FR3035235B1 - Procede et systeme de commande de vol d'un aeronef selon l'axe de tangage - Google Patents

Procede et systeme de commande de vol d'un aeronef selon l'axe de tangage

Info

Publication number
FR3035235B1
FR3035235B1 FR1553269A FR1553269A FR3035235B1 FR 3035235 B1 FR3035235 B1 FR 3035235B1 FR 1553269 A FR1553269 A FR 1553269A FR 1553269 A FR1553269 A FR 1553269A FR 3035235 B1 FR3035235 B1 FR 3035235B1
Authority
FR
France
Prior art keywords
tanging
axis
aircraft according
controlling flight
flight
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
FR1553269A
Other languages
English (en)
Other versions
FR3035235A1 (fr
Inventor
Mathieu Carton
Pierre Debusschere
Laurent Albugues
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
Priority to FR1553269A priority Critical patent/FR3035235B1/fr
Priority to US15/096,812 priority patent/US10023301B2/en
Priority to CN201610224102.0A priority patent/CN106054904B/zh
Publication of FR3035235A1 publication Critical patent/FR3035235A1/fr
Application granted granted Critical
Publication of FR3035235B1 publication Critical patent/FR3035235B1/fr
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 or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • 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
    • B64C13/04—Initiating means actuated personally
    • B64C13/042—Initiating means actuated personally operated by hand
    • B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
    • 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
    • B64C13/22—Initiating means actuated automatically, e.g. responsive to gust detectors readily revertible to personal control
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/101—Simultaneous control of position or course in three dimensions specially adapted for aircraft
FR1553269A 2015-04-14 2015-04-14 Procede et systeme de commande de vol d'un aeronef selon l'axe de tangage Active FR3035235B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1553269A FR3035235B1 (fr) 2015-04-14 2015-04-14 Procede et systeme de commande de vol d'un aeronef selon l'axe de tangage
US15/096,812 US10023301B2 (en) 2015-04-14 2016-04-12 Method and system for controlling the flight of an aircraft with respect to the pitch axis
CN201610224102.0A CN106054904B (zh) 2015-04-14 2016-04-12 根据俯仰轴控制飞行器的飞行的方法和系统及相关飞行器

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1553269A FR3035235B1 (fr) 2015-04-14 2015-04-14 Procede et systeme de commande de vol d'un aeronef selon l'axe de tangage

Publications (2)

Publication Number Publication Date
FR3035235A1 FR3035235A1 (fr) 2016-10-21
FR3035235B1 true FR3035235B1 (fr) 2017-05-12

Family

ID=54356387

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1553269A Active FR3035235B1 (fr) 2015-04-14 2015-04-14 Procede et systeme de commande de vol d'un aeronef selon l'axe de tangage

Country Status (3)

Country Link
US (1) US10023301B2 (fr)
CN (1) CN106054904B (fr)
FR (1) FR3035235B1 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10259564B2 (en) * 2016-08-08 2019-04-16 Gulfstream Aerospace Corporation Controlling elevator to stabilizer offload in fly-by-wire aircraft systems
FR3057370B1 (fr) * 2016-10-11 2019-08-23 Airbus Operations Procede et systeme de commande de vol d'un aeronef.
US10216471B1 (en) * 2017-08-17 2019-02-26 Honeywell International Inc. Aircraft systems and methods for unusual attitude recovery
CN116679750B (zh) * 2023-06-06 2024-03-29 北京理工大学 一种基于动态舵资源控制分配的飞行器制导控制方法

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3200839C1 (de) * 1982-01-14 1983-08-25 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Vorrichtung zum Trimmen von Flugzeugen
US4642774A (en) * 1982-07-01 1987-02-10 Rockwell International Corporation Automatic flight control with pilot fly-through
FR2603866A1 (fr) 1986-09-12 1988-03-18 Messerschmitt Boelkow Blohm Systeme de commande de gouvernes de profondeur
CN1230721C (zh) * 1996-08-22 2005-12-07 波音公司 飞机俯仰增稳和指令增控系统
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
US7021587B1 (en) * 2004-01-07 2006-04-04 Trutrak Flight Systems, Inc Dual channel fail-safe system and method for adjusting aircraft trim
FR2874204B1 (fr) * 2004-08-13 2007-12-14 Airbus France Sas Systeme de commande de vol electriques pour les gouvernes de profondeur d'un aeronef
FR2909462B1 (fr) * 2006-12-05 2008-12-26 Airbus France Sas Procede et dispositif de controle actif du tangage d'un avion.
US20090187292A1 (en) * 2008-01-17 2009-07-23 Mark Andrew Hreha Integrated pitch, roll, and yaw inceptor
US8718839B2 (en) * 2009-12-06 2014-05-06 Evolved Aircraft Systems, L.L.C. Method and apparatus for automatically controlling aircraft flight control trim systems
CA2974171C (fr) * 2011-07-15 2019-11-12 Bell Helicopter Textron Inc. Lois de commandes de vol pour maintien automatique en vol stationnaire
JP5893890B2 (ja) * 2011-10-18 2016-03-23 三菱重工業株式会社 航空機及び航空機の制御方法
FR2982964B1 (fr) * 2011-11-23 2013-11-22 Eurocopter France Procede de pilotage assiste d'un aeronef a voilure tournante comprenant au moins une helice propulsive, dispositif de pilotage assiste et aeronef
FR2990528B1 (fr) * 2012-05-11 2015-12-25 Airbus Operations Sas Procede de commande de pilotage d'un aeronef
FR3010696B1 (fr) * 2013-09-13 2015-10-09 Airbus Operations Sas Procede et systeme de commande de vol d'un aeronef.

Also Published As

Publication number Publication date
CN106054904B (zh) 2019-06-04
US20160304189A1 (en) 2016-10-20
US10023301B2 (en) 2018-07-17
FR3035235A1 (fr) 2016-10-21
CN106054904A (zh) 2016-10-26

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