FR2530579B1 - Dispositif pour l'equilibrage d'avions - Google Patents
Dispositif pour l'equilibrage d'avionsInfo
- Publication number
- FR2530579B1 FR2530579B1 FR8300096A FR8300096A FR2530579B1 FR 2530579 B1 FR2530579 B1 FR 2530579B1 FR 8300096 A FR8300096 A FR 8300096A FR 8300096 A FR8300096 A FR 8300096A FR 2530579 B1 FR2530579 B1 FR 2530579B1
- Authority
- FR
- France
- Prior art keywords
- airplanes
- balancing
- balancing airplanes
- 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
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
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
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)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Feedback Control In General (AREA)
- Toys (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3200839A DE3200839C1 (de) | 1982-01-14 | 1982-01-14 | Vorrichtung zum Trimmen von Flugzeugen |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2530579A1 FR2530579A1 (fr) | 1984-01-27 |
FR2530579B1 true FR2530579B1 (fr) | 1986-08-14 |
Family
ID=6152988
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8300096A Expired FR2530579B1 (fr) | 1982-01-14 | 1983-01-05 | Dispositif pour l'equilibrage d'avions |
Country Status (4)
Country | Link |
---|---|
US (1) | US4758958A (fr) |
BR (1) | BR8300286A (fr) |
DE (1) | DE3200839C1 (fr) |
FR (1) | FR2530579B1 (fr) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2217878B (en) * | 1988-04-23 | 1992-01-29 | Ferranti Plc | A system including an autopilot, with a simulator, for a fluid borne vehicle |
US5012423A (en) * | 1989-04-17 | 1991-04-30 | Mcdonnell Douglas Corporation | Back-up fly by wire control system |
US5008825A (en) * | 1989-05-01 | 1991-04-16 | Nadkarni Arun A | Apparatus and methods for automatically maintaining aircraft track angle |
FR2741855B1 (fr) * | 1995-12-05 | 1998-01-30 | Eurocopter France | Systeme de manche cyclique assurant la stabilite en vitesse d'un helicoptere |
US5853152A (en) * | 1997-04-29 | 1998-12-29 | Sikorsky Aircraft Corporation | Collective detent system for vertical takeoff flight operations |
FR2787763B1 (fr) * | 1998-12-24 | 2001-02-23 | Eurocopter France | Dispositif d'aide au recentrage d'un organe de commande d'un aeronef |
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 |
US6246929B1 (en) | 1999-06-16 | 2001-06-12 | Lockheed Martin Corporation | Enhanced stall and recovery control system |
US6236914B1 (en) | 1999-06-16 | 2001-05-22 | Lockheed Martin Corporation | Stall and recovery control system |
US7021587B1 (en) | 2004-01-07 | 2006-04-04 | Trutrak Flight Systems, Inc | Dual channel fail-safe system and method for adjusting aircraft trim |
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 |
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 |
US9193439B2 (en) * | 2013-03-14 | 2015-11-24 | Textron Innovations, Inc. | Reversible flight control systems |
FR3035235B1 (fr) * | 2015-04-14 | 2017-05-12 | Airbus Operations Sas | Procede et systeme de commande de vol d'un aeronef selon l'axe de tangage |
US11059577B2 (en) * | 2019-03-25 | 2021-07-13 | Textron Innovations Inc. | System and method for monitoring aircraft pilot control position and providing a retrim prompt |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1234925A (fr) * | 1958-10-03 | 1960-07-01 | United Aircraft Corp | équipement de commande de vol |
FR1347243A (fr) * | 1962-11-20 | 1963-12-27 | Boeing Co | Installation d'auto-pilotage pour avion à décollage vertical et avion ou analogue pourvu de ladite installation |
US3345018A (en) * | 1965-05-24 | 1967-10-03 | Honeywell Inc | Dirigible craft control apparatus |
US3700995A (en) * | 1971-05-20 | 1972-10-24 | United Aircraft Corp | Trim reference for helicopter feel augmentation system |
US4092716A (en) * | 1975-07-11 | 1978-05-30 | Mcdonnell Douglas Corporation | Control means and method for controlling an object |
US3960348A (en) * | 1975-08-04 | 1976-06-01 | United Technologies Corporation | Aerodynamic surface control feel augmentation system |
US4159444A (en) * | 1978-03-21 | 1979-06-26 | Sperry Rand Corporation | Fail operational dual electromechanical servo actuator for aircraft with model monitoring |
US4198017A (en) * | 1978-10-13 | 1980-04-15 | The United States Of America As Represented By The Secretary Of The Army | Control augmentation system for flight vehicles |
US4281811A (en) * | 1979-06-15 | 1981-08-04 | Edo-Aire Mitchell | Pitch trim system for aircraft |
US4370706A (en) * | 1980-09-26 | 1983-01-25 | The Bendix Corporation | Controller for a dual servo system |
US4500967A (en) * | 1981-11-27 | 1985-02-19 | United Technologies Corporation | Aircraft short-term roll attitude retention system |
US4481586A (en) * | 1982-03-09 | 1984-11-06 | Sperry Corporation | Adaptive washout circuit for use in a stability augmentation system |
US4642774A (en) * | 1982-07-01 | 1987-02-10 | Rockwell International Corporation | Automatic flight control with pilot fly-through |
DE3431597A1 (de) * | 1984-08-28 | 1986-03-13 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Vorrichtung zur verbesserung der laengssteuerstabilitaet von luftfahrzeugen |
-
1982
- 1982-01-14 DE DE3200839A patent/DE3200839C1/de not_active Expired
-
1983
- 1983-01-05 FR FR8300096A patent/FR2530579B1/fr not_active Expired
- 1983-01-14 BR BR8300286A patent/BR8300286A/pt unknown
-
1986
- 1986-02-20 US US06/831,644 patent/US4758958A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2530579A1 (fr) | 1984-01-27 |
BR8300286A (pt) | 1983-10-25 |
US4758958A (en) | 1988-07-19 |
DE3200839C1 (de) | 1983-08-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |