RU2017143766A3 - - Google Patents

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Publication number
RU2017143766A3
RU2017143766A3 RU2017143766A RU2017143766A RU2017143766A3 RU 2017143766 A3 RU2017143766 A3 RU 2017143766A3 RU 2017143766 A RU2017143766 A RU 2017143766A RU 2017143766 A RU2017143766 A RU 2017143766A RU 2017143766 A3 RU2017143766 A3 RU 2017143766A3
Authority
RU
Russia
Application number
RU2017143766A
Other languages
Russian (ru)
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RU2017143766A (ru
RU2738643C2 (ru
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 filed Critical
Publication of RU2017143766A publication Critical patent/RU2017143766A/ru
Publication of RU2017143766A3 publication Critical patent/RU2017143766A3/ru
Application granted granted Critical
Publication of RU2738643C2 publication Critical patent/RU2738643C2/ru

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • B64C13/50Transmitting means with power amplification using electrical energy
    • B64C13/503Fly-by-Wire
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02Initiating means
    • B64C13/16Initiating means actuated automatically, e.g. responsive to gust detectors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/24Transmitting means
    • B64C13/38Transmitting means with power amplification
    • B64C13/50Transmitting means with power amplification using electrical energy
    • B64C13/505Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Feedback Control In General (AREA)
RU2017143766A 2016-12-15 2017-12-14 Управляющая система для управления исполнительными органами летательного аппарата RU2738643C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102016014974.4 2016-12-15
DE102016014974.4A DE102016014974A1 (de) 2016-12-15 2016-12-15 Aktuatorsteuerung zur Steuerung von Aktuatoren eines Fluggeräts

Publications (3)

Publication Number Publication Date
RU2017143766A RU2017143766A (ru) 2019-06-17
RU2017143766A3 true RU2017143766A3 (pt) 2020-11-09
RU2738643C2 RU2738643C2 (ru) 2020-12-15

Family

ID=62250622

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2017143766A RU2738643C2 (ru) 2016-12-15 2017-12-14 Управляющая система для управления исполнительными органами летательного аппарата

Country Status (4)

Country Link
CN (1) CN108216580B (pt)
DE (1) DE102016014974A1 (pt)
FR (2) FR3060527B1 (pt)
RU (1) RU2738643C2 (pt)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10988237B1 (en) * 2019-12-17 2021-04-27 The Boeing Company Feed forward equalization control for active-active redundant actuation systems
EP4029776A1 (en) * 2021-01-18 2022-07-20 Goodrich Actuation Systems SAS Actuator control for force fight mitigation

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH235834A (de) * 1943-10-29 1944-12-31 Sinniger Edgar Elektromechanische Reguliereinrichtung für Primär-Kraftmaschinen.
US4382281A (en) * 1980-08-08 1983-05-03 United Technologies Corporation Helicopter force feel actuator automatic static null compensation
JP3620907B2 (ja) * 1995-11-16 2005-02-16 カヤバ工業株式会社 航空機舵面のサーボ制御システム
JPH1091210A (ja) * 1996-09-18 1998-04-10 Kayaba Ind Co Ltd 航空機舵面のサーボ制御システム
US7007179B2 (en) * 2001-02-08 2006-02-28 Honeywell International Inc. Electric load management center
DE10258020B3 (de) * 2002-12-12 2004-06-09 Daimlerchrysler Ag Fahrzeugsitz mit aktiver Sitzfederung mit zwei Bewegungsfreiheitsgraden
DE10325890A1 (de) * 2003-06-06 2004-12-30 Siemens Ag Verfahren zum Initialisieren einer fremdkraftbetätigten Verstellvorrichtung und Vorrichtung zur Durchführung des Initialisierungsverfahrens
WO2006134425A2 (en) * 2004-05-06 2006-12-21 Zf Friedrichshafen Ag Helicopter rotor control system with individual blade control
US8033509B2 (en) 2007-02-27 2011-10-11 Honeywell International Inc. Load optimized redundant flight control surface actuation system and method
RU68145U1 (ru) * 2007-06-26 2007-11-10 Закрытое акционерное общество "НТЦ РИССА НАУЧНО-ПРОИЗВОДСТВЕННОЕ ПРЕДПРИЯТИЕ" Система автоматического управления беспилотным летательным аппаратом
US8245967B2 (en) * 2008-11-25 2012-08-21 The Boeing Company Actuator force equalization controller
RU2403610C1 (ru) * 2009-08-05 2010-11-10 Федеральное государственное унитарное предприятие "Научно-производственное объединение автоматики имени академика Н.А. Семихатова" Способ высокоточного и динамичного управления траекторией движения подвижного объекта (морские и речные суда, летательные аппараты, управляемые ракеты)
DE102010022200A1 (de) * 2010-05-20 2011-11-24 Liebherr-Aerospace Lindenberg Gmbh Steuerknüppelsystem
DE102010063359A1 (de) * 2010-12-17 2012-06-21 Robert Bosch Gmbh Verfahren zum Einstellen der von einer Feststellbremse ausgeübten Stellkraft
BG111127A (bg) * 2012-01-30 2013-07-31 Hrisimira ираИЛИЕВА Хрисим Ilieva Метод за пространствено проектиране на тренажори за летателни и космически апарати и авиационен тренажор, съгласно метода
US8874360B2 (en) * 2012-03-09 2014-10-28 Proxy Technologies Inc. Autonomous vehicle and method for coordinating the paths of multiple autonomous vehicles
US9296474B1 (en) * 2012-08-06 2016-03-29 The United States of America as represented by the Administrator of the National Aeronautics & Space Administration (NASA) Control systems with normalized and covariance adaptation by optimal control modification
US9446838B2 (en) * 2014-08-14 2016-09-20 Gulfstream Aerospace Corporation Systems for inceptor control in fly-by-wire aircraft systems

Also Published As

Publication number Publication date
FR3071479A1 (fr) 2019-03-29
FR3060527B1 (fr) 2022-01-14
CN108216580B (zh) 2023-03-24
RU2017143766A (ru) 2019-06-17
FR3060527A1 (fr) 2018-06-22
DE102016014974A1 (de) 2018-06-21
RU2738643C2 (ru) 2020-12-15
CN108216580A (zh) 2018-06-29

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