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FR2339920A1 - Systeme de commande de stabilite selon l'axe des lacets pour engin aerien - Google Patents

Systeme de commande de stabilite selon l'axe des lacets pour engin aerien

Info

Publication number
FR2339920A1
FR2339920A1 FR7702364A FR7702364A FR2339920A1 FR 2339920 A1 FR2339920 A1 FR 2339920A1 FR 7702364 A FR7702364 A FR 7702364A FR 7702364 A FR7702364 A FR 7702364A FR 2339920 A1 FR2339920 A1 FR 2339920A1
Authority
FR
France
Prior art keywords
laces
aircraft
axis
control system
stability control
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.)
Pending
Application number
FR7702364A
Other languages
English (en)
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.)
Sperry Corp
Original Assignee
Sperry Rand Corp
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 Sperry Rand Corp filed Critical Sperry Rand Corp
Publication of FR2339920A1 publication Critical patent/FR2339920A1/fr
Pending legal-status Critical Current

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
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Control Devices (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR7702364A 1976-01-29 1977-01-28 Systeme de commande de stabilite selon l'axe des lacets pour engin aerien Pending FR2339920A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US65355576A 1976-01-29 1976-01-29

Publications (1)

Publication Number Publication Date
FR2339920A1 true FR2339920A1 (fr) 1977-08-26

Family

ID=24621355

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7702364A Pending FR2339920A1 (fr) 1976-01-29 1977-01-28 Systeme de commande de stabilite selon l'axe des lacets pour engin aerien

Country Status (6)

Country Link
US (1) US4094479A (fr)
JP (1) JPS5295499A (fr)
DE (1) DE2703565A1 (fr)
FR (1) FR2339920A1 (fr)
GB (1) GB1561650A (fr)
IT (1) IT1112101B (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3431597A1 (de) * 1984-08-28 1986-03-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zur verbesserung der laengssteuerstabilitaet von luftfahrzeugen
EP0438816A1 (fr) * 1990-01-26 1991-07-31 The Boeing Company Système d'atterrissage automatique avec mesures dans le cas de défaillance d'un moteur
EP0807574A1 (fr) * 1996-05-14 1997-11-19 The Boeing Company Méthode et dispositif d'adaptation du gain d'un coordinateur de virage en fonction de la position des volets
EP2581798A1 (fr) 2011-10-10 2013-04-17 Eurocopter Système de pilotage en lacet pour giravion, mettant en oeuvre un organe mobile de commande entrainé par le pilote et qui génere des commandes de vol par objectif

Families Citing this family (45)

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US4371939A (en) * 1981-03-30 1983-02-01 United Technologies Corporation Roll attitude inhibit of aircraft coordinated turn disengagement
US4482961A (en) * 1981-09-18 1984-11-13 The Boeing Company Automatic control system for directional control of an aircraft during landing rollout
US4527242A (en) * 1982-06-28 1985-07-02 Rockwell International Corporation Automatic flight control pilot assist system
US4622667A (en) * 1984-11-27 1986-11-11 Sperry Corporation Digital fail operational automatic flight control system utilizing redundant dissimilar data processing
JPH06104455B2 (ja) * 1985-03-15 1994-12-21 日産自動車株式会社 車両運動状態推定装置
US4814764A (en) * 1986-09-30 1989-03-21 The Boeing Company Apparatus and method for warning of a high yaw condition in an aircraft
US4855725A (en) 1987-11-24 1989-08-08 Fernandez Emilio A Microprocessor based simulated book
US4935682A (en) * 1988-08-11 1990-06-19 The Boeing Company Full authority engine-out control augmentation subsystem
US4992713A (en) * 1988-10-11 1991-02-12 Rockwell International Corporation Aircraft autopilot with yaw control by rudder force
US5170969A (en) * 1988-11-23 1992-12-15 The Boeing Company Aircraft rudder command system
US5008825A (en) * 1989-05-01 1991-04-16 Nadkarni Arun A Apparatus and methods for automatically maintaining aircraft track angle
US5060889A (en) * 1989-05-01 1991-10-29 The Boeing Company Apparatus and methods for maintaining aircraft track angle during an asymmetric flight condition
US5107080A (en) * 1989-12-01 1992-04-21 Massachusetts Institute Of Technology Multiple degree of freedom damped hand controls
US5050086A (en) * 1990-04-30 1991-09-17 The Boeing Company Aircraft lateral-directional control 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
US5178307A (en) * 1991-08-28 1993-01-12 United Technologies Corporation High speed yaw control system for rotary wing aircraft
US5590853A (en) * 1992-02-03 1997-01-07 Safe Flight Instrument Corporation Aircraft control system
US5667166A (en) * 1995-01-12 1997-09-16 The Boeing Company Aircraft frequency adaptive modal suppression system
US5654906A (en) * 1995-07-06 1997-08-05 Youngquist; John S. Rate gyro error correction and use as heading source
GB9518800D0 (en) * 1995-09-14 1995-11-15 Gkn Westland Helicopters Ltd Method & apparatus for determining the airspeed of rotary wing aircraft
US5761681A (en) * 1995-12-14 1998-06-02 Motorola, Inc. Method of substituting names in an electronic book
US5761682A (en) * 1995-12-14 1998-06-02 Motorola, Inc. Electronic book and method of capturing and storing a quote therein
US5893132A (en) * 1995-12-14 1999-04-06 Motorola, Inc. Method and system for encoding a book for reading using an electronic book
US5815407A (en) * 1995-12-14 1998-09-29 Motorola Inc. Method and device for inhibiting the operation of an electronic device during take-off and landing of an aircraft
FR2789500B1 (fr) 1999-02-04 2001-03-30 Aerospatiale Systeme pour la commande en lacet d'un aeronef
US20030014674A1 (en) * 2001-07-10 2003-01-16 Huffman James R. Method and electronic book for marking a page in a book
US7185858B2 (en) * 2003-11-26 2007-03-06 The Boeing Company Spacecraft gyro calibration system
US7081729B2 (en) * 2004-03-23 2006-07-25 The Boeing Company Variable-structure diagnostics approach achieving optimized low-frequency data sampling for EMA motoring subsystem
US7502675B2 (en) * 2004-04-01 2009-03-10 Delphi Technologies, Inc. Feedforward control of motor vehicle roll angle
US7191047B2 (en) * 2004-09-27 2007-03-13 Delphi Technologies, Inc. Motor vehicle control using a dynamic feedforward approach
WO2009068064A1 (fr) * 2007-11-29 2009-06-04 Airbus Operations Gmbh Yappareil et procédé destinés à tester un système de pédale d'aéronef
FR2948781B1 (fr) * 2009-08-03 2012-02-24 Airbus Operations Sas Procede et dispositif pour attenuer sur un aeronef des effets lateraux engendres par une turbulence
US8718841B2 (en) * 2012-02-14 2014-05-06 Sikorsky Aircraft Corporation Method and system for providing sideslip envelope protection
US8874286B2 (en) * 2012-02-27 2014-10-28 Textron Innovations, Inc. Yaw damping system and method for aircraft
US8949090B2 (en) * 2013-01-28 2015-02-03 The Boeing Company Formation flight control
CN104691742B (zh) * 2013-12-10 2017-07-25 中国航空工业第六一八研究所 一种飞翼布局无人飞机应用阻力方向舵的控制方法
EP2913265B1 (fr) * 2014-02-27 2019-07-17 Goodrich Actuation Systems SAS Système d'augmentation de stabilité et de commande
US9821903B2 (en) 2014-07-14 2017-11-21 The Boeing Company Closed loop control of aircraft control surfaces
US9646505B2 (en) 2014-12-23 2017-05-09 Ge Aviation Systems Llc Method of automatically controlling the descent phase of an aircraft using aircraft avionics executing a descent algorithm
CN105259903A (zh) * 2015-09-30 2016-01-20 中国人民解放军空军工程大学 基于信号流图的飞机自动飞控系统滚转姿态控制结构设计方法
CN105334735A (zh) * 2015-11-13 2016-02-17 成都飞机工业（集团）有限责任公司 一种基于角速率的飞翼布局无人机控制律
WO2018089934A1 (fr) * 2016-11-14 2018-05-17 Boom Technology, Inc. Aéronef supersonique commercial ainsi que systèmes et procédés associés
CA2972495A1 (fr) 2017-06-28 2018-12-28 Bombardier Inc. Orientation de derive destinee a un etat non fonctionnel d'un moteur
CN107745822B (zh) * 2017-09-20 2020-12-18 中国航空工业集团公司沈阳飞机设计研究所 一种无人机侧风着陆控制方法
CN113050676B (zh) * 2019-12-26 2022-11-22 中国航空工业集团公司西安飞机设计研究所 一种飞机偏航阻尼控制指令的监控方法

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB753371A (en) * 1953-03-13 1956-07-25 Northrop Aircraft Inc Improvements in or relating to control apparatus for aircraft
US2827250A (en) * 1954-02-11 1958-03-18 Honeywell Regulator Co Automatic pilots for aircraft
FR1339114A (fr) * 1961-10-30 1963-10-04 Lear Siegler Inc Moyens de commande automatique pour avion
FR1423522A (fr) * 1964-02-05 1966-01-03 Elliott Brothers London Ltd Système de maintien de trajectoire pour avions ou engins aériens analogues
US3636324A (en) * 1970-01-28 1972-01-18 Us Federal Aviation Admin Air data lateral-directional stability augmentation system

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3404856A (en) * 1961-11-14 1968-10-08 Boeing Co Automatic stabilization of aircraft
US3386689A (en) * 1967-02-06 1968-06-04 Sperry Rand Corp Aircraft autopilot with control wheel steering

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB753371A (en) * 1953-03-13 1956-07-25 Northrop Aircraft Inc Improvements in or relating to control apparatus for aircraft
US2827250A (en) * 1954-02-11 1958-03-18 Honeywell Regulator Co Automatic pilots for aircraft
FR1339114A (fr) * 1961-10-30 1963-10-04 Lear Siegler Inc Moyens de commande automatique pour avion
FR1423522A (fr) * 1964-02-05 1966-01-03 Elliott Brothers London Ltd Système de maintien de trajectoire pour avions ou engins aériens analogues
US3636324A (en) * 1970-01-28 1972-01-18 Us Federal Aviation Admin Air data lateral-directional stability augmentation system

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3431597A1 (de) * 1984-08-28 1986-03-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zur verbesserung der laengssteuerstabilitaet von luftfahrzeugen
EP0175883A2 (fr) * 1984-08-28 1986-04-02 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Dispositif pour améliorer la stabilité de commande longitudinale des aéronefs
EP0175883A3 (en) * 1984-08-28 1987-07-15 Messerschmitt-Bolkow-Blohm Gesellschaft Mit Beschrankter Haftung Longitudinal control stability device for aircraft
EP0438816A1 (fr) * 1990-01-26 1991-07-31 The Boeing Company Système d'atterrissage automatique avec mesures dans le cas de défaillance d'un moteur
EP0807574A1 (fr) * 1996-05-14 1997-11-19 The Boeing Company Méthode et dispositif d'adaptation du gain d'un coordinateur de virage en fonction de la position des volets
EP2581798A1 (fr) 2011-10-10 2013-04-17 Eurocopter Système de pilotage en lacet pour giravion, mettant en oeuvre un organe mobile de commande entrainé par le pilote et qui génere des commandes de vol par objectif
US9073635B2 (en) 2011-10-10 2015-07-07 Airbus Helicopters Rotorcraft yaw piloting system making use of a member of the human-operated type and of a flight control generator of the objective type

Also Published As

Publication number Publication date
JPS5295499A (en) 1977-08-11
IT1112101B (it) 1986-01-13
GB1561650A (en) 1980-02-27
DE2703565A1 (de) 1977-08-04
US4094479A (en) 1978-06-13

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