BR112012015965A2 - sistema de controle de aeronave, método para controlar aeronave e aeronave - Google Patents

sistema de controle de aeronave, método para controlar aeronave e aeronave

Info

Publication number
BR112012015965A2
BR112012015965A2 BR112012015965-8A BR112012015965A BR112012015965A2 BR 112012015965 A2 BR112012015965 A2 BR 112012015965A2 BR 112012015965 A BR112012015965 A BR 112012015965A BR 112012015965 A2 BR112012015965 A2 BR 112012015965A2
Authority
BR
Brazil
Prior art keywords
aircraft
control
propulsion
control signal
control system
Prior art date
Application number
BR112012015965-8A
Other languages
English (en)
Japanese (ja)
Inventor
Yamasaki Koicho
Original Assignee
Mitsubishi Heavy Industries, Ltd
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 Mitsubishi Heavy Industries, Ltd filed Critical Mitsubishi Heavy Industries, Ltd
Publication of BR112012015965A2 publication Critical patent/BR112012015965A2/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control; Arrangement thereof
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically

Abstract

sistema de controle de aeronave, método para controlar aeronave e aeronave o voo estável pode ser alcançado sem a necssidade por uma operação de acelerador complicada por um piloto mesmo quando parte ou todas as superfícies de controle funcionam com defeito. um meio de computação (15) calcula um sinal de controle de propulsão para controlar propulsão de motor e um sinal de controle de ângulo de deflexão para controlar superfícies de controle com base em informações de estado relacionados a uma estrutura de avião e um sinal de comando de operação de uma extremidade de operação. um meio de acionamento de motor (17) aciona um motor com base de sinal de controle de propulsão. um meio de movimentação de superfície de controle (16) move a superfície de controle de base no sinal de controle de ângulo de deflexão.
BR112012015965-8A 2010-02-26 2011-02-25 sistema de controle de aeronave, método para controlar aeronave e aeronave BR112012015965A2 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
JP2010-043521 2010-02-26
JP2010043521A JP5123964B2 (ja) 2010-02-26 2010-02-26 航空機の制御システム、航空機の制御方法、及び航空機
PCT/JP2011/054253 WO2011105536A1 (ja) 2010-02-26 2011-02-25 航空機の制御システム、航空機の制御方法、及び航空機

Publications (1)

Publication Number Publication Date
BR112012015965A2 true BR112012015965A2 (pt) 2018-05-29

Family

ID=44506933

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012015965-8A BR112012015965A2 (pt) 2010-02-26 2011-02-25 sistema de controle de aeronave, método para controlar aeronave e aeronave

Country Status (8)

Country Link
US (1) US9045220B2 (pt)
EP (1) EP2540621B1 (pt)
JP (1) JP5123964B2 (pt)
CN (1) CN102695649B (pt)
BR (1) BR112012015965A2 (pt)
CA (1) CA2785692C (pt)
RU (1) RU2537883C2 (pt)
WO (1) WO2011105536A1 (pt)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2970702B1 (fr) * 2011-01-26 2013-05-10 Astrium Sas Procede et systeme de pilotage d'un engin volant a propulseur arriere
JP5812633B2 (ja) * 2011-03-14 2015-11-17 三菱重工業株式会社 航空機の制御システム、航空機、航空機の制御プログラム、及び航空機の制御方法
CN103057712B (zh) * 2012-12-31 2015-06-17 北京航空航天大学 微小型飞行机器人集成飞行控制系统
CN103324202A (zh) * 2013-07-12 2013-09-25 无锡华航电子科技有限责任公司 基于舵面故障的容错飞行控制系统和方法
CN104477376B (zh) * 2014-12-23 2016-08-24 北京航空航天大学 一种高超声速飞行器气动舵/反作用控制系统复合气动控制方法
RU171721U1 (ru) * 2016-03-30 2017-06-13 Общество с ограниченной ответственностью "Научно-инженерная компания "Объектные системы автоматики" (ООО "НИК "ОСА") Система управления основными летными функциями самолета с помощью рулевых поверхностей с электромеханическими приводами
RU2622321C1 (ru) * 2016-03-30 2017-06-14 Общество с ограниченной ответственностью "Научно-инженерная компания "Объектные системы автоматики" (ООО "НИК "ОСА") Система рулевых поверхностей с электромеханическими приводами для управления основными летными функциями самолета
RU171693U1 (ru) * 2016-03-30 2017-06-13 Общество с ограниченной ответственностью "Научно-инженерная компания "Объектные системы автоматики" (ООО "НИК "ОСА") Система управления основными летными функциями самолета
US10604236B2 (en) 2016-06-01 2020-03-31 Regents Of The University Of Minnesota Fault-tolerant aircraft flight control using a subset of aerodynamic control surfaces
US10005561B2 (en) * 2016-06-16 2018-06-26 Ge Aviation Systems Llc Controlling aircraft using thrust differential trim
RU2630030C1 (ru) * 2016-10-28 2017-09-05 Публичное акционерное общество "Авиационная холдинговая компания "Сухой" Многофункциональный одноместный самолет с комплексной системой управления
US10059432B1 (en) 2017-02-22 2018-08-28 Pratt & Whitney Canada Corp. Single lever control in twin turbopropeller aircraft
US10793260B1 (en) * 2017-10-30 2020-10-06 The Boeing Company Methods and systems for controlling aircraft flight performance
US11111814B2 (en) 2017-12-20 2021-09-07 General Electric Company Turbine engine operational testing
US20190283862A1 (en) * 2018-03-16 2019-09-19 Honeywell International Inc. Flight control system
US10775784B2 (en) * 2018-06-14 2020-09-15 Wing Aviation Llc Unmanned aerial vehicle with decentralized control system
RU2689054C1 (ru) * 2018-08-30 2019-05-23 Публичное акционерное общество "Московский институт электромеханики и автоматики" (ПАО "МИЭА") Способ управления скоростью полёта самолёта с учетом стабилизации скорости
CN112373704A (zh) * 2020-11-17 2021-02-19 中国商用飞机有限责任公司 通过控制发动机推力来实现飞机的应急控制的系统及飞机

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3003231C2 (de) * 1980-01-30 1984-01-05 Dornier Gmbh, 7990 Friedrichshafen Steuereinrichtung für durch Strahlreaktion angetriebene Flugkörper, Raketen o.dgl.
US4536843A (en) * 1982-09-30 1985-08-20 The Boeing Company Total energy based flight control system
US4787201A (en) * 1985-03-25 1988-11-29 General Electric Company Method and apparatus for controlling multiple engine aircraft
FR2668750B1 (fr) * 1990-11-06 1993-01-22 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
JPH0597095A (ja) * 1991-10-09 1993-04-20 Mitsubishi Heavy Ind Ltd 航空機用非常操舵システム
US5337982A (en) * 1991-10-10 1994-08-16 Honeywell Inc. Apparatus and method for controlling the vertical profile of an aircraft
US5330131A (en) 1992-05-28 1994-07-19 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Engines-only flight control system
JPH08183497A (ja) * 1994-12-30 1996-07-16 Kawasaki Heavy Ind Ltd 飛行体の制御方法および制御装置
CN1230721C (zh) 1996-08-22 2005-12-07 波音公司 飞机俯仰增稳和指令增控系统
US6041273A (en) 1997-07-01 2000-03-21 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Emergency control aircraft system using thrust modulation
US6102330A (en) 1997-07-29 2000-08-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Emergency multiengine aircraft system for lateral control using differential thrust control of wing engines
RU2122511C1 (ru) * 1998-06-22 1998-11-27 Акционерное общество открытого типа "ОКБ Сухого" Управление самолетом посредством управления вектором тяги
US7017861B1 (en) * 2000-05-22 2006-03-28 Saab Ab Control system for actuators in an aircraft
RU2194886C2 (ru) * 2000-06-14 2002-12-20 Открытое акционерное общество "Павловский машиностроительный завод "Восход" Комбинированный привод
US6622972B2 (en) 2001-10-31 2003-09-23 The Boeing Company Method and system for in-flight fault monitoring of flight control actuators
JP3637326B2 (ja) * 2002-04-03 2005-04-13 三菱重工業株式会社 制御システム、航空機・宇宙機の飛行制御システム、車両の運動制御システム
FR2854962B1 (fr) * 2003-05-14 2005-08-05 Airbus France Procede et dispositif de pilotage d'un aeronef
RU2235043C1 (ru) * 2003-11-12 2004-08-27 Оао "Миэа" Система управления самолетом
FR2874204B1 (fr) * 2004-08-13 2007-12-14 Airbus France Sas Systeme de commande de vol electriques pour les gouvernes de profondeur d'un aeronef
US8016243B2 (en) 2006-10-12 2011-09-13 The Boeing Company Aircraft backup control

Also Published As

Publication number Publication date
JP2011178248A (ja) 2011-09-15
RU2537883C2 (ru) 2015-01-10
CN102695649A (zh) 2012-09-26
CA2785692A1 (en) 2011-09-01
US9045220B2 (en) 2015-06-02
EP2540621A4 (en) 2018-01-17
JP5123964B2 (ja) 2013-01-23
WO2011105536A1 (ja) 2011-09-01
RU2012125844A (ru) 2013-12-27
US20120298806A1 (en) 2012-11-29
EP2540621A1 (en) 2013-01-02
EP2540621B1 (en) 2020-03-18
CA2785692C (en) 2015-01-06
CN102695649B (zh) 2015-06-17

Similar Documents

Publication Publication Date Title
BR112012015965A2 (pt) sistema de controle de aeronave, método para controlar aeronave e aeronave
GB201108450D0 (en) Aircraft wing assembly
BR112013021765A2 (pt) sistema de controle de aeronave, aeronave, programa de controle de aeronave e método para o controle de aeronave
WO2008137217A3 (en) Vertical speed and flight path command algorithm for displacement collective utilizing tactile cueing and tactile feedback
US10967953B2 (en) Combined active stick and control boost actuator system
BR112013022291A2 (pt) método de operar de maneira simultânea atuadores para movimentar flaps de aeronave, um dispositivo de acionamento de flap de aeronave e uma aeronave dotada de tal dispositivo
BR112016006370A2 (pt) método para controlar a operação de um mecanismo motor de turbopropulsor de aeronave e sistema de controle de turbopropulsor
NO20070810A (no) System for å kontrollere flygeretning
DE602007009203D1 (de) Multimodale bemannte und unbemannte fahrzeugsysteme und -verfahren
ATE510768T1 (de) Schneller weitbereichs-hybridhelikopter mit längshaltungssteuerung
RU2011146418A (ru) Система увеличения подъемной силы самолета, самолетная система и винтовой самолет с системой увеличения подъемной силы
BR112012024094A2 (pt) sistema de controle do tipo hidráulico para um dispositivo de reversão de empuxo e nacela
MX2020011021A (es) Sistemas y métodos para aterrizaje y despegue vertical usando levitación magnética.
US20070235594A1 (en) Pilot flight control stick feedback system
FR2898584B1 (fr) Procede et dispositif de commande de la poussee d'un aeronef multimoteur
WO2009023340A3 (en) Autodrag function for glide slope control
RU2011101565A (ru) Система управления летательным аппаратом
EP2599712A3 (en) Aerodynamic wing load distribution control
BR112017020041A2 (pt) sistema de controle para controle de acionamento de motor elétrico submersível
Walker et al. F-35B integrated flight-propulsion control development
GB201317925D0 (en) Actuator control system
GB201206333D0 (en) Process for guiding the flight of an aircraft to a predetermined target object, and flight-guidance system
ITTO20130489A1 (it) Metodo per il controllo automatico dell'asse di imbardata per un aeromobile con comandi di volo meccanici.
BRPI0604440A (pt) configuração aplicada em sistema para controle da autoridade do leme de uma aeronave
CN103921959A (zh) 星上二维指向系统构型设计方法

Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according art. 34 industrial property law
B06U Preliminary requirement: requests with searches performed by other patent offices: suspension of the patent application procedure
B06A Notification to applicant to reply to the report for non-patentability or inadequacy of the application according art. 36 industrial patent law
B11B Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements