WO2002068905A3 - Closure indicator for cockpit traffic display - Google Patents

Closure indicator for cockpit traffic display Download PDF

Info

Publication number
WO2002068905A3
WO2002068905A3 PCT/US2001/050311 US0150311W WO02068905A3 WO 2002068905 A3 WO2002068905 A3 WO 2002068905A3 US 0150311 W US0150311 W US 0150311W WO 02068905 A3 WO02068905 A3 WO 02068905A3
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
selected target
closure
closure indicator
target aircraft
Prior art date
Application number
PCT/US2001/050311
Other languages
French (fr)
Other versions
WO2002068905A8 (en
WO2002068905A2 (en
Inventor
Steve Horvath
Craig Bowers
Robert Grove
Original Assignee
United Parcel Service 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 United Parcel Service Inc filed Critical United Parcel Service Inc
Priority to JP2002567776A priority Critical patent/JP2004534208A/en
Priority to MXPA03003629A priority patent/MXPA03003629A/en
Priority to AU2002258373A priority patent/AU2002258373A1/en
Priority to CA002426726A priority patent/CA2426726A1/en
Priority to EP01273064A priority patent/EP1332335A2/en
Publication of WO2002068905A2 publication Critical patent/WO2002068905A2/en
Publication of WO2002068905A3 publication Critical patent/WO2002068905A3/en
Publication of WO2002068905A8 publication Critical patent/WO2002068905A8/en

Links

Classifications

    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0017Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
    • G08G5/0021Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
    • G01C23/005Flight directors
    • GPHYSICS
    • G08SIGNALLING
    • G08GTRAFFIC CONTROL SYSTEMS
    • G08G5/00Traffic control systems for aircraft, e.g. air-traffic control [ATC]
    • G08G5/0073Surveillance aids
    • G08G5/0078Surveillance aids for monitoring traffic from the aircraft

Abstract

A system for graphically displaying on a cockpit display an indication of closure (i.e. a 'closure indicator') with a selected target aircraft. In a preferred embodiment of the invention, the system only displays a closure indicator if: (1) the selected target aircraft is within a pre-determined monitoring zone; and (2) the track of the selected target aircraft is within a pre-determined variation angle of the track of the Own Ship aircraft. If the rate of closure between the selected target aircraft and the Own Ship aircraft is within a predetermined range of values, the closure indicator includes a closing/receding indicia (such as an upwardly or downwardly directed arrow) that indicates whether the Own Ship aircraft is closing in on or receding from the selected target aircraft. The system preferably removes the closure indicator from display when the Own Ship aircraft or the selected target aircraft ceases to be airborne.
PCT/US2001/050311 2000-10-25 2001-10-25 Closure indicator for cockpit traffic display WO2002068905A2 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
JP2002567776A JP2004534208A (en) 2000-10-25 2001-10-25 Approach indicator for cockpit traffic display
MXPA03003629A MXPA03003629A (en) 2000-10-25 2001-10-25 Graphic closure indicator for cockpit traffic display.
AU2002258373A AU2002258373A1 (en) 2000-10-25 2001-10-25 Closure indicator for cockpit traffic display
CA002426726A CA2426726A1 (en) 2000-10-25 2001-10-25 Closure indicator for cockpit traffic display
EP01273064A EP1332335A2 (en) 2000-10-25 2001-10-25 Graphic closure indicator for cockpit traffic display

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US24323900P 2000-10-25 2000-10-25
US60/243,239 2000-10-25

Publications (3)

Publication Number Publication Date
WO2002068905A2 WO2002068905A2 (en) 2002-09-06
WO2002068905A3 true WO2002068905A3 (en) 2003-03-06
WO2002068905A8 WO2002068905A8 (en) 2003-11-13

Family

ID=22917895

Family Applications (2)

Application Number Title Priority Date Filing Date
PCT/US2001/050311 WO2002068905A2 (en) 2000-10-25 2001-10-25 Closure indicator for cockpit traffic display
PCT/US2001/050171 WO2002058033A2 (en) 2000-10-25 2001-10-25 Altitude range filter for cockpit traffic display

Family Applications After (1)

Application Number Title Priority Date Filing Date
PCT/US2001/050171 WO2002058033A2 (en) 2000-10-25 2001-10-25 Altitude range filter for cockpit traffic display

Country Status (8)

Country Link
US (4) US6826458B2 (en)
EP (2) EP1332483A2 (en)
JP (2) JP2004518213A (en)
CN (2) CN1476593A (en)
AU (2) AU2002251706A1 (en)
CA (2) CA2426726A1 (en)
MX (2) MXPA03003629A (en)
WO (2) WO2002068905A2 (en)

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Also Published As

Publication number Publication date
CA2426724A1 (en) 2002-07-25
US20050065671A1 (en) 2005-03-24
US20020111740A1 (en) 2002-08-15
WO2002058033A8 (en) 2003-11-13
MXPA03003628A (en) 2004-03-26
US7124000B2 (en) 2006-10-17
US20020128755A1 (en) 2002-09-12
US20090069959A1 (en) 2009-03-12
MXPA03003629A (en) 2004-03-26
EP1332335A2 (en) 2003-08-06
CN1476592A (en) 2004-02-18
US7382285B2 (en) 2008-06-03
WO2002058033A3 (en) 2003-03-13
WO2002058033A2 (en) 2002-07-25
JP2004534208A (en) 2004-11-11
AU2002251706A1 (en) 2002-07-30
EP1332483A2 (en) 2003-08-06
WO2002068905A8 (en) 2003-11-13
US7696904B2 (en) 2010-04-13
CN1476593A (en) 2004-02-18
JP2004518213A (en) 2004-06-17
US6826458B2 (en) 2004-11-30
CA2426726A1 (en) 2002-09-06
WO2002068905A2 (en) 2002-09-06
AU2002258373A1 (en) 2002-09-12

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