Close/intra-formation positioning collision avoidance system and method

Abstract

A passive Traffic Alert and Collision Avoidance System (TCAS) and method is based on receiving and processing Mode-S transponder messages without the TCAS computer having to interrogate the transponders of the respective aircraft flying in formation (i.e., a passive TCAS). A TCAS computer and Mode-S transponder are used to provide distributed intra-formation control among multiple cells of aircraft flying in formation or close-in. The Mode-S transponder provides ADS-B Global Positioning System (GPS) squitter data to the TCAS computer; the TCAS computer receives and processes the data without having to interrogate the transponders of the multiple cells of aircraft. The method and system allow a safe separation between 2 to 250 aircraft flying in formation at selectable ranges.

Description

I. CROSS-REFERENCE TO RELATED APPLICATIONS[0001] This application is related to co-pending application, filed on even date herewith, entitled "Vertical Speed Indicator / Traffic Resolution Advisory Display For TCAS."II. BACKGROUND OF THE INVENTION[0002] The present invention relates generally to the field of avionics for collision avoidance systems (CAS). More specifically, the present invention relates generally to airborne traffic alert and collision avoidance systems and transponders. The collision avoidance system described herein has the capability to position and separate aircraft in a large flight formation in, for example, night / instrument meteorological conditions.[0003] Spurred by the collision of two airliners over the Grand Canyon in 1956, the airlines initiated a study of collision avoidance concepts. By the late 1980's, a system for airborne collision avoidance was developed with the cooperation of the airlines, the aviation industry, and the Federal Aviation Administrat...

AI Technical Summary

Problems solved by technology

Furthermore, collision avoidance is a problem for both military and commercial aircraft alike.

In addition, a large, simultaneous number of TCAS interrogations from close-in formation aircraft members generate significant radio frequency (RF) interference and could potentially degrade the effectiveness of maintaining precise position / separation criteria with respect to other aircraft and obstacles.

Also, the system is to be compatible (primarily because of cost issues) with current station keeping equipment (SKE) systems or they will not be able to fly IMC formation with SKE-equipped aircraft.

First, once an aircraft joins the formation, the ETCAS does not itself or in conjunction with any other on-board system maintain aircraft position and separation within the formation.

Second, the ETCAS Vertical Speed Indicator / Traffic Resolution Alert (VSI / TRA) display does not annunciate relative velocity (range-rate) of the lead formation and member aircraft.

Transponder interrogations and the resulting Mode-S transponder replies significantly increase RF reception interference with a large formation of aircraft and could degrade the effectiveness of maintaining precise position / separation criteria.

In addition, the increased composite level of RF severely inhibits a large formation from covertly traversing airspace undetected.

Another problem is presented in previous systems wherein station keeping equipment (SKE) on existing military aircraft can support a formation of only 16 aircraft.

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