprising:

providing a plurality of ground based first digital radio transceiver means, each first digital radio transceiver means being located in specific geographic sectors, respectively, and having a first frequency channel for supporting party-line digital voice, and a second frequency channel dedicated to supporting a digital data channel for down-linking dependent surveillance data and for both up-link and down-link data communications, each said ground based first radio transceiver means having a communication controller for formatting up-link data and separating down-linked surveillance data and disseminating same to air traffic controllers in the sectors of said aircraft,

providing a plurality of aircraft based second digital radio transceiver means, one located in each aircraft, each second radio transceiver having corresponding first and second frequency channels, a navigational data source on each aircraft, said navigational data source including GPS receiver means for producing aircraft navigation data selected from aircraft latitude, longitude, altitude, speed, heading and glide, and means coupling said navigational data source to the respective aircraft transceiver for transmission on said second channel to at least one of said plurality of ground based first radio transceiver means,

pairing said first and second frequency channels such that each time a frequency change is commanded by the ground both the first and second frequency channels will be automatically tuned to a new air-ground frequency pair.