PL359134A1 - System sterowania urządzeniami uruchamiającymi w samolocie - Google Patents

System sterowania urządzeniami uruchamiającymi w samolocie

Info

Publication number
PL359134A1
PL359134A1 PL01359134A PL35913401A PL359134A1 PL 359134 A1 PL359134 A1 PL 359134A1 PL 01359134 A PL01359134 A PL 01359134A PL 35913401 A PL35913401 A PL 35913401A PL 359134 A1 PL359134 A1 PL 359134A1
Authority
PL
Poland
Prior art keywords
actuator
control commands
servo node
control
computer
Prior art date
Application number
PL01359134A
Other languages
English (en)
Other versions
PL200659B1 (pl
Inventor
Rikard Johansson
Jan Torin
Kristina Ahlström
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 PL359134A1 publication Critical patent/PL359134A1/pl
Publication of PL200659B1 publication Critical patent/PL200659B1/pl

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)
PL359134A 2000-05-22 2001-05-18 Układ do sterowania urządzeniami uruchamiającymi w samolocie PL200659B1 (pl)

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 (2)

Publication Number Publication Date
PL359134A1 true PL359134A1 (pl) 2004-08-23
PL200659B1 PL200659B1 (pl) 2009-01-30

Family

ID=20279793

Family Applications (1)

Application Number Title Priority Date Filing Date
PL359134A PL200659B1 (pl) 2000-05-22 2001-05-18 Układ do sterowania urządzeniami uruchamiającymi w samolocie

Country Status (12)

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

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 (en) * 2006-12-28 2011-05-18 Saab Ab System, computer program product and method for adjusting gain in a control system
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 (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
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
SE518927C2 (sv) 2002-12-10
BR0110766A (pt) 2003-02-11
DE60106449D1 (de) 2004-11-18
DE60106449T2 (de) 2005-04-14
EP1297426A1 (en) 2003-04-02
ZA200208581B (en) 2003-10-23
EP1297426B1 (en) 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

Similar Documents

Publication Publication Date Title
AU2001260916A1 (en) Control system for actuators in an aircraft
CA2358416A1 (en) Process facility control systems using an efficient prediction form and methods of operating the same
WO2004097557A3 (en) Distributed control systems and methods
GB2597346A8 (en) Control architectures for autonomous vehicles
WO2003023322A3 (en) Airplane emergency navigational system
EP1315055A3 (en) System and method for function block execution order generation
GB2398203B (en) Dynamic rdf groups
JPS5890203A (ja) サ−ボ系
WO1997046929A3 (en) 3-brain architecture for an intelligent decision and control system
WO2001033760A8 (en) Hybrid control of haptic feedback for host computer and interface device
CA2339687A1 (en) Three-dimensional cad system and recording medium for three-dimensional cad system
EP1324183A3 (en) System and method for intermediating communication with a moveable media library utilizing a plurality of partitions
WO2002079972A3 (de) Verfahren zum betrieb eines verteilten computersystems
WO2022123268A3 (en) Improvements in or relating to quantum computing systems and methods
DE60111303T2 (de) Flugzeug mit elektrischer Flugsteuerung, versehen mit einem Autopilotsystem
WO2007066271A3 (en) Resource control
AU4905197A (en) General purpose distributed operating room control system
CA2064162A1 (en) Personal computer with local bus arbitration
Leland et al. Reliable H/sub/spl infin//norm bounding controllers with redundant control elements
KR950004022A (ko) 분산처리통합 관리시스템
EP0055078B1 (en) Blended mode concept for control of flight simulator motion systems
US4773000A (en) DMA for digital computer system
JP2006327299A (ja) 操縦システム
JPH11308258A (ja) 端末の電源制御方式
Tischler et al. Comparison of flight control system design methods using the CONDUIT [registered trademark] design tool