DE602006011208D1 - Verfahren und system zum begrenzen eines flugzeug-steueroberflächen-lenkwinkels - Google Patents

Verfahren und system zum begrenzen eines flugzeug-steueroberflächen-lenkwinkels

Info

Publication number
DE602006011208D1
DE602006011208D1 DE602006011208T DE602006011208T DE602006011208D1 DE 602006011208 D1 DE602006011208 D1 DE 602006011208D1 DE 602006011208 T DE602006011208 T DE 602006011208T DE 602006011208 T DE602006011208 T DE 602006011208T DE 602006011208 D1 DE602006011208 D1 DE 602006011208D1
Authority
DE
Germany
Prior art keywords
steering angle
control surface
limiting
plane control
aircraft
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
DE602006011208T
Other languages
English (en)
Inventor
Didier Averseng
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Publication of DE602006011208D1 publication Critical patent/DE602006011208D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • 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
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0066—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for limitation of acceleration or stress

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Steering Control In Accordance With Driving Conditions (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Traffic Control Systems (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Power Steering Mechanism (AREA)
  • Length Measuring Devices With Unspecified Measuring Means (AREA)
  • Radio Relay Systems (AREA)
  • Retarders (AREA)
DE602006011208T 2005-10-27 2006-10-19 Verfahren und system zum begrenzen eines flugzeug-steueroberflächen-lenkwinkels Active DE602006011208D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0553267A FR2892699B1 (fr) 2005-10-27 2005-10-27 Procede et systeme de limitation d'un angle de braquage de la gouverne d'un aeronef
PCT/FR2006/051071 WO2007048960A2 (fr) 2005-10-27 2006-10-19 Procede et systeme de limitation d'un angle de braquage de la gouverne d'un aeronef

Publications (1)

Publication Number Publication Date
DE602006011208D1 true DE602006011208D1 (de) 2010-01-28

Family

ID=36939019

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006011208T Active DE602006011208D1 (de) 2005-10-27 2006-10-19 Verfahren und system zum begrenzen eines flugzeug-steueroberflächen-lenkwinkels

Country Status (11)

Country Link
US (1) US8285426B2 (de)
EP (1) EP1949196B1 (de)
JP (1) JP5225852B2 (de)
CN (1) CN101297250B (de)
AT (1) ATE452357T1 (de)
BR (1) BRPI0618013A2 (de)
CA (1) CA2625747C (de)
DE (1) DE602006011208D1 (de)
FR (1) FR2892699B1 (de)
RU (1) RU2411566C2 (de)
WO (1) WO2007048960A2 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2971486B1 (fr) * 2011-02-15 2013-03-08 Airbus Operations Sas Procede et dispositif pour le controle d'un aeronef en lacet.
CN103303465A (zh) * 2012-03-09 2013-09-18 陕西飞机工业（集团）有限公司 一种飞机方向舵调整片偏角限制装置电气控制方法及其系统
CN102815394A (zh) * 2012-08-13 2012-12-12 湖南山河科技股份有限公司 轻型飞机方向舵弹簧对中定位机构
FR2995873B1 (fr) * 2012-09-27 2014-10-03 Airbus Operations Sas Procede et dispositif d'alerte contre un actionnement inapproprie d'un palonnier d'un aeronef.
CN105109671B (zh) * 2015-09-25 2017-05-17 江西洪都航空工业集团有限责任公司 一种前缘襟翼控制方法
US10228692B2 (en) 2017-03-27 2019-03-12 Gulfstream Aerospace Corporation Aircraft flight envelope protection and recovery autopilot
US11897597B2 (en) * 2020-07-20 2024-02-13 The Boeing Company Flap pressure shape biasing
CN111976955B (zh) * 2020-07-24 2023-03-14 中国航空工业集团公司西安飞行自动控制研究所 民机电传飞控双驾驶杆盘的单侧卡阻故障处理方法和装置
CN114560073B (zh) * 2021-12-30 2024-01-30 中国航空工业集团公司西安飞机设计研究所 一种螺旋桨飞机滑流预感知方向舵偏转控制方法及其系统
US20240124152A1 (en) * 2022-10-14 2024-04-18 Beta Air, Llc Apparatus and method for displaying pilot authority

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4455004A (en) * 1982-09-07 1984-06-19 Lockheed Corporation Flight control device for airplanes
DE3638820A1 (de) * 1986-09-12 1988-03-24 Messerschmitt Boelkow Blohm Seitenruder-steuerungsanordnung fuer luftfahrzeuge
US5170969A (en) * 1988-11-23 1992-12-15 The Boeing Company Aircraft rudder command system
EP0488428A3 (en) * 1990-09-24 1992-10-14 The Boeing Company Apparatus and method for reducing aircraft loads resulting from atmospheric turbulence and gusts
JP2885125B2 (ja) * 1995-03-30 1999-04-19 トヨタ自動車株式会社 車両の旋回に伴って変化する運動状態量の推定方法
FR2760718B1 (fr) * 1997-03-14 1999-05-28 Aerospatiale Procede et dispositif de commande d'une gouverne d'inclinaison ou de profondeur d'un aeronef
FR2738796B1 (fr) * 1995-09-15 1997-12-05 Aerospatiale Procede et dispositif de commande de la gouverne de direction d'un aeronef
US5823479A (en) * 1996-05-20 1998-10-20 The Boeing Company Landing attitude modifier for airplane
FR2809373B1 (fr) * 2000-05-29 2002-08-09 Aerospatiale Matra Airbus Systeme de commande electrique pour une gouverne de direction d'aeronef
US6561020B2 (en) * 2001-05-08 2003-05-13 Rosemount Aerospace Inc. Method to calculate sideslip angle and correct static pressure for sideslip effects using inertial information
FR2844251B1 (fr) * 2002-09-09 2005-05-27 Airbus France Procede et systeme pour deplacer une gouverne d'un aeronef.

Also Published As

Publication number Publication date
CN101297250A (zh) 2008-10-29
WO2007048960A3 (fr) 2007-06-14
JP2009513433A (ja) 2009-04-02
US20090222151A1 (en) 2009-09-03
CA2625747A1 (fr) 2007-05-03
BRPI0618013A2 (pt) 2011-08-16
CA2625747C (fr) 2014-08-05
RU2008121220A (ru) 2009-12-10
FR2892699B1 (fr) 2008-02-08
RU2411566C2 (ru) 2011-02-10
US8285426B2 (en) 2012-10-09
CN101297250B (zh) 2010-12-15
FR2892699A1 (fr) 2007-05-04
EP1949196A2 (de) 2008-07-30
EP1949196B1 (de) 2009-12-16
ATE452357T1 (de) 2010-01-15
JP5225852B2 (ja) 2013-07-03
WO2007048960A2 (fr) 2007-05-03

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Legal Events

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