BRPI0709485A8 - Sistema de controle de vôo - Google Patents

Sistema de controle de vôo

Info

Publication number
BRPI0709485A8
BRPI0709485A8 BRPI0709485A BRPI0709485A BRPI0709485A8 BR PI0709485 A8 BRPI0709485 A8 BR PI0709485A8 BR PI0709485 A BRPI0709485 A BR PI0709485A BR PI0709485 A BRPI0709485 A BR PI0709485A BR PI0709485 A8 BRPI0709485 A8 BR PI0709485A8
Authority
BR
Brazil
Prior art keywords
control system
flight control
aircraft
flight
airspeed
Prior art date
Application number
BRPI0709485A
Other languages
English (en)
Inventor
Vitor Polati De Souza Álvaro
Gangsaas Dagfinn
Reis Caldeira Fabrício
Klein Jerome
Rocha Borges Lauro
Paulo Fonseca Marco
Luiz Andrioli Reneu Jr
Tury Pastorini Luciano
Original Assignee
Embraer Empresa Brasileira De Aeronautica S A
Embraer Sa
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 Embraer Empresa Brasileira De Aeronautica S A, Embraer Sa filed Critical Embraer Empresa Brasileira De Aeronautica S A
Publication of BRPI0709485A2 publication Critical patent/BRPI0709485A2/pt
Publication of BRPI0709485A8 publication Critical patent/BRPI0709485A8/pt
Publication of BRPI0709485B1 publication Critical patent/BRPI0709485B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • 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
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C19/00—Aircraft control not otherwise provided for
    • B64C19/02—Conjoint controls
    • 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
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • 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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • 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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft

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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Traffic Control Systems (AREA)

Abstract

SISTEMA DE CONTROLE DE VÔO Descreve-se um sistema de controle vôo que comanda dispositivos de arrasto tais como aerofólios de acordo com um comando longitudinal do piloto ou do piloto-automático. Além disso, o sistema de controle vôo monitora um conjunto de parâmetros de vôo (18 - 21) para determinar se a aeronave está operando dentro do envelope seguro permitido, conseqüentemente, incorporando desacionamento automático de envelopes excedentes. Esta invenção permite que a aeronave desça em um caminho de planagem mais íngreme do que os 3° usados na aproximação normal, enquanto mantém a velocidade inalterada.
BRPI0709485A 2006-12-11 2007-12-11 sistema de controle de vôo BRPI0709485B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB0624700.1 2006-12-11
GB0624700A GB2444742B (en) 2006-12-11 2006-12-11 Flight Control System
PCT/BR2007/000340 WO2008070944A2 (en) 2006-12-11 2007-12-11 Flight control system

Publications (3)

Publication Number Publication Date
BRPI0709485A2 BRPI0709485A2 (pt) 2011-07-19
BRPI0709485A8 true BRPI0709485A8 (pt) 2018-05-02
BRPI0709485B1 BRPI0709485B1 (pt) 2019-01-29

Family

ID=37711920

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0709485A BRPI0709485B1 (pt) 2006-12-11 2007-12-11 sistema de controle de vôo

Country Status (6)

Country Link
US (1) US9405295B2 (pt)
EP (1) EP2104886B1 (pt)
BR (1) BRPI0709485B1 (pt)
CA (1) CA2670918C (pt)
GB (1) GB2444742B (pt)
WO (1) WO2008070944A2 (pt)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2942612B1 (fr) 2009-03-02 2012-09-28 Airbus France Procede et dispositif d'optimisation automatique au sol de la configuration aerodynamique d'un avion
RU2443602C2 (ru) * 2009-11-26 2012-02-27 Московский государственный университет приборостроения и информатики Система автоматического управления самолетом по углу тангажа
FR2956512B1 (fr) * 2010-02-16 2012-03-09 Airbus Operations Sas Procede et dispositif de protection automatique d'un aeronef contre un taux de descente excessif.
US8666567B2 (en) 2011-03-31 2014-03-04 Honeywell International Inc. Systems and methods for controlling the speed of an aircraft
FR2980610B1 (fr) * 2011-09-23 2014-07-11 Airbus Operations Sas Procede et dispositif de prediction de la consommation de carburant sur un aeronef.
US8606437B2 (en) * 2011-11-28 2013-12-10 Embraer S.A. Flight control system mode and method providing aircraft speed control through the usage of momentary on-off control
US8781653B2 (en) * 2012-01-11 2014-07-15 The Boeing Company Quiet landing attitude modifier for airplane
US9153139B2 (en) 2012-12-21 2015-10-06 Embraer S.A. Steep approach performance improvements and optimization
JP6097596B2 (ja) * 2013-02-28 2017-03-15 三菱航空機株式会社 グランドスポイラの駆動システム、及び、航空機
FR3010696B1 (fr) * 2013-09-13 2015-10-09 Airbus Operations Sas Procede et systeme de commande de vol d'un aeronef.
US20150321748A1 (en) * 2014-05-08 2015-11-12 Honeywell International Inc. Speed brake alerting system and method
CN105094141A (zh) * 2014-05-20 2015-11-25 哈尔滨飞机工业集团有限责任公司 一种轻型固定翼飞机数字式自动驾驶仪系统
US9821903B2 (en) * 2014-07-14 2017-11-21 The Boeing Company Closed loop control of aircraft control surfaces
US10001776B2 (en) * 2016-03-21 2018-06-19 The Boeing Company Unmanned aerial vehicle flight control system
CN105955288B (zh) * 2016-07-15 2021-04-09 北京远度互联科技有限公司 飞行器定位及控制方法及系统
US10228692B2 (en) 2017-03-27 2019-03-12 Gulfstream Aerospace Corporation Aircraft flight envelope protection and recovery autopilot
CN110162064B (zh) * 2019-06-14 2024-07-19 湖南汽车工程职业学院 一种用于观光车的自动驾驶定位及控制系统
US11679865B2 (en) 2021-06-21 2023-06-20 Honeywell International Inc. Aircraft yoke interference detection system and method

Family Cites Families (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3040316A (en) * 1959-06-22 1962-06-19 Delaine C Sather Limiting circuit for an aircraft control system
US3252675A (en) * 1963-10-18 1966-05-24 Sperry Rand Corp Monitoring apparatus for aircraft control system
US3589648A (en) * 1969-01-02 1971-06-29 Lockheed Aircraft Corp Means for controlling the vertical path of an aircraft
US3870253A (en) * 1971-07-21 1975-03-11 Mc Donnell Douglas Corp Aircraft vectored flight control means
US3738594A (en) 1971-08-16 1973-06-12 Mc Donnell Douglas Corp Lift control mechanism
US3774869A (en) 1972-03-07 1973-11-27 K Harmon Combined throttle spoiler actuator for aircraft
US3850388A (en) 1972-03-23 1974-11-26 Nasa Integrated lift/drag controller for aircraft
US4106730A (en) * 1976-10-01 1978-08-15 The Boeing Company Engine out control system for STOL aircraft
US4261537A (en) * 1979-02-28 1981-04-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Velocity vector control system augmented with direct lift control
US4266743A (en) * 1979-02-28 1981-05-12 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Pitch attitude stabilization system utilizing engine pressure ratio feedback signals
US4363098A (en) * 1980-06-24 1982-12-07 The Boeing Company Electric command spoiler system
US4489907A (en) 1982-06-23 1984-12-25 Precise Flight, Inc. Selectively integrated throttle spoiler actuator for aircraft
US4849900A (en) * 1986-05-02 1989-07-18 The Boeing Company Flight control system and method
FR2661149B1 (fr) * 1990-04-24 1992-08-14 Aerospatiale Systeme pour le pilotage d'un avion en tangage.
US5337982A (en) * 1991-10-10 1994-08-16 Honeywell Inc. Apparatus and method for controlling the vertical profile of an aircraft
FR2719548B1 (fr) * 1994-05-03 1996-07-05 Aerospatiale Avion de transport à empennage avant.
US5826834A (en) * 1994-10-19 1998-10-27 Honeywell Inc. Self adaptive limiter for automatic control of approach and landing
US5823479A (en) * 1996-05-20 1998-10-20 The Boeing Company Landing attitude modifier for airplane
US6062513A (en) * 1998-09-14 2000-05-16 The Boeing Company Total energy based flight control system
US6246929B1 (en) * 1999-06-16 2001-06-12 Lockheed Martin Corporation Enhanced stall and recovery control system
DE10160315A1 (de) * 2001-12-07 2003-11-13 Airbus Gmbh Einrichtung zur Landeanflug-Steuerung eines Flugszeuges
US6885917B2 (en) * 2002-11-07 2005-04-26 The Boeing Company Enhanced flight control systems and methods for a jet powered tri-mode aircraft
FR2859174B1 (fr) * 2003-08-26 2006-03-10 Airbus France Procede et dispositif pour controler l'assiette d'un avion
EP1768899B1 (fr) * 2004-07-16 2013-12-11 Airbus Operations Procede et dispositif d'amelioration de la manoeuvrabilite d'un aeronef lors des phases d'approche avant l'atterrissage puis d'arrondi

Also Published As

Publication number Publication date
WO2008070944A2 (en) 2008-06-19
EP2104886A4 (en) 2013-07-24
EP2104886A2 (en) 2009-09-30
US9405295B2 (en) 2016-08-02
CA2670918A1 (en) 2008-06-19
GB0624700D0 (en) 2007-01-17
BRPI0709485B1 (pt) 2019-01-29
EP2104886B1 (en) 2017-11-22
CA2670918C (en) 2016-05-03
BRPI0709485A2 (pt) 2011-07-19
US20100217460A1 (en) 2010-08-26
GB2444742B (en) 2011-06-08
WO2008070944A3 (en) 2009-04-02
GB2444742A (en) 2008-06-18

Similar Documents

Publication Publication Date Title
BRPI0709485A8 (pt) Sistema de controle de vôo
JP6786294B2 (ja) 航空機失速保護システム
BRPI0802621A2 (pt) sistema de proteção contra estol, turbulência, baixa velocidade e elevada atitude
WO2008137217A3 (en) Vertical speed and flight path command algorithm for displacement collective utilizing tactile cueing and tactile feedback
BRPI0517266A (pt) sistema de controle de vÈo que tem um projeto de laço de controle triplo
WO2008108787A3 (en) Surface contact override landing scheme for a fbw rotary-wing aircraft
BR112013004540A2 (pt) sistema de elevador para alocar pelo menos um elevador em serviço em resposta a cada chamada de cabine comandada, meio legível por computador, e, método
BR112018074141A2 (pt) sistemas de controle de veículo autônomo dinâmico em cabine
BR112016018702A2 (pt) Método para prever uma falha em um sistema de controle de temperatura de cabine
BR102013016640A2 (pt) sistema de controle de voo, meio de armazenamento legível por computador não transitório e aeronave
BR112018077386A2 (pt) sistemas e métodos de engrenagens de pouso inclinado
WO2016053944A3 (en) Main rotor rotational speed control for rotorcraft
BR112014008198A2 (pt) válvula de controle sanguíneo de múltiplo uso contendo frestas circunferênciais
BR112014015107A2 (pt) elevador aéreo com dispositivo de segurança e alarme
ATE496666T1 (de) System zur steuerung einer flugrichtung
GB2396706A (en) Airplane emergency navigational system
BR112018000764A2 (pt) normalização de controle para sistemas autônomos não-tripulados
BR112018009344A2 (pt) veículo aéreo com componentes desdobráveis
BR112017027819A2 (pt) controle de um dispositivo de iot usando um dispositivo de controle remoto via um dispositivo de proxy de controle remoto
BRPI0702323A (pt) sistema de iluminação de uma cabine de elevador e método para orientar os passageiros de um elevador
BR102017022759A8 (pt) Sistema de controle de auto-brake e aeronave
PL2166372T3 (pl) Interfejs do komunikacji człowieka z maszyną do wspierania pilota podczas startu lub lądowania urządzenia latającego przy ograniczonej widoczności
WO2009023340A3 (en) Autodrag function for glide slope control
BRPI0516143A (pt) sistema de controle automático de velocidade para aeronave
DE50115848D1 (de) Flugkontrollsystem

Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: EMBRAER S.A. (BR/SP)

B06A Patent application procedure suspended [chapter 6.1 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: 10 (DEZ) ANOS CONTADOS A PARTIR DE 29/01/2019, OBSERVADAS AS CONDICOES LEGAIS.