SE518927C2 - Styrsystem för beräkning av styrkommandon till ställdon baserat på distribuerade datorer - Google Patents

Styrsystem för beräkning av styrkommandon till ställdon baserat på distribuerade datorer

Info

Publication number
SE518927C2
SE518927C2 SE0001910A SE0001910A SE518927C2 SE 518927 C2 SE518927 C2 SE 518927C2 SE 0001910 A SE0001910 A SE 0001910A SE 0001910 A SE0001910 A SE 0001910A SE 518927 C2 SE518927 C2 SE 518927C2
Authority
SE
Sweden
Prior art keywords
control
actuator
servo node
control system
commands
Prior art date
Application number
SE0001910A
Other languages
English (en)
Swedish (sv)
Other versions
SE0001910D0 (sv
SE0001910L (sv
Inventor
Rikard Johansson
Jan Torin
Kristina Ahlstroem
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
Priority to US10/296,159 priority Critical patent/US7017861B1/en
Application filed by Saab Ab filed Critical Saab Ab
Priority to SE0001910A priority patent/SE518927C2/sv
Publication of SE0001910D0 publication Critical patent/SE0001910D0/xx
Priority to AT01934764T priority patent/ATE279749T1/de
Priority to EP01934764A priority patent/EP1297426B1/de
Priority to BR0110766-6A priority patent/BR0110766A/pt
Priority to PCT/SE2001/001123 priority patent/WO2001093039A1/en
Priority to PL359134A priority patent/PL200659B1/pl
Priority to AU2001260916A priority patent/AU2001260916A1/en
Priority to RU2002134492/09A priority patent/RU2237276C1/ru
Priority to DE60106449T priority patent/DE60106449T2/de
Priority to ES01934764T priority patent/ES2230314T3/es
Publication of SE0001910L publication Critical patent/SE0001910L/xx
Priority to ZA200208581A priority patent/ZA200208581B/en
Publication of SE518927C2 publication Critical patent/SE518927C2/sv

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)
SE0001910A 2000-05-22 2000-05-22 Styrsystem för beräkning av styrkommandon till ställdon baserat på distribuerade datorer SE518927C2 (sv)

Priority Applications (12)

Application Number Priority Date Filing Date Title
US10/296,159 US7017861B1 (en) 2000-05-22 2000-05-18 Control system for actuators in an aircraft
SE0001910A SE518927C2 (sv) 2000-05-22 2000-05-22 Styrsystem för beräkning av styrkommandon till ställdon baserat på distribuerade datorer
ES01934764T ES2230314T3 (es) 2000-05-22 2001-05-18 Sistema de control para accionamientos en un avion.
PL359134A PL200659B1 (pl) 2000-05-22 2001-05-18 Układ do sterowania urządzeniami uruchamiającymi w samolocie
EP01934764A EP1297426B1 (de) 2000-05-22 2001-05-18 Steuersystem für betätigungsvorrichtungen in einem flugzeug
BR0110766-6A BR0110766A (pt) 2000-05-22 2001-05-18 Sistema de controle para atuadores em uma aeronave
PCT/SE2001/001123 WO2001093039A1 (en) 2000-05-22 2001-05-18 Control system for actuators in an aircraft
AT01934764T ATE279749T1 (de) 2000-05-22 2001-05-18 Steuersystem für betätigungsvorrichtungen in einem flugzeug
AU2001260916A AU2001260916A1 (en) 2000-05-22 2001-05-18 Control system for actuators in an aircraft
RU2002134492/09A RU2237276C1 (ru) 2000-05-22 2001-05-18 Система управления приводами в самолете
DE60106449T DE60106449T2 (de) 2000-05-22 2001-05-18 Steuersystem für betätigungsvorrichtungen in einem flugzeug
ZA200208581A ZA200208581B (en) 2000-05-22 2002-10-23 Control system for actuators in an aircraft.

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
SE0001910D0 SE0001910D0 (sv) 2000-05-22
SE0001910L SE0001910L (sv) 2001-11-23
SE518927C2 true SE518927C2 (sv) 2002-12-10

Family

ID=20279793

Family Applications (1)

Application Number Title Priority Date Filing Date
SE0001910A SE518927C2 (sv) 2000-05-22 2000-05-22 Styrsystem för beräkning av styrkommandon till ställdon baserat på distribuerade datorer

Country Status (12)

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

Families Citing this family (43)

* 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
US6883748B2 (en) 2001-06-04 2005-04-26 Rafi Yoeli Vehicles particularly useful as VTOL vehicles
WO2004031876A1 (en) * 2002-10-01 2004-04-15 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
RU2235042C1 (ru) * 2003-11-12 2004-08-27 Оао "Миэа" Способ управления самолетом
RU2235044C1 (ru) * 2003-11-12 2004-08-27 ОАО "ОКБ им. А.С. Яковлева" Легкий многоцелевой самолет
RU2235043C1 (ru) * 2003-11-12 2004-08-27 Оао "Миэа" Система управления самолетом
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
JP2008526599A (ja) 2005-01-10 2008-07-24 アーバン エアロノーティクス リミテッド ダクト内ファン垂直離着陸ビークル
US20100318245A1 (en) * 2005-03-03 2010-12-16 Nabtesco Corporation Flight control system
US7789345B2 (en) * 2005-03-03 2010-09-07 Nabtesco Corporation Actuator control apparatus
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
FR2899561B1 (fr) * 2006-04-11 2008-05-16 Airbus France Sas Procede et dispostif de pilotage d'un aeronef autour d'un axe de pilotage
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
EP1939703B1 (de) * 2006-12-28 2011-05-18 Saab Ab System, Computerprogrammprodukt und Verfahren zur Verstärkungsregelung in einem Steuerungssystem
ES2420110T3 (es) * 2007-01-08 2013-08-22 Saab Ab Un procedimiento, un sistema eléctrico, un módulo de control digital y un módulo de control de activador en un vehículo
WO2008135973A2 (en) 2007-05-02 2008-11-13 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
US8342441B2 (en) 2008-09-02 2013-01-01 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
CN117581474A (zh) 2021-06-30 2024-02-20 莱格特普莱特加拿大公司 利用本地智能的智能电机系统和方法
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 (17)

* 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 (de) 1982-06-16 1989-09-06 The Boeing Company Autopilotflugrichtungssystem
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 (de) * 1985-03-25 1990-04-25 British Aerospace Public Limited Company Steuerungssystem mit Rechner
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
KR970002667U (ko) * 1995-06-29 1997-01-24 접근신관의 작동시간 감시회로
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
RU2237276C1 (ru) 2004-09-27
PL200659B1 (pl) 2009-01-30
AU2001260916A1 (en) 2001-12-11
WO2001093039A1 (en) 2001-12-06
BR0110766A (pt) 2003-02-11
DE60106449D1 (de) 2004-11-18
DE60106449T2 (de) 2005-04-14
PL359134A1 (en) 2004-08-23
EP1297426A1 (de) 2003-04-02
ZA200208581B (en) 2003-10-23
EP1297426B1 (de) 2004-10-13
SE0001910D0 (sv) 2000-05-22
ES2230314T3 (es) 2005-05-01
ATE279749T1 (de) 2004-10-15
SE0001910L (sv) 2001-11-23
US7017861B1 (en) 2006-03-28

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