WO2000065373A3 - Midair collision avoidance system - Google Patents

Midair collision avoidance system Download PDF

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Publication number
WO2000065373A3
WO2000065373A3 PCT/US2000/009517 US0009517W WO0065373A3 WO 2000065373 A3 WO2000065373 A3 WO 2000065373A3 US 0009517 W US0009517 W US 0009517W WO 0065373 A3 WO0065373 A3 WO 0065373A3
Authority
WO
WIPO (PCT)
Prior art keywords
tactical
air
module
formation
collision avoidance
Prior art date
Application number
PCT/US2000/009517
Other languages
French (fr)
Other versions
WO2000065373A2 (en
Inventor
My Tran
Original Assignee
Honeywell Int Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honeywell Int Inc filed Critical Honeywell Int Inc
Priority to JP2000617003A priority Critical patent/JP2003522990A/en
Priority to AU66044/00A priority patent/AU751278B2/en
Priority to IL14581900A priority patent/IL145819A/en
Priority to EP00953627A priority patent/EP1279047A2/en
Priority to CA002367794A priority patent/CA2367794A1/en
Publication of WO2000065373A2 publication Critical patent/WO2000065373A2/en
Publication of WO2000065373A3 publication Critical patent/WO2000065373A3/en

Links

Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0004—Transmission of traffic-related information to or from an aircraft
    • G08G5/0008—Transmission of traffic-related information to or from an aircraft with other aircraft
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
    • G01S13/88—Radar or analogous systems specially adapted for specific applications
    • G01S13/93—Radar or analogous systems specially adapted for specific applications for anti-collision purposes
    • G01S13/933—Radar or analogous systems specially adapted for specific applications for anti-collision purposes of aircraft or spacecraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0047—Navigation or guidance aids for a single aircraft
    • G08G5/0052—Navigation or guidance aids for a single aircraft for cruising
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0073—Surveillance aids
    • G08G5/0078—Surveillance aids for monitoring traffic from the aircraft
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/04—Anti-collision systems
    • G08G5/045—Navigation or guidance aids, e.g. determination of anti-collision manoeuvers

Abstract

A midair collision avoidance system (MCAS) employs an existing design of Traffic Alert and Collision Avoidance System (TCAS) as a module (20) and seamlessly integrates it with a customized tactical module (22) which is capable of providing unique tactical avoidance guidance control and display. The tactical module handles all phases of a tactical mission, including formation flight (62) (e.g., formation fall-in, arming formation flight, engaging formation flight following, and formation break-away), and an air-refueling sequence (64) (e.g., rendezvous, link-up, re-fueling, and disengaging air-refueling). The tactical module divides the air space around the aircraft into advisory (84), caution (82), and warning (80) zones and for each provides display, tone and voice alerts to facilitate pop-up avoidance guidance commands. Military aircraft can thus effectively avoid mid air and near mid air colision situations in all three different operation modes: air traffic control (ATC) management mode, tactical mode, and a mixed mode.
PCT/US2000/009517 1999-04-08 2000-04-07 Midair collision avoidance system WO2000065373A2 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP2000617003A JP2003522990A (en) 1999-04-08 2000-04-07 Air collision avoidance system
AU66044/00A AU751278B2 (en) 1999-04-08 2000-04-07 Midair collision avoidance system
IL14581900A IL145819A (en) 1999-04-08 2000-04-07 Midair collision avoidance system
EP00953627A EP1279047A2 (en) 1999-04-08 2000-04-07 Midair collision avoidance system
CA002367794A CA2367794A1 (en) 1999-04-08 2000-04-07 Midair collision avoidance system

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12865599P 1999-04-08 1999-04-08
US60/128,655 1999-04-08
US09/538,804 US6262679B1 (en) 1999-04-08 2000-03-30 Midair collision avoidance system

Publications (2)

Publication Number Publication Date
WO2000065373A2 WO2000065373A2 (en) 2000-11-02
WO2000065373A3 true WO2000065373A3 (en) 2001-03-01

Family

ID=26826796

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2000/009517 WO2000065373A2 (en) 1999-04-08 2000-04-07 Midair collision avoidance system

Country Status (7)

Country Link
US (4) US6262679B1 (en)
EP (1) EP1279047A2 (en)
JP (1) JP2003522990A (en)
AU (1) AU751278B2 (en)
CA (1) CA2367794A1 (en)
IL (1) IL145819A (en)
WO (1) WO2000065373A2 (en)

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