PL359134A1 - System sterowania urządzeniami uruchamiającymi w samolocie - Google Patents
System sterowania urządzeniami uruchamiającymi w samolocieInfo
- 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
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)
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 (39)
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 |
CA2605111A1 (en) | 2005-01-10 | 2006-07-13 | Raphael Yoeli | 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 |
WO2007099543A2 (en) | 2006-03-01 | 2007-09-07 | Urban Aeronautics Ltd. | Ground effect vanes arrangement |
WO2008065654A2 (en) | 2006-11-27 | 2008-06-05 | 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 |
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 |
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)
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 |
WO1984000071A1 (en) | 1982-06-16 | 1984-01-05 | Boeing Co | 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 |
-
2000
- 2000-05-18 US US10/296,159 patent/US7017861B1/en not_active Expired - Fee Related
- 2000-05-22 SE SE0001910A patent/SE518927C2/sv unknown
-
2001
- 2001-05-18 AU AU2001260916A patent/AU2001260916A1/en not_active Abandoned
- 2001-05-18 RU RU2002134492/09A patent/RU2237276C1/ru not_active IP Right Cessation
- 2001-05-18 ES ES01934764T patent/ES2230314T3/es not_active Expired - Lifetime
- 2001-05-18 AT AT01934764T patent/ATE279749T1/de not_active IP Right Cessation
- 2001-05-18 PL PL359134A patent/PL200659B1/pl unknown
- 2001-05-18 WO PCT/SE2001/001123 patent/WO2001093039A1/en active IP Right Grant
- 2001-05-18 BR BR0110766-6A patent/BR0110766A/pt not_active Application Discontinuation
- 2001-05-18 EP EP01934764A patent/EP1297426B1/en not_active Expired - Lifetime
- 2001-05-18 DE DE60106449T patent/DE60106449T2/de not_active Expired - Lifetime
-
2002
- 2002-10-23 ZA ZA200208581A patent/ZA200208581B/en unknown
Also Published As
Publication number | Publication date |
---|---|
PL200659B1 (pl) | 2009-01-30 |
ZA200208581B (en) | 2003-10-23 |
SE518927C2 (sv) | 2002-12-10 |
ATE279749T1 (de) | 2004-10-15 |
DE60106449D1 (de) | 2004-11-18 |
DE60106449T2 (de) | 2005-04-14 |
EP1297426B1 (en) | 2004-10-13 |
SE0001910L (sv) | 2001-11-23 |
EP1297426A1 (en) | 2003-04-02 |
BR0110766A (pt) | 2003-02-11 |
RU2237276C1 (ru) | 2004-09-27 |
SE0001910D0 (sv) | 2000-05-22 |
WO2001093039A1 (en) | 2001-12-06 |
AU2001260916A1 (en) | 2001-12-11 |
ES2230314T3 (es) | 2005-05-01 |
US7017861B1 (en) | 2006-03-28 |
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