FR2200982A5 - - Google Patents
Info
- Publication number
- FR2200982A5 FR2200982A5 FR7333884A FR7333884A FR2200982A5 FR 2200982 A5 FR2200982 A5 FR 2200982A5 FR 7333884 A FR7333884 A FR 7333884A FR 7333884 A FR7333884 A FR 7333884A FR 2200982 A5 FR2200982 A5 FR 2200982A5
- Authority
- FR
- France
- 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
- G05D1/08—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
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)
- Feedback Control In General (AREA)
- Navigation (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US00291441A US3857535A (en) | 1972-09-22 | 1972-09-22 | Monitor for the elastic mode stabilizing channels of an automatic flight control system |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2200982A5 true FR2200982A5 (fr) | 1974-04-19 |
Family
ID=23120295
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7333884A Expired FR2200982A5 (fr) | 1972-09-22 | 1973-09-21 |
Country Status (7)
Country | Link |
---|---|
US (1) | US3857535A (fr) |
JP (2) | JPS4970400A (fr) |
DE (1) | DE2347673A1 (fr) |
FR (1) | FR2200982A5 (fr) |
GB (1) | GB1439782A (fr) |
IT (1) | IT994402B (fr) |
SE (1) | SE389650B (fr) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5555293A (en) * | 1978-10-20 | 1980-04-23 | Hitachi Ltd | Failed fuel detector |
US5082207A (en) * | 1985-02-04 | 1992-01-21 | Rockwell International Corporation | Active flexible wing aircraft control system |
US4692610A (en) * | 1986-01-30 | 1987-09-08 | Grumman Aerospace Corporation | Fiber optic aircraft load relief control system |
US4734577A (en) * | 1986-01-30 | 1988-03-29 | Grumman Aerospace Corporation | Continuous strain measurement along a span |
US4947693A (en) * | 1987-07-28 | 1990-08-14 | Grumman Aerospace Corporation | Discrete strain sensor |
US4879643A (en) * | 1987-11-19 | 1989-11-07 | The Boeing Company | Decentralized cautious adaptive control system |
FR2668750B1 (fr) * | 1990-11-06 | 1993-01-22 | Aerospatiale | Systeme pour la commande integree en profondeur et en poussee d'un aeronef. |
US5667166A (en) * | 1995-01-12 | 1997-09-16 | The Boeing Company | Aircraft frequency adaptive modal suppression system |
US5669582A (en) * | 1995-05-12 | 1997-09-23 | The Boeing Company | Method and apparatus for reducing unwanted sideways motion in the aft cabin and roll-yaw upsets of an airplane due to atmospheric turbulence and wind gusts |
US6505108B2 (en) * | 2000-03-01 | 2003-01-07 | Delphi Technologies, Inc. | Damper based vehicle yaw control |
DE10012517C2 (de) * | 2000-03-15 | 2002-02-07 | Eads Deutschland Gmbh | Verfahren zur Auslegung von Flugreglern |
WO2006135405A2 (fr) | 2004-08-30 | 2006-12-21 | Lord Corporation | Systeme de commande de vibrations d'un helicoptere et generateur de force rotative destine a annuler des vibrations |
US8162606B2 (en) * | 2004-08-30 | 2012-04-24 | Lord Corporation | Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations |
US7722322B2 (en) * | 2004-08-30 | 2010-05-25 | Lord Corporation | Computer system and program product for controlling vibrations |
US8267652B2 (en) * | 2004-08-30 | 2012-09-18 | Lord Corporation | Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations |
US8090482B2 (en) * | 2007-10-25 | 2012-01-03 | Lord Corporation | Distributed active vibration control systems and rotary wing aircraft with suppressed vibrations |
FR2938085B1 (fr) * | 2008-11-05 | 2010-12-03 | Airbus France | Procede et dispositif d'attenuation des effets d'une turbulence sur un aeronef |
US8816260B2 (en) | 2010-12-01 | 2014-08-26 | Raytheon Company | Flight-control system for canard-controlled flight vehicles and methods for adaptively limiting acceleration |
US8880242B2 (en) * | 2011-06-06 | 2014-11-04 | The Boeing Company | Structural health management with active control using integrated elasticity measurement |
GB2507295B (en) * | 2012-10-25 | 2020-02-05 | Bae Systems Plc | Control systems for unmanned vehicles |
US9935776B2 (en) | 2012-10-25 | 2018-04-03 | Bae Systems Plc | Control systems for unmanned vehicles |
US9284043B2 (en) * | 2013-11-21 | 2016-03-15 | Aai Corporation | Evaluating aileron deflection while an unmanned aerial vehicle is in flight |
US9797490B2 (en) * | 2014-03-27 | 2017-10-24 | Lcdrives Corp. | High reliability actuator |
US20200363560A1 (en) * | 2019-05-13 | 2020-11-19 | Honeywell International Inc. | Vehicle disturbance measurement and isolation system |
GB2585185B (en) * | 2019-06-24 | 2021-12-08 | Windracers Ltd | Method of controlling an aircraft |
FR3101968B1 (fr) * | 2019-10-14 | 2021-10-08 | Airbus Operations Sas | Système et procédé de commande d’un actionneur d’une gouverne d’un aéronef. |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3051416A (en) * | 1958-11-06 | 1962-08-28 | Honeywell Regulator Co | Maneuver limiting autopilot monitor |
SU126623A1 (ru) * | 1959-05-29 | 1959-11-30 | И.Я. Герасименко | Система гироскопов с взаимной коррекцией и осредненным выходным сигналом |
US3079108A (en) * | 1960-09-14 | 1963-02-26 | Honeywell Regulator Co | Control apparatus |
US3240447A (en) * | 1962-01-10 | 1966-03-15 | North American Aviation Inc | Vehicle control system |
US3221229A (en) * | 1962-01-22 | 1965-11-30 | Massachusetts Inst Technology | Model reference adaptive control system |
US3279725A (en) * | 1963-12-11 | 1966-10-18 | North American Aviation Inc | Flight controller for flexible vehicles |
US3403874A (en) * | 1965-07-20 | 1968-10-01 | Honeywell Inc | Control apparatus for aircraft having fail-safe monitoring gyros |
US3412961A (en) * | 1966-07-27 | 1968-11-26 | Nasa Usa | Means for suppressing or attenuating bending motion of elastic bodies |
US3665217A (en) * | 1969-12-29 | 1972-05-23 | United Aircraft Corp | Flight control disabling system |
-
1972
- 1972-09-22 US US00291441A patent/US3857535A/en not_active Expired - Lifetime
-
1973
- 1973-09-17 GB GB4346073A patent/GB1439782A/en not_active Expired
- 1973-09-21 IT IT52690/73A patent/IT994402B/it active
- 1973-09-21 DE DE19732347673 patent/DE2347673A1/de not_active Withdrawn
- 1973-09-21 JP JP48106852A patent/JPS4970400A/ja active Pending
- 1973-09-21 SE SE7312876A patent/SE389650B/xx unknown
- 1973-09-21 FR FR7333884A patent/FR2200982A5/fr not_active Expired
-
1979
- 1979-04-26 JP JP1979056519U patent/JPS54168000U/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
JPS54168000U (fr) | 1979-11-27 |
IT994402B (it) | 1975-10-20 |
US3857535A (en) | 1974-12-31 |
JPS4970400A (fr) | 1974-07-08 |
DE2347673A1 (de) | 1974-04-04 |
SE389650B (sv) | 1976-11-15 |
GB1439782A (en) | 1976-06-16 |
Similar Documents
Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |