U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Air traffic surveillance and communication system

Patent 5459469 Issued on October 17, 1995. Estimated Expiration Date: Icon_subject February 4, 2014. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

3495260

Integrated terminal area surveillance system
Patent #: 4060805
Issued on: 11/29/1977
Inventor: McComas

Satellite-based vehicle position determining system Patent #: 4359733
Issued on: 11/16/1982
Inventor: O'Neill

Inventors

Assignee

Application

No. 192327 filed on 02/04/1994

US Classes:

342/37, Secondary Surveilance Radar (SSR) or Air Traffic Control Radar Beacon System (ATCRBS)342/32, Included in Secondary Surveilance Radar (SSR) or Air Traffic Control Radio Beacon System (ATCRBS)342/36AIR TRAFFIC CONTROL

Examiners

Primary: Lobo, Ian J.

Attorney, Agent or Firm

International Classes

G01S 013/93
G01S 013/74

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.

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