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
Links
Classifications
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- 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
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/503—Fly-by-Wire
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- 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
-
- 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
-
- 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
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
- B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions
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- 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
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)
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)
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)
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 |
-
2016
- 2016-12-15 DE DE102016014974.4A patent/DE102016014974A1/de active Pending
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2017
- 2017-12-04 FR FR1761580A patent/FR3060527B1/fr active Active
- 2017-12-14 RU RU2017143766A patent/RU2738643C2/ru active
- 2017-12-15 CN CN201711348818.2A patent/CN108216580B/zh active Active
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2018
- 2018-09-28 FR FR1858970A patent/FR3071479A1/fr not_active Withdrawn
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 |