BR0110766A - Sistema de controle para atuadores em uma aeronave - Google Patents

Sistema de controle para atuadores em uma aeronave

Info

Publication number
BR0110766A
BR0110766A BR0110766-6A BR0110766A BR0110766A BR 0110766 A BR0110766 A BR 0110766A BR 0110766 A BR0110766 A BR 0110766A BR 0110766 A BR0110766 A BR 0110766A
Authority
BR
Brazil
Prior art keywords
actuator
control commands
servo node
control
computer
Prior art date
Application number
BR0110766-6A
Other languages
English (en)
Inventor
Rikard Johansson
Jantorin
Kristina Ahlstrom
Original Assignee
Saab Ab
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 Saab Ab filed Critical Saab Ab
Publication of BR0110766A publication Critical patent/BR0110766A/pt

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B9/00—Safety arrangements
    • G05B9/02—Safety arrangements electric
    • G05B9/03—Safety arrangements electric with multiple-channel loop, i.e. redundant control systems

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Safety Devices In Control Systems (AREA)
  • Feedback Control In General (AREA)
  • Retarders (AREA)
  • Control Of Electric Motors In General (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Servomotors (AREA)

Abstract

"SISTEMA DE CONTROLE PARA ATUADORES EM UMA AERONAVE". A presente invenção se refere a um sistema de controle para calcular comandos de controle para atuadores em uma aeronave, em que os comandos de controle são calculados por computadores distribuídos na aeronave, na dependência de sinais de entrada contendo parâmetros que servem como base para os ditos comandos, em que um computador (C) é disposto em cada respectivo atuador local (A) e junto com o atuador (A) forma um nó servo (S), onde o computador (C) recebe sinais de entrada através de um barramento de dados (B), pelo que o computador (C) em cada nó servo (S) calcula comandos de controle para o atuador local (A), baseado em um ou mais conjuntos de leis de controle, na dependência de parâmetros recebidos e em que o computador (C) calcula, de uma maneira correspondente, comandos de controle para pelo menos um atuador adicional (A) em outro nó servo (S) e em que uma escolha dos comandos de controle é usada como comando de controle (7) para o atuador (A) localmente no nó servo (S), na dependência de uma comparação entre os comandos de controle (4), calculados localmente no nó servo (S) e um comando de controle (3) calculado para o atuador (A) em pelo menos outro nó servo (S) para o atuador (A).
BR0110766-6A 2000-05-22 2001-05-18 Sistema de controle para atuadores em uma aeronave BR0110766A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
SE0001910A SE518927C2 (sv) 2000-05-22 2000-05-22 Styrsystem för beräkning av styrkommandon till ställdon baserat på distribuerade datorer
PCT/SE2001/001123 WO2001093039A1 (en) 2000-05-22 2001-05-18 Control system for actuators in an aircraft

Publications (1)

Publication Number Publication Date
BR0110766A true BR0110766A (pt) 2003-02-11

Family

ID=20279793

Family Applications (1)

Application Number Title Priority Date Filing Date
BR0110766-6A BR0110766A (pt) 2000-05-22 2001-05-18 Sistema de controle para atuadores em uma aeronave

Country Status (12)

Country Link
US (1) US7017861B1 (pt)
EP (1) EP1297426B1 (pt)
AT (1) ATE279749T1 (pt)
AU (1) AU2001260916A1 (pt)
BR (1) BR0110766A (pt)
DE (1) DE60106449T2 (pt)
ES (1) ES2230314T3 (pt)
PL (1) PL200659B1 (pt)
RU (1) RU2237276C1 (pt)
SE (1) SE518927C2 (pt)
WO (1) WO2001093039A1 (pt)
ZA (1) ZA200208581B (pt)

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6464166B1 (en) 2001-05-29 2002-10-15 Romeo Yankee Ltd. Ducted fan vehicles particularly useful as VTOL aircraft
US7275712B2 (en) 2002-05-28 2007-10-02 Urban Aeronautics, Ltd. Ducted fan vehicles particularly useful as VTOL aircraft
WO2002098732A2 (en) 2001-06-04 2002-12-12 Romeo Yankee Ltd. Vehicles particularly useful as vtol vehicles
AU2003269439A1 (en) * 2002-10-01 2004-04-23 Urban Aeronautics Ltd. Flight control system for vtol aircraft
US7209809B2 (en) * 2003-10-15 2007-04-24 The Boeing Company Method and apparatus for obtaining high integrity and availability in multi-channel systems
US7857253B2 (en) 2003-10-27 2010-12-28 Urban Aeronautics Ltd. Ducted fan VTOL vehicles
US8984500B2 (en) * 2004-06-14 2015-03-17 Hewlett-Packard Development Company, L.P. Programming a computing node connected to a sensor and an actuator
US8942882B2 (en) * 2004-07-02 2015-01-27 The Boeing Company Vehicle health management systems and methods
WO2006072960A2 (en) 2005-01-10 2006-07-13 Urban Aeronautics Ltd. Ducted fan vtol vehicles
US7789345B2 (en) * 2005-03-03 2010-09-07 Nabtesco Corporation Actuator control apparatus
US20100318245A1 (en) * 2005-03-03 2010-12-16 Nabtesco Corporation Flight control system
US7946528B2 (en) 2005-04-15 2011-05-24 Urban Aeronautics, Ltd. Flight control system especially suited for VTOL vehicles
US7717368B2 (en) 2005-06-07 2010-05-18 Urban Aeronautics Ltd. Apparatus for generating horizontal forces in aerial vehicles and related method
US8020804B2 (en) 2006-03-01 2011-09-20 Urban Aeronautics, Ltd. Ground effect vanes arrangement
US8833692B2 (en) 2006-11-27 2014-09-16 Urban Aeronautics Ltd. Wall effects on VTOL vehicles
GB0624090D0 (en) * 2006-12-01 2007-01-10 Selamine Ltd Ramipril amine salts
ES2363370T3 (es) * 2006-12-28 2011-08-02 Saab Ab Sistema, producto de programa de ordenador y procedimiento para ajustar la ganancia en un sistema de control.
EP1942054B1 (en) * 2007-01-08 2013-05-29 Saab Ab A method, an electrical system, a digital control module, and an actuator control module in a vehicle
US8496200B2 (en) 2007-05-02 2013-07-30 Urban Aeronautics Ltd. Control flows and forces in VTOL vehicles
US8948960B2 (en) * 2007-11-30 2015-02-03 Honeywell International Inc. Systems and methods for arbitrating sensor and actuator signals in a multi-channel control system
US7840316B2 (en) * 2007-12-17 2010-11-23 Honeywell International Inc. Limited authority and full authority mode fly-by-wire flight control surface actuation control system
EP2318273A4 (en) 2008-09-02 2017-09-06 Urban Aeronautics Ltd. Vtol vehicle with coaxially tilted or tiltable rotors
US8070091B2 (en) * 2008-10-08 2011-12-06 Honeywell International Inc. Electromechanical actuation system and method
DE102009017653A1 (de) * 2009-04-16 2010-10-21 Airbus Deutschland Gmbh Hochauftriebssystem eines Flugzeugs, Flugzeugsystem und Propeller-Flugzeug mit einem Hochauftriebssystem
DE102009022602A1 (de) * 2009-05-26 2010-12-02 Airbus Deutschland Gmbh Flugzeug mit einem Hochauftriebssystem
JP5123964B2 (ja) 2010-02-26 2013-01-23 三菱重工業株式会社 航空機の制御システム、航空機の制御方法、及び航空機
US20110251739A1 (en) * 2010-04-09 2011-10-13 Honeywell International Inc. Distributed fly-by-wire system
FR2960680B1 (fr) * 2010-05-28 2013-05-17 Airbus Operations Sas Systeme embarque a bord d'un aeronef
US8876038B2 (en) 2010-10-05 2014-11-04 Urban Aeronautics Ltd. Ducted fan for VTOL vehicles with system and method to reduce roll moments
US8534599B2 (en) * 2011-03-31 2013-09-17 Hamilton Sundstrand Corporation Redundant two stage electro-hydraulic servo actuator control
DE102011115362A1 (de) * 2011-10-07 2013-04-11 Liebherr-Aerospace Lindenberg Gmbh Modulares elektronisches Flugsteuerungssystem
FR2992122B1 (fr) * 2012-06-15 2014-06-27 Thales Sa Dispositif de conversion securise de commandes numeriques en signaux analogiques de puissance pour aeronef
RU2681509C1 (ru) * 2017-11-08 2019-03-06 Российская Федерация в лице Министерства промышленности и торговли Российской Федерации (Минпромторг России) Способ управления рулём высоты самолёта
US11203440B2 (en) * 2018-01-04 2021-12-21 Hamilton Sundstrand Corporation System for integrated engine and flight control
US10843792B2 (en) * 2018-02-01 2020-11-24 Hamilton Sundstrand Corporation Autonomous reconfiguration of a multi-redundant actuator control system
US11243098B2 (en) 2019-02-08 2022-02-08 Simmonds Precision Products, Inc. Configurable nodes for sensing systems
US10938643B2 (en) 2019-02-08 2021-03-02 Simmonds Precision Products, Inc. Distributed sensing systems and nodes therefor
KR20240012583A (ko) 2021-06-30 2024-01-29 레겟 앤드 플랫 캐나다 코포레이션 로컬 지능을 이용한 스마트 모터 시스템들 및 방법들
RU2764322C1 (ru) * 2021-09-14 2022-01-17 Федеральное государственное автономное образовательное учреждение высшего образования «Санкт-Петербургский государственный университет аэрокосмического приборостроения» Способ минимизации средней высоты полета летательного аппарата, движущегося вблизи неровной поверхности, и устройство для его осуществления

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4412281A (en) 1980-07-11 1983-10-25 Raytheon Company Distributed signal processing system
US4327437A (en) * 1980-07-30 1982-04-27 Nasa Reconfiguring redundancy management
EP0110885B1 (en) * 1982-06-16 1989-09-06 The Boeing Company Autopilot flight director system
US4622667A (en) 1984-11-27 1986-11-11 Sperry Corporation Digital fail operational automatic flight control system utilizing redundant dissimilar data processing
US4672530A (en) 1984-12-17 1987-06-09 Combustion Engineering, Inc. Distributed control with universal program
EP0200352A3 (en) * 1985-03-25 1990-04-25 British Aerospace Public Limited Company Computer control system
DE3621106C2 (de) 1986-06-24 1995-03-23 Vdo Schindling Verfahren zur ON-LINE-Verarbeitung gleicher Eingabegrößen mittels zweier Prozessoren
DE3638820A1 (de) * 1986-09-12 1988-03-24 Messerschmitt Boelkow Blohm Seitenruder-steuerungsanordnung fuer luftfahrzeuge
FR2628858B1 (fr) 1988-03-15 1990-08-17 Aerospatiale Systeme de commande de vol pour aeronef
DE3906846C2 (de) 1989-03-03 1994-02-17 Bodenseewerk Geraetetech Redundante Rechneranordnung für Steuersysteme
US5493497A (en) * 1992-06-03 1996-02-20 The Boeing Company Multiaxis redundant fly-by-wire primary flight control system
US5377109A (en) * 1992-07-31 1994-12-27 Lear Astronics Corp. Failsafe digital bus to analog protocol converter system
JPH07262148A (ja) 1994-03-22 1995-10-13 Nec Corp コンピュータシステム
US5515282A (en) * 1994-04-25 1996-05-07 The Boeing Company Method and apparatus for implementing a databus voter to select flight command signals from one of several redundant asynchronous digital primary flight computers
US6206329B1 (en) * 1995-09-15 2001-03-27 Jean-Pierre Gautier Process and device for the control of the rudder of an aircraft
DE19835191C1 (de) 1998-08-04 2000-04-20 Daimler Chrysler Ag Flugsteuerungseinrichtung zur Verbesserung der Längsstabilität eines geregelten Flugzeugs

Also Published As

Publication number Publication date
ES2230314T3 (es) 2005-05-01
SE518927C2 (sv) 2002-12-10
RU2237276C1 (ru) 2004-09-27
EP1297426A1 (en) 2003-04-02
US7017861B1 (en) 2006-03-28
AU2001260916A1 (en) 2001-12-11
ATE279749T1 (de) 2004-10-15
DE60106449D1 (de) 2004-11-18
DE60106449T2 (de) 2005-04-14
PL200659B1 (pl) 2009-01-30
SE0001910L (sv) 2001-11-23
WO2001093039A1 (en) 2001-12-06
PL359134A1 (en) 2004-08-23
ZA200208581B (en) 2003-10-23
EP1297426B1 (en) 2004-10-13
SE0001910D0 (sv) 2000-05-22

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B07A Application suspended after technical examination (opinion) [chapter 7.1 patent gazette]
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