FR2750947B1 - Systeme de commande de vol pour un avion - Google Patents

Systeme de commande de vol pour un avion

Info

Publication number
FR2750947B1
FR2750947B1 FR9708575A FR9708575A FR2750947B1 FR 2750947 B1 FR2750947 B1 FR 2750947B1 FR 9708575 A FR9708575 A FR 9708575A FR 9708575 A FR9708575 A FR 9708575A FR 2750947 B1 FR2750947 B1 FR 2750947B1
Authority
FR
France
Prior art keywords
airplane
control system
flight control
flight
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.)
Expired - Fee Related
Application number
FR9708575A
Other languages
English (en)
Other versions
FR2750947A1 (fr
Inventor
Shinagawa Takashi
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.)
Subaru Corp
Original Assignee
Fuji Jukogyo KK
Fuji Heavy Industries Ltd
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 Fuji Jukogyo KK, Fuji Heavy Industries Ltd filed Critical Fuji Jukogyo KK
Publication of FR2750947A1 publication Critical patent/FR2750947A1/fr
Application granted granted Critical
Publication of FR2750947B1 publication Critical patent/FR2750947B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • 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
    • G05D1/085—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability to ensure coordination between different movements

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR9708575A 1996-07-05 1997-07-07 Systeme de commande de vol pour un avion Expired - Fee Related FR2750947B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17675596A JP3645038B2 (ja) 1996-07-05 1996-07-05 航空機の飛行制御装置

Publications (2)

Publication Number Publication Date
FR2750947A1 FR2750947A1 (fr) 1998-01-16
FR2750947B1 true FR2750947B1 (fr) 1999-02-19

Family

ID=16019253

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9708575A Expired - Fee Related FR2750947B1 (fr) 1996-07-05 1997-07-07 Systeme de commande de vol pour un avion

Country Status (4)

Country Link
US (2) US5984240A (fr)
JP (1) JP3645038B2 (fr)
FR (1) FR2750947B1 (fr)
GB (1) GB2315138B (fr)

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2777535B1 (fr) * 1998-04-21 2000-06-16 Eurocopter France Systeme de commande de vol d'un aeronef, en particulier d'un helicoptere
US6282466B1 (en) 1998-11-03 2001-08-28 The Boeing Company Method of automated thrust-based roll guidance limiting
JP3195918B2 (ja) 1999-03-12 2001-08-06 株式会社コミュータヘリコプタ先進技術研究所 ヘリコプタ用飛行制御装置
US6915989B2 (en) * 2002-05-01 2005-07-12 The Boeing Company Aircraft multi-axis modal suppression system
US6676071B1 (en) * 2002-06-21 2004-01-13 The United States Of America As Represented By The Secretary Of The Navy Gliding vehicle guidance
FR2841532B1 (fr) * 2002-06-27 2004-12-17 Airbus France Avion a controle actif du vrillage de ses ailes
US6814330B2 (en) * 2002-12-12 2004-11-09 The Boeing Company Method and computer program product for controlling the control effectors of an aerodynamic vehicle
WO2007001369A2 (fr) * 2004-09-17 2007-01-04 Aurora Flight Sciences Systeme et methode pour commander le regime d'un moteur a soufflante canalisee
EP1796962A2 (fr) * 2004-09-17 2007-06-20 Aurora Flight Sciences Commande d'approche destinee a un avion a decollage et a atterrissage vertical de type tail sitter (assis sur la queue)
WO2007001371A2 (fr) * 2004-09-17 2007-01-04 Aurora Flight Sciences Systeme d'attache reacteur antivibratile, et procede se rapportant a un aeronef a soufflante canalisee
US7441724B2 (en) * 2004-09-17 2008-10-28 Aurora Flight Sciences Corporation System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft
US20070221783A1 (en) * 2004-09-17 2007-09-27 Robert Parks Adaptive landing gear
FR2876483B1 (fr) * 2004-10-08 2007-07-20 Airbus France Sas Procede et systeme d'evitement pour un aeronef
US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
FR2897838B1 (fr) * 2006-02-27 2009-01-09 Airbus France Sas Systeme de commande electrique pour une gouverne de direction d'un avion.
FR2909462B1 (fr) * 2006-12-05 2008-12-26 Airbus France Sas Procede et dispositif de controle actif du tangage d'un avion.
DE602006012860D1 (de) 2006-12-22 2010-04-22 Saab Ab Vorrichtung an einem Flugkörper und Verfahren zur Kollisionsvermeidung
JP2008201183A (ja) * 2007-02-17 2008-09-04 Morioka Seiko Instruments Inc 姿勢制御装置
TWI361095B (en) * 2007-03-23 2012-04-01 Yu Tuan Lee Remote-controlled motion apparatus with acceleration self-sense and remote control apparatus therefor
US8311508B2 (en) * 2007-09-11 2012-11-13 Verizon Patent And Licensing Inc. Wireless enabled device tracking system and method
US8200375B2 (en) 2008-02-12 2012-06-12 Stuckman Katherine C Radio controlled aircraft, remote controller and methods for use therewith
ATE545924T1 (de) * 2008-11-04 2012-03-15 Saab Ab Vermeidungsmanöver-generator für ein flugzeug
US9085371B2 (en) * 2008-11-20 2015-07-21 The Boeing Company Automatic throttle roll angle compensation
US9058040B2 (en) * 2009-02-27 2015-06-16 The Boeing Company Automatic pilot pitch angle compensation
RU2462745C1 (ru) * 2011-08-25 2012-09-27 Федеральное Государственное Автономное Образовательное Учреждение Высшего Профессионального Образования "Дальневосточный Федеральный Университет" (Двфу) Система коррекции траектории движения манипулятора
DE102013202585A1 (de) 2013-02-18 2014-08-21 Hochschule Ostwestfalen-Lippe Kontrolleinheit für ein Flugobjekt
CN105912014B (zh) 2013-06-25 2019-01-15 深圳市大疆创新科技有限公司 飞行器的控制***及控制方法
US9650155B2 (en) 2013-06-25 2017-05-16 SZ DJI Technology Co., Ltd Aircraft control apparatus, control system and control method
US10059446B2 (en) * 2016-06-06 2018-08-28 Traxxas Lp Ground vehicle-like control for remote control aircraft
CN106094859B (zh) * 2016-08-26 2018-08-10 杨百川 一种无人机在线实时飞行品质评估与调参方法
US10486809B2 (en) * 2016-10-13 2019-11-26 The Boeing Company Unmanned aerial system targeting
CN113961011B (zh) * 2021-09-16 2024-03-19 中国航空工业集团公司西安飞机设计研究所 一种航迹倾角保持控制方法

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2595309A (en) * 1946-06-26 1952-05-06 Sperry Corp Flight control apparatus for aircraft
US3077557A (en) * 1960-09-30 1963-02-12 Sperry Rand Corp Flight path computer
US3578269A (en) * 1969-06-11 1971-05-11 Lear Siegler Inc Automatic flare and altitude hold system
US3945593A (en) * 1972-10-10 1976-03-23 Bodenseewerk Geratetechnik Gmbh Flight control apparatus
US4261537A (en) * 1979-02-28 1981-04-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Velocity vector control system augmented with direct lift control
US4357661A (en) * 1980-02-22 1982-11-02 The Boeing Company Aircraft landing control system
US4413320A (en) * 1980-08-22 1983-11-01 The Bendix Corporation Control system
US4511972A (en) * 1982-01-04 1985-04-16 General Electric Company Large angle, gravity compensated, bank-to-turn pursuit controller
JPS61196896A (ja) 1985-02-27 1986-09-01 日本電気株式会社 航空機自動操縦装置
US4674710A (en) * 1985-10-17 1987-06-23 The United States Of America As Represented By The Secretary Of The Air Force Automatic formation turns
US4924401A (en) * 1987-10-30 1990-05-08 The United States Of America As Represented By The Secretary Of The Air Force Aircraft ground collision avoidance and autorecovery systems device
IL85731A (en) * 1988-03-14 1995-05-26 B T A Automatic Piloting Syste Aircraft control facility and method, in particular remotely controlled aircraft
US5170969A (en) * 1988-11-23 1992-12-15 The Boeing Company Aircraft rudder command system
FR2658636B1 (fr) * 1990-02-22 1994-08-26 Sextant Avionique Procede de pilotage d'un aeronef en vol a tres basse altitude.

Also Published As

Publication number Publication date
JP3645038B2 (ja) 2005-05-11
US6168117B1 (en) 2001-01-02
GB2315138A (en) 1998-01-21
US5984240A (en) 1999-11-16
JPH1016892A (ja) 1998-01-20
FR2750947A1 (fr) 1998-01-16
GB2315138B (en) 1998-11-11
GB9713828D0 (en) 1997-09-03

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20150331