BR112013008383A2 - sistema de direção de roda de nariz de controle de ganho variável - Google Patents

sistema de direção de roda de nariz de controle de ganho variável

Info

Publication number
BR112013008383A2
BR112013008383A2 BR112013008383A BR112013008383A BR112013008383A2 BR 112013008383 A2 BR112013008383 A2 BR 112013008383A2 BR 112013008383 A BR112013008383 A BR 112013008383A BR 112013008383 A BR112013008383 A BR 112013008383A BR 112013008383 A2 BR112013008383 A2 BR 112013008383A2
Authority
BR
Brazil
Prior art keywords
gain
steering system
parking
wheel steering
nose wheel
Prior art date
Application number
BR112013008383A
Other languages
English (en)
Other versions
BR112013008383B1 (pt
Inventor
Hiroki Oyama
Original Assignee
Honda Patents & Tech North Am
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 Honda Patents & Tech North Am filed Critical Honda Patents & Tech North Am
Publication of BR112013008383A2 publication Critical patent/BR112013008383A2/pt
Publication of BR112013008383B1 publication Critical patent/BR112013008383B1/pt

Links

Classifications

    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/50—Steerable undercarriages; Shimmy-damping

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
  • Automatic Cycles, And Cycles In General (AREA)

Abstract

sistema de direção de roda de nariz de controle de ganho variável. a invenção refere-se a um método para determinar um ângulo de direção alvo para o trem de pouso de nariz de um avião que inclui receber os dados de entrada de pedal de leme em uma unidade de controle de direção, receber os dados de velocidades de avião na unidade de controle de direção, calcular um ganho normal, calcular um ganho de estacionamento, e somar o ganho normal e o ganho de estacionamento para determinar o ângulo de direção alvo. o ganho normal é uma quantidade positiva em todas as faixas de velocidade de avião e de curso de pedal. o ganho de estacionamento é uma quantidade positiva nas faixas de velocidade de estacionamento e de taxiamento. um sistema de direção de roda de nariz está também descrito.
BR112013008383-2A 2010-10-08 2011-10-06 método para determinar ângulo de direção alvo para o trem de pouso de nariz de avião e unidade de controle de direção para sistema de direção de roda de nariz para avião BR112013008383B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12/900,825 2010-10-08
US12/900,825 US8473159B2 (en) 2010-10-08 2010-10-08 Variable gain control nose wheel steering system
PCT/US2011/055146 WO2012048139A2 (en) 2010-10-08 2011-10-06 Variable gain control nose wheel steering system

Publications (2)

Publication Number Publication Date
BR112013008383A2 true BR112013008383A2 (pt) 2016-06-14
BR112013008383B1 BR112013008383B1 (pt) 2020-12-22

Family

ID=45925767

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013008383-2A BR112013008383B1 (pt) 2010-10-08 2011-10-06 método para determinar ângulo de direção alvo para o trem de pouso de nariz de avião e unidade de controle de direção para sistema de direção de roda de nariz para avião

Country Status (10)

Country Link
US (1) US8473159B2 (pt)
EP (1) EP2625578B1 (pt)
JP (1) JP5767713B2 (pt)
CN (1) CN103562065B (pt)
AU (1) AU2011311970B2 (pt)
BR (1) BR112013008383B1 (pt)
CA (1) CA2813603C (pt)
ES (1) ES2626703T3 (pt)
MX (1) MX2013003839A (pt)
WO (1) WO2012048139A2 (pt)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8732753B2 (en) * 2010-06-07 2014-05-20 Guest Tek Interactive Entertainment Ltd. Method of operating one or more controllable devices in dependence upon commands received from a plurality of mobile devices and system controller thereof
JP5735253B2 (ja) * 2010-10-20 2015-06-17 住友精密工業株式会社 航空機のステアリング装置の制御方法、並びに航空機のステアリング装置及びこれを備えた航空機
IL230099A (en) 2013-12-23 2017-09-28 Israel Aerospace Ind Ltd Monitoring the angle of contact between a leading vehicle and a driven aircraft
CN104085528B (zh) * 2014-07-10 2016-08-24 中国商用飞机有限责任公司 飞机前轮转弯控制系统和飞机前轮转弯控制方法
FR3028084B1 (fr) * 2014-11-03 2020-12-25 Sagem Defense Securite Procede et dispositif de guidage d'un aeronef
KR101745943B1 (ko) * 2014-12-17 2017-06-13 한국항공우주산업 주식회사 항공기용 전륜조향장치 선택 제어기 및 그 선택의 제어 방법
EP3178738A1 (en) * 2015-12-07 2017-06-14 Safran Landing Systems UK Limited Fully electric speed-proportional nose wheel steering system for an aircraft

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2814452A (en) 1950-10-26 1957-11-26 Bendix Aviat Corp Aircraft steering control system
US3067832A (en) 1960-12-16 1962-12-11 Dunlap And Associates Inc Velocity modulated steering system
US3885759A (en) 1973-06-21 1975-05-27 Lear Avia Corp Nose wheel steering system
US4011771A (en) 1975-10-16 1977-03-15 Mcdonnell Douglas Corporation Steering range selector
US6928363B2 (en) 2002-09-20 2005-08-09 The Boeing Company Autotiller control system for aircraft
US6722610B1 (en) 2002-11-25 2004-04-20 The Boeing Company Method, system, and computer program product for controlling maneuverable wheels on a vehicle
US6732979B1 (en) 2003-08-28 2004-05-11 The Boeing Company Steer-by-wire tiller with position feel system
GB2418185A (en) * 2004-08-03 2006-03-22 Joseph Zabrana Michael Ball and socket type landing gear for an airship
WO2007027588A1 (en) * 2005-08-29 2007-03-08 Borealis Technical Limited Nosewheel control apparatus
US7623044B2 (en) * 2006-04-06 2009-11-24 Honeywell International Inc. Runway and taxiway turning guidance
GB0702332D0 (en) 2007-02-07 2007-03-21 Airbus Uk Ltd A method, apparatus or software for controlling the heading of an aircraft on the ground
FR2941311B1 (fr) * 2009-01-16 2012-10-26 Messier Bugatti Procede de gestion de la commande d'orientation d'un atterrisseur d'aeronef

Also Published As

Publication number Publication date
US8473159B2 (en) 2013-06-25
ES2626703T3 (es) 2017-07-25
JP2014504223A (ja) 2014-02-20
JP5767713B2 (ja) 2015-08-19
EP2625578A2 (en) 2013-08-14
AU2011311970A1 (en) 2013-04-11
CN103562065A (zh) 2014-02-05
WO2012048139A3 (en) 2013-10-24
BR112013008383B1 (pt) 2020-12-22
US20120089277A1 (en) 2012-04-12
CA2813603C (en) 2016-02-23
AU2011311970B2 (en) 2014-10-30
MX2013003839A (es) 2013-09-13
EP2625578A4 (en) 2014-11-26
EP2625578B1 (en) 2017-05-17
CN103562065B (zh) 2015-11-25
WO2012048139A2 (en) 2012-04-12
CA2813603A1 (en) 2012-04-12

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 06/10/2011, OBSERVADAS AS CONDICOES LEGAIS.