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

Aircraft traffic alert and collision avoidance device

Patent 5157615 Issued on October 20, 1992. Estimated Expiration Date: Icon_subject December 31, 2011. 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

Computer system to prevent collision between moving objects such as aircraft moving from one sector to another
Patent #: 4063073
Issued on: 12/13/1977
Inventor: Strayer

Terrain advisory system
Patent #: 4646244
Issued on: 02/24/1987
Inventor: Bateman ,   et al.

Resource allocation system and method
Patent #: 4797839
Issued on: 01/10/1989
Inventor: Powell

N-Dimensional information display method for air traffic control
Patent #: 4823272
Issued on: 04/18/1989
Inventor: Inselberg

Process for en route aircraft conflict alert determination and prediction
Patent #: 4839658
Issued on: 06/13/1989
Inventor: Kathol ,   et al.

Tactical routing system and method
Patent #: 4947350
Issued on: 08/07/1990
Inventor: Murray, et al.

Conflict detection and resolution between moving objects
Patent #: 5058024
Issued on: 10/15/1991
Inventor: Inselberg

Aircraft traffic alert and collision avoidance device Patent #: 5077673
Issued on: 12/31/1991
Inventor: Brodegard, et al.

Inventors

Assignee

Application

No. 815489 filed on 12/31/1991

US Classes:

701/301, Collision avoidance342/30, With transponder342/455Having collision avoidance

Examiners

Primary: Black, Thomas G.

Attorney, Agent or Firm

International Class

G06F 015/50

Abstract

A passive aircraft Traffic alert and Collision Avoidance Device (TCAD) is based on sensing and responding to transponder replies of other aircraft to SSR interrogations. In order to avoid masking other aircraft replies by the host transponder TCAD repeatedly and randomly suppresses the host transponder and simultaneoulsly listens for other aircraft replies. Suppression on each occasion is effective for an equal and predetermined duration which is much longer than a typical replay, in a preferred embodiment the suppression/listen duration is 725 μs. In this embodiment the time between successive suppression/listen occasions is random between 725 μs. and 5.025 ms. with an average value of about 2.9 ms. Digital signal processing is used to detect and discard garbled or overlapping replies. Each valid reply, exhibiting a minimum pulse amplitude, is decoded and correlated with a calibrated range parameter and given a time tag. Successive replies which match to within predetermined criteria in time and calibrated range are merged to track the positional relation between the host and other aircraft. The positional relation between other aircraft and the host are evaluated via a priority table in terms of relative altitude and range to locate that craft which poses the highest threat to the host. Parameters of such a craft are displayed. In the event a craft penetrates a shield of programmable size an audible alert is sounded. TCAD provides for shields for each of a plurality of flight regimes, such as terminal, standard and enroute.

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