BRPI1008968A2 - sistema de comando de vôo para aeronave, e, aeronave - Google Patents
sistema de comando de vôo para aeronave, e, aeronaveInfo
- Publication number
- BRPI1008968A2 BRPI1008968A2 BRPI1008968A BRPI1008968A BRPI1008968A2 BR PI1008968 A2 BRPI1008968 A2 BR PI1008968A2 BR PI1008968 A BRPI1008968 A BR PI1008968A BR PI1008968 A BRPI1008968 A BR PI1008968A BR PI1008968 A2 BRPI1008968 A2 BR PI1008968A2
- Authority
- BR
- Brazil
- Prior art keywords
- aircraft
- control system
- flight control
- aircraft flight
- flight
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/80—Arrangements for reacting to or preventing system or operator failure
- G05D1/87—Arrangements for reacting to or preventing system or operator failure using redundant control arrangements
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D2109/00—Types of controlled vehicles
- G05D2109/20—Aircraft, e.g. drones
- G05D2109/22—Aircraft, e.g. drones with fixed wings
Landscapes
- Engineering & Computer Science (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Safety Devices In Control Systems (AREA)
- Fluid Mechanics (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0951527A FR2943036B1 (fr) | 2009-03-11 | 2009-03-11 | Systeme distribue de commande de vol implemente selon une architecture avionique modulaire integree. |
| PCT/FR2010/050405 WO2010103233A1 (fr) | 2009-03-11 | 2010-03-10 | Système distribué de commande de vol implémenté selon une architecture avionique modulaire intégrée |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| BRPI1008968A2 true BRPI1008968A2 (pt) | 2016-03-15 |
Family
ID=41226156
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| BRPI1008968A BRPI1008968A2 (pt) | 2009-03-11 | 2010-03-10 | sistema de comando de vôo para aeronave, e, aeronave |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US9081372B2 (pt) |
| CN (1) | CN102421667B (pt) |
| BR (1) | BRPI1008968A2 (pt) |
| CA (1) | CA2754031C (pt) |
| FR (1) | FR2943036B1 (pt) |
| WO (1) | WO2010103233A1 (pt) |
Families Citing this family (48)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2959835B1 (fr) * | 2010-05-10 | 2012-06-15 | Airbus Operations Sas | Systeme de commande de vol et aeronef le comportant |
| FR2962619B1 (fr) * | 2010-07-09 | 2013-01-18 | Thales Sa | Dispositif d'acces a des donnees a bord d'un aeronef |
| US8924498B2 (en) * | 2010-11-09 | 2014-12-30 | Honeywell International Inc. | Method and system for process control network migration |
| US8988025B2 (en) * | 2012-01-20 | 2015-03-24 | GM Global Technology Operations LLC | Systems and methods for controlling a brushless motor |
| US8976043B2 (en) * | 2012-08-20 | 2015-03-10 | Textron Innovations, Inc. | Illuminated sidestick controller, such as an illuminated sidestick controller for use in aircraft |
| FR2999152B1 (fr) | 2012-12-12 | 2016-07-22 | Airbus Operations Sas | Systeme de commande d'aeronef a voies fusionnees |
| FR3000196B1 (fr) | 2012-12-21 | 2015-02-06 | Airbus Operations Sas | Dispositif de mise a disposition de valeurs de parametres de navigation d'un vehicule |
| EP2790073A1 (en) * | 2013-04-09 | 2014-10-15 | Airbus Operations GmbH | Control of aircraft systems with at least two remote data concentrators for control of an aircraft system component |
| US9110838B2 (en) | 2013-07-31 | 2015-08-18 | Honeywell International Inc. | Apparatus and method for synchronizing dynamic process data across redundant input/output modules |
| EP2851291B1 (fr) * | 2013-09-23 | 2016-05-11 | Airbus Operations (S.A.S) | Système de commande d'un aéronef |
| US9656741B2 (en) * | 2013-09-24 | 2017-05-23 | The Boeing Company | Control interface for leading and trailing edge devices |
| FR3013468B1 (fr) * | 2013-11-15 | 2017-04-28 | European Aeronautic Defence & Space Co Eads France | Equipement d'entree/sortie pour meuble electronique et meuble comprenant un tel equipement |
| US9720404B2 (en) | 2014-05-05 | 2017-08-01 | Honeywell International Inc. | Gateway offering logical model mapped to independent underlying networks |
| FR3022356B1 (fr) * | 2014-06-16 | 2018-03-02 | Thales | Procede et dispositif de generation d'au moins une consigne parmi une consigne de commande de vol, une consigne de commande moteur et une consigne de guidage d'un aeronef, produit programme d'ordinateur et aeronef associes |
| US10536526B2 (en) | 2014-06-25 | 2020-01-14 | Honeywell International Inc. | Apparatus and method for virtualizing a connection to a node in an industrial control and automation system |
| US10148485B2 (en) | 2014-09-03 | 2018-12-04 | Honeywell International Inc. | Apparatus and method for on-process migration of industrial control and automation system across disparate network types |
| FR3025617B1 (fr) * | 2014-09-05 | 2016-12-16 | Sagem Defense Securite | Architecture bi-voies |
| US10260877B2 (en) * | 2015-02-26 | 2019-04-16 | Stmicroelectronics, Inc. | Reconfigurable sensor unit for electronic device |
| US10162827B2 (en) | 2015-04-08 | 2018-12-25 | Honeywell International Inc. | Method and system for distributed control system (DCS) process data cloning and migration through secured file system |
| US10409270B2 (en) | 2015-04-09 | 2019-09-10 | Honeywell International Inc. | Methods for on-process migration from one type of process control device to different type of process control device |
| CN105807761B (zh) * | 2015-09-02 | 2019-07-12 | 南京乐朋电子科技有限公司 | 一种仿生智能机器鱼的控制系统 |
| FR3047274B1 (fr) * | 2016-01-29 | 2018-01-26 | Safran Power Units | Systeme de regulation electronique partiellement redondant |
| US10599511B2 (en) * | 2016-07-15 | 2020-03-24 | Chippewa Data Control LLC | Method and architecture for critical systems utilizing multi-centric orthogonal topology and pervasive rules-driven data and control encoding |
| FR3061344B1 (fr) * | 2016-12-23 | 2021-01-01 | Thales Sa | Systeme d'aide au pilotage d'aeronef |
| FR3064979B1 (fr) * | 2017-04-07 | 2019-04-05 | Airbus Operations (S.A.S.) | Systeme de commande de vol d'un aeronef |
| US10401816B2 (en) | 2017-07-20 | 2019-09-03 | Honeywell International Inc. | Legacy control functions in newgen controllers alongside newgen control functions |
| US10759520B2 (en) * | 2017-09-29 | 2020-09-01 | The Boeing Company | Flight control system and method of use |
| US10370123B2 (en) * | 2017-11-21 | 2019-08-06 | The Boeing Company | Aircraft control surface actuation systems and methods |
| FR3075997B1 (fr) * | 2017-12-26 | 2020-01-10 | Thales | Calculateur electronique de mise en oeuvre d'au moins une fonction critique, dispositif electronique, procede et programme d'ordinateur associes |
| CN108319158A (zh) * | 2018-01-08 | 2018-07-24 | 北京航空航天大学 | 基于约束满足问题的飞控作动系统配置方法 |
| US10906634B2 (en) * | 2018-01-22 | 2021-02-02 | Hamilton Sunstrand Corporation | Electric vehicle management architecture |
| US10843792B2 (en) | 2018-02-01 | 2020-11-24 | Hamilton Sundstrand Corporation | Autonomous reconfiguration of a multi-redundant actuator control system |
| US11099936B2 (en) * | 2018-09-11 | 2021-08-24 | Embraer S.A. | Aircraft integrated multi system electronic architecture |
| US11440677B2 (en) * | 2018-11-16 | 2022-09-13 | Rolls-Royce Corporation | Secured backup feature for an embedded system |
| FR3088897A1 (fr) | 2018-11-26 | 2020-05-29 | Airbus Operations (S.A.S.) | Système de commande de vol d’un aéronef. |
| CN109617721A (zh) * | 2018-12-11 | 2019-04-12 | 中国航空工业集团公司西安航空计算技术研究所 | 一种机载网络管理端双机容错备份方法、装置及存储介质 |
| US11273906B2 (en) * | 2019-05-10 | 2022-03-15 | Honeywell International Inc. | Redundant fly-by-wire systems with fault resiliency |
| EP3839688B1 (en) * | 2019-12-20 | 2024-07-10 | Volocopter GmbH | Motor control system, method of operating a motor control system and aircraft |
| EP3862835B1 (en) * | 2020-02-10 | 2023-10-25 | Volocopter GmbH | Method and system for monitoring a condition of a vtol-aircraft |
| DE102020107172A1 (de) * | 2020-03-16 | 2021-09-16 | Volocopter Gmbh | Verfahren zur Steuerung eines Fluggeräts, Steuerungseinrichtung für ein Fluggerät und Fluggerät mit einer solchen Steuerungseinrichtung |
| CN112261333B (zh) * | 2020-10-19 | 2022-07-29 | 中国科学院光电技术研究所 | 一种通过光纤1553总线进行图像传输的方法 |
| CN112498664B (zh) * | 2020-11-18 | 2021-12-03 | 中国商用飞机有限责任公司 | 飞行控制系统以及飞行控制方法 |
| CN112644689B (zh) * | 2020-12-29 | 2022-11-22 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机法向过载信号状态确定方法 |
| US11479344B2 (en) | 2021-02-19 | 2022-10-25 | Beta Air, Llc | Methods and systems for fall back flight control configured for use in electric aircraft |
| WO2022192698A1 (en) | 2021-03-12 | 2022-09-15 | Essex Industries, Inc., | Rocker switch |
| US11688568B2 (en) | 2021-03-15 | 2023-06-27 | Essex Industries, Inc. | Five-position switch |
| US11281237B1 (en) * | 2021-05-18 | 2022-03-22 | Beta Air, Llc | System and method for distributed control of an aircraft |
| US11834153B2 (en) * | 2021-05-18 | 2023-12-05 | Beta Air, Llc | System and method for distributed pilot control of an aircraft |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| DE3533720A1 (de) * | 1985-09-21 | 1987-04-16 | Messerschmitt Boelkow Blohm | Notversorgungssystem |
| US4887214A (en) * | 1987-10-27 | 1989-12-12 | The Boeing Company | Flight control system employing two dual controllers operating a dual actuator |
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| US5074495A (en) * | 1987-12-29 | 1991-12-24 | The Boeing Company | Load-adaptive hybrid actuator system and method for actuating control surfaces |
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| US5809220A (en) * | 1995-07-20 | 1998-09-15 | Raytheon Company | Fault tolerant distributed control system |
| US5806805A (en) * | 1996-08-07 | 1998-09-15 | The Boeing Company | Fault tolerant actuation system for flight control actuators |
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| US6112141A (en) * | 1997-10-15 | 2000-08-29 | Dassault Aviation | Apparatus and method for graphically oriented aircraft display and control |
| FR2787759B1 (fr) * | 1998-12-28 | 2001-03-16 | Aerospatiale | Procede et systeme de commande d'une gouverne d'un aeronef a actionnement par verins hydrauliques multiples et a puissance modulable |
| FR2804227B1 (fr) * | 2000-01-24 | 2002-12-13 | Labinal | Ensemble de pilotage et/ou de controle d'organes fonctionnels d'un avion |
| US6550018B1 (en) * | 2000-02-18 | 2003-04-15 | The University Of Akron | Hybrid multiple redundant computer system |
| FR2811780B1 (fr) * | 2000-07-13 | 2002-08-30 | Aerospatiale Matra Airbus | Procede et dispositif de commande d'organes de manoeuvre d'un aeronef, a modules de secours electriques |
| US6443399B1 (en) * | 2000-07-14 | 2002-09-03 | Honeywell International Inc. | Flight control module merged into the integrated modular avionics |
| US6664656B2 (en) * | 2000-09-14 | 2003-12-16 | The Boeing Company | Aircraft electrical power distribution network |
| US6636786B2 (en) * | 2001-10-18 | 2003-10-21 | The Boeing Company | Aircraft energy systems management method |
| US6856045B1 (en) * | 2002-01-29 | 2005-02-15 | Hamilton Sundstrand Corporation | Power distribution assembly with redundant architecture |
| FR2838532B1 (fr) | 2002-04-10 | 2004-07-30 | Airbus France | Systeme et procede de controle de plusieurs actionneurs |
| DE10223880B4 (de) * | 2002-05-29 | 2004-06-17 | Robert Bosch Gmbh | Verfahren zur gegenseitigen Überwachung von Komponenten eines dezentral verteilten Rechnersystems |
| US7505400B2 (en) * | 2004-09-22 | 2009-03-17 | Honeywell International Inc. | Dual lane connection to dual redundant avionics networks |
| GB0422951D0 (en) * | 2004-10-15 | 2004-11-17 | Rolls Royce Plc | Electrical control systems |
| US7337044B2 (en) * | 2004-11-10 | 2008-02-26 | Thales Canada Inc. | Dual/triplex flight control architecture |
| US7159817B2 (en) * | 2005-01-13 | 2007-01-09 | Vandermey Timothy | Vertical take-off and landing (VTOL) aircraft with distributed thrust and control |
| US7946528B2 (en) * | 2005-04-15 | 2011-05-24 | Urban Aeronautics, Ltd. | Flight control system especially suited for VTOL vehicles |
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| JP2009523658A (ja) * | 2006-01-17 | 2009-06-25 | ガルフストリーム・エアロスペース・コーポレイション | 分散型飛行制御システムのバックアップ制御のための装置及び方法 |
| EP1977292A2 (en) * | 2006-01-17 | 2008-10-08 | Gulfstream Aerospace Corporation | System and method for an integrated backup control system |
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| FR2902956B1 (fr) * | 2006-06-23 | 2008-09-19 | Airbus France Sas | Procede de routage de liens virtuels dans un reseau a commutation de trames a determinisme garanti |
| FR2903511B1 (fr) * | 2006-07-07 | 2008-11-14 | Airbus France Sas | Systeme et architecture avionique a gestion de puissance integree |
| US7675919B2 (en) * | 2006-08-02 | 2010-03-09 | Honeywell International Inc. | End system scheduling for switched networks |
| US7393248B2 (en) * | 2006-11-03 | 2008-07-01 | The Boeing Company | Modular power control system with multipin connectors and airflow conrol module |
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| 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 |
| FR2913122B1 (fr) * | 2007-02-22 | 2010-10-15 | Airbus France | Systeme d'information embarque a restauration automatique |
| FR2914446B1 (fr) * | 2007-03-30 | 2009-07-10 | Airbus France Sas | Procede et dispositif de modification du volume sonore d'un signal d'avertissement audio a bord d'un aeronef |
| CA2683132C (en) * | 2007-04-05 | 2013-10-29 | Bombardier Inc. | Multi-axis serially redundant, single channel, multi-path fly-by-wire flight control system |
| FR2915292B1 (fr) * | 2007-04-19 | 2009-07-03 | Airbus France Sas | Procede et systeme de modification d'un contenu d'un message d'alerte a bord d'un aeronef. |
| US8036805B2 (en) * | 2007-07-13 | 2011-10-11 | Honeywell International Inc. | Distributed engine control system |
| FR2920410B1 (fr) * | 2007-09-03 | 2009-10-30 | Airbus France Sas | Architecture repartie entre un fadec et des composants avioniques |
| US8135807B2 (en) * | 2007-09-18 | 2012-03-13 | The Boeing Company | Packet generator for a communication network |
| FR2925191B1 (fr) * | 2007-12-14 | 2010-03-05 | Thales Sa | Architecture de traitement numerique a haute integrite a multiples ressources supervisees |
| FR2927308B1 (fr) * | 2008-02-08 | 2010-10-22 | Airbus France | Systeme distribue de commande de vol. |
| US8130773B2 (en) * | 2008-06-25 | 2012-03-06 | Honeywell International Inc. | Hybrid topology ethernet architecture |
| US8761970B2 (en) * | 2008-10-21 | 2014-06-24 | The Boeing Company | Alternative method to determine the air mass state of an aircraft and to validate and augment the primary method |
| US8442702B2 (en) * | 2008-10-22 | 2013-05-14 | Airbus Operations Gmbh | Fault diagnosis device and method for optimizing maintenance measures in technical systems |
| FR2940786B1 (fr) | 2009-01-08 | 2012-10-19 | Airbus France | Systeme de commandes de vol pour un avion |
| FR2940787A1 (fr) | 2009-01-08 | 2010-07-09 | Airbus France | Systeme de commandes de vol plus electrique a bord d'un aeronef |
| GB2468652B (en) * | 2009-03-16 | 2011-08-31 | Ge Aviat Systems Ltd | Electrical power distribution |
| DE102009041599A1 (de) * | 2009-09-15 | 2011-04-14 | Airbus Operations Gmbh | Steuervorrichtung, Ein-/Ausgabevorrichtung, Verbindungsschaltevorrichtung und Verfahren für ein Flugzeug-Steuersystem |
| FR2952447B1 (fr) * | 2009-11-06 | 2012-08-17 | Ratier Figeac Soc | Dispositif de controle electronique de fonctionnement d'un organe de pilotage a surveillance croisee, dispositif de pilotage et aeronef |
| FR2955309B1 (fr) | 2010-01-18 | 2013-05-10 | Airbus Operations Sas | Systeme de commande de vol pour un aeronef |
| FR2957164B1 (fr) * | 2010-03-03 | 2012-05-11 | Airbus Operations Sas | Procedes et dispositifs de validation de configuration d'un systeme multielements complexe |
| US20110251739A1 (en) * | 2010-04-09 | 2011-10-13 | Honeywell International Inc. | Distributed fly-by-wire system |
| US8434301B2 (en) * | 2010-04-16 | 2013-05-07 | Nabtesco Corporation | Local backup hydraulic actuator for aircraft control systems |
| FR2959578B1 (fr) * | 2010-05-03 | 2012-08-03 | Airbus Operations Sas | Verification d'un systeme de communication d'un aeronef en developpement |
| FR2959835B1 (fr) * | 2010-05-10 | 2012-06-15 | Airbus Operations Sas | Systeme de commande de vol et aeronef le comportant |
| WO2011159209A1 (en) * | 2010-06-17 | 2011-12-22 | Saab Ab | Distributed avionics |
| FR2963447B1 (fr) * | 2010-07-28 | 2012-09-07 | Airbus Operations Sas | Procede et dispositif de test d?interfaces d?entree/sortie de modules |
| US8499193B2 (en) * | 2010-07-30 | 2013-07-30 | Honeywell International Inc. | Integrated dissimilar high integrity processing |
| US8935015B2 (en) * | 2011-05-09 | 2015-01-13 | Parker-Hannifin Corporation | Flight control system with alternate control path |
-
2009
- 2009-03-11 FR FR0951527A patent/FR2943036B1/fr active Active
-
2010
- 2010-03-10 CA CA2754031A patent/CA2754031C/fr not_active Expired - Fee Related
- 2010-03-10 WO PCT/FR2010/050405 patent/WO2010103233A1/fr not_active Ceased
- 2010-03-10 BR BRPI1008968A patent/BRPI1008968A2/pt not_active IP Right Cessation
- 2010-03-10 US US13/255,778 patent/US9081372B2/en active Active
- 2010-03-10 CN CN201080020654.0A patent/CN102421667B/zh active Active
Also Published As
| Publication number | Publication date |
|---|---|
| US9081372B2 (en) | 2015-07-14 |
| CA2754031C (fr) | 2017-02-28 |
| CA2754031A1 (fr) | 2010-09-16 |
| US20120101663A1 (en) | 2012-04-26 |
| WO2010103233A1 (fr) | 2010-09-16 |
| FR2943036A1 (fr) | 2010-09-17 |
| FR2943036B1 (fr) | 2011-04-15 |
| CN102421667A (zh) | 2012-04-18 |
| CN102421667B (zh) | 2015-04-01 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
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