Air traffic surveillance and communication system

• US 5,798,726 A
• Filed: 01/24/1997
• Issued: 08/25/1998
• Est. Priority Date: 02/03/1995
• Status: Expired due to Term

• Current Assignee: Harris Corporation (L3Harris Technologies, Inc.)
• Original Assignee: Stanford Telecommunications, Inc. (Nokia Corporation)
• Inventors: Greenberg, Steve, Zakrzewski, Edward J., Kefaliotis, John, Schuchman, Leonard, Bruno, Ronald
• Primary Examiner(s): Lobo, Ian J.
• Application Number:
  US08/682,546
• Time in Patent Office: 578 Days
• Field of Search: 342/29, 342/32, 342/36, 342/37, 342/38, 342/43
• US Class Current: 342/37
• CPC Class Codes: G08G 5/0013 with a ground station
• CPC Class Codes: G08G 5/0082 for monitoring traffic from a ground station radar or analogous systems specially adapted for traffic control G01S13/91
• CPC Class Codes: H04B 7/18502 Airborne stations

Abstract

Air traffic surveillance and communication system for air traffic controllers includes a plurality of ground based first digital radio transceivers, each first digital radio transceiver 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. 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 pair. A plurality of aircraft based second digital radio transceivers are provided, 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 a GPS receiver system for producing aircraft navigation data selected from aircraft latitude, longitude, altitude, speed, heading and glide. The navigational data source is coupled to the respective aircraft transceiver for transmission on the 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 the aircraft.

Claims

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

a plurality of around 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, 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 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 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 around 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 wherein each said digital radio transceiver means includes means for causing said digital radio transceiver to operate with a 10 kHz spacing.

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

a plurality of ground based first 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, 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 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 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 around 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 wherein said GPS receiver means includes triply redundant GPS receivers and majority voting means to ensure high accuracy of said navigational data.

3. The air traffic surveillance and communication system defined in claim 2 wherein each said digital audio transceivers incorporate differential QPSK signal modulation.

4. 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.

5. The air traffic surveillance and communication system defined in claim 2 wherein said system includes means for causing said transceiver to operate in a time division multiple access (TDMA) mode having super-frames with multiple subframes within each super-frame.

6. The air traffic surveillance and communication system defined in claim 5 wherein each said subframe has guard band and a synchronizing preamble followed by a predetermined data format.

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

providing a plurality of ground based first 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 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.

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

a plurality of ground based first 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, 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 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 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 around 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 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.