WO2006137937A3 - Takeoff and landing performance indicator for fixed wing aircraft - Google Patents

Takeoff and landing performance indicator for fixed wing aircraft Download PDF

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Publication number
WO2006137937A3
WO2006137937A3 PCT/US2005/040655 US2005040655W WO2006137937A3 WO 2006137937 A3 WO2006137937 A3 WO 2006137937A3 US 2005040655 W US2005040655 W US 2005040655W WO 2006137937 A3 WO2006137937 A3 WO 2006137937A3
Authority
WO
WIPO (PCT)
Prior art keywords
takeoff
aircraft
velocity
performance
control
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
PCT/US2005/040655
Other languages
French (fr)
Other versions
WO2006137937A2 (en
Inventor
Paul A Voisin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
L3 Aviation Products Inc
Original Assignee
L3 Communications Avionics Systems 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 L3 Communications Avionics Systems Inc filed Critical L3 Communications Avionics Systems Inc
Priority to US11/718,907 priority Critical patent/US20090125168A1/en
Priority to CA002586766A priority patent/CA2586766A1/en
Priority to EP05858312A priority patent/EP1811887A2/en
Priority to BRPI0517702-2A priority patent/BRPI0517702A/en
Publication of WO2006137937A2 publication Critical patent/WO2006137937A2/en
Anticipated expiration legal-status Critical
Publication of WO2006137937A3 publication Critical patent/WO2006137937A3/en
Ceased legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G08G5/52—Navigation or guidance aids for take-off
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0083—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots to help an aircraft pilot in the rolling phase
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G08G5/54—Navigation or guidance aids for approach or landing
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/50—Navigation or guidance aids
    • G08G5/55—Navigation or guidance aids for a single aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Traffic Control Systems (AREA)

Abstract

A runway performance monitor and method for an aircraft, includes providing a control, and monitoring aircraft performance. The control has baseline performance data of the aircraft during takeoff and/or landing. The control compares actual performance of the aircraft during takeoff and/or landing with the baseline performance data and calculates predicted information relevant to takeoff velocity and/or landed velocity. The control may determine braking point data and/or takeoff point data for that aircraft as a function of aircraft performance and runway location and length. The braking point data defines a location relevant to decelerating of the aircraft to a landed velocity. The takeoff point data defines a location relevant to accelerating of the aircraft to takeoff velocity. A display may be provided to display the information relevant to takeoff velocity and/or landed velocity.
PCT/US2005/040655 2004-11-10 2005-11-09 Takeoff and landing performance indicator for fixed wing aircraft Ceased WO2006137937A2 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US11/718,907 US20090125168A1 (en) 2004-11-10 2005-11-09 Takeoff and landing performance indicator for fixed wing aircraft
CA002586766A CA2586766A1 (en) 2004-11-10 2005-11-09 Takeoff and landing performance indicator for fixed wing aircraft
EP05858312A EP1811887A2 (en) 2004-11-10 2005-11-09 Takeoff and landing performance indicator for fixed wing aircraft
BRPI0517702-2A BRPI0517702A (en) 2004-11-10 2005-11-09 Take-off and landing performance indicator for fixed wing aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US52281304P 2004-11-10 2004-11-10
US60/522,813 2004-11-10

Publications (2)

Publication Number Publication Date
WO2006137937A2 WO2006137937A2 (en) 2006-12-28
WO2006137937A3 true WO2006137937A3 (en) 2007-07-26

Family

ID=37570912

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2005/040655 Ceased WO2006137937A2 (en) 2004-11-10 2005-11-09 Takeoff and landing performance indicator for fixed wing aircraft

Country Status (5)

Country Link
US (1) US20090125168A1 (en)
EP (1) EP1811887A2 (en)
BR (1) BRPI0517702A (en)
CA (1) CA2586766A1 (en)
WO (1) WO2006137937A2 (en)

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* Cited by examiner, † Cited by third party
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US20080215198A1 (en) * 2006-09-22 2008-09-04 Richards Robert E Method and apparatus for providing takeoff runway information and predicting end of runway overrun
JP5174034B2 (en) 2006-12-19 2013-04-03 エンジニアード・アレスティング・システムズ・コーポレーション System and method for improving or increasing information, particularly information regarding runway conditions available to landing aircraft pilots
FR2914770B1 (en) 2007-04-04 2015-11-06 Airbus France METHOD AND DEVICE FOR DETERMINING A DELAY MARGIN AT AIRCRAFT LANDING
US8204637B1 (en) * 2007-12-20 2012-06-19 The United States Of America As Represented By The Secretary Of The Navy Aircraft approach to landing analysis method
FR2936077B1 (en) * 2008-09-16 2014-12-12 Airbus France METHOD AND DEVICE FOR AIDING THE CONTROL OF AN AIRCRAFT DURING A LANDING PHASE.
US8195347B2 (en) * 2009-05-28 2012-06-05 The Boeing Company Method and system for approach decision display
US8560150B1 (en) * 2010-07-07 2013-10-15 The Boeing Company Methods and systems for landing decision point
US8359542B2 (en) 2010-08-13 2013-01-22 Lockheed Martin Corporation Machines, program products, and computer-implemented methods for interactive aircraft performance substantiation
US8441376B1 (en) * 2010-09-29 2013-05-14 Rockwell Collins, Inc. System, module, and method for presenting surface symbology on an aircraft display unit
US8630752B2 (en) 2011-09-08 2014-01-14 Honeywell International Inc. System and method of displaying airspeed information for an aircraft
US9058742B2 (en) 2013-02-12 2015-06-16 Ge Aviation Systems, Llc Methods for illustrating aircraft situational information
US20150100182A1 (en) * 2013-10-04 2015-04-09 Shouqin Zhu Method for fighter takeoff and landing within ultra-short distance (ultra-stol)
US9643735B2 (en) 2015-05-27 2017-05-09 Honeywell International Inc. Integration of braking action information with flight deck runway functions
US10214300B2 (en) * 2016-11-10 2019-02-26 Honeywell International Inc. System and method for displaying runway overrun information
US20190354644A1 (en) * 2018-05-18 2019-11-21 Honeywell International Inc. Apparatuses and methods for detecting anomalous aircraft behavior using machine learning applications
JP7560458B2 (en) * 2018-12-11 2024-10-02 イーグル エアロスペース，リミテッド Method and software program for assessing aircraft landing and surface movement performance - Patents.com
US20220024601A1 (en) * 2020-07-23 2022-01-27 Gulfstream Aerospace Corporation Controllers and aircraft with variable engine thrust takeoff system
EP4086877A1 (en) * 2021-05-07 2022-11-09 Honeywell International Inc. Method and apparatus for runway overrun avoidance function for pilot defined custom landing surface
CN117002747A (en) * 2023-06-26 2023-11-07 中国商用飞机有限责任公司 A method and device for monitoring aircraft pollution runway performance test flight

Citations (2)

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US20050230529A1 (en) * 1996-05-13 2005-10-20 Andrew James Towne Hiigh wing monoplane aerospace plane based fighter.
US20060095156A1 (en) * 2004-10-20 2006-05-04 Baiada R M Method and system for tactical airline system management

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US3128445A (en) * 1958-09-04 1964-04-07 Bendix Corp Aircraft take-off monitoring
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Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050230529A1 (en) * 1996-05-13 2005-10-20 Andrew James Towne Hiigh wing monoplane aerospace plane based fighter.
US20060095156A1 (en) * 2004-10-20 2006-05-04 Baiada R M Method and system for tactical airline system management

Also Published As

Publication number Publication date
CA2586766A1 (en) 2006-12-28
US20090125168A1 (en) 2009-05-14
EP1811887A2 (en) 2007-08-01
WO2006137937A2 (en) 2006-12-28
BRPI0517702A (en) 2008-10-21

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