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)

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US7857253B2 (en) 2003-10-27 2010-12-28 Urban Aeronautics Ltd. Ducted fan VTOL vehicles
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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
BRPI0708425A2 (pt) 2006-03-01 2011-05-31 Urban Aeronautics Ltd disposição de palhetas em efeito solo
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
WO2008065654A2 (en) 2006-11-27 2008-06-05 Urban Aeronautics Ltd. Wall effects on vtol vehicles
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ATE510249T1 (de) * 2006-12-28 2011-06-15 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
EP2152576A2 (en) 2007-05-02 2010-02-17 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
WO2010026517A2 (en) 2008-09-02 2010-03-11 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
US10938643B2 (en) 2019-02-08 2021-03-02 Simmonds Precision Products, Inc. Distributed sensing systems and nodes therefor
US11243098B2 (en) 2019-02-08 2022-02-08 Simmonds Precision Products, Inc. Configurable nodes for sensing systems
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

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Also Published As

Publication number Publication date
AU2001260916A1 (en) 2001-12-11
SE518927C2 (sv) 2002-12-10
SE0001910L (sv) 2001-11-23
US7017861B1 (en) 2006-03-28
PL200659B1 (pl) 2009-01-30
RU2237276C1 (ru) 2004-09-27
WO2001093039A1 (en) 2001-12-06
ATE279749T1 (de) 2004-10-15
EP1297426A1 (en) 2003-04-02
BR0110766A (pt) 2003-02-11
DE60106449D1 (de) 2004-11-18
DE60106449T2 (de) 2005-04-14
ZA200208581B (en) 2003-10-23
ES2230314T3 (es) 2005-05-01
EP1297426B1 (en) 2004-10-13
SE0001910D0 (sv) 2000-05-22

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