FR3024249B1 - Procede et systeme de commande de vol d'un aeronef. - Google Patents
Procede et systeme de commande de vol d'un aeronef. Download PDFInfo
- Publication number
- FR3024249B1 FR3024249B1 FR1457145A FR1457145A FR3024249B1 FR 3024249 B1 FR3024249 B1 FR 3024249B1 FR 1457145 A FR1457145 A FR 1457145A FR 1457145 A FR1457145 A FR 1457145A FR 3024249 B1 FR3024249 B1 FR 3024249B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- lift
- control
- flight
- apply
- 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
Links
Classifications
-
- 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
-
- 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
- G05D1/04—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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D39/00—Refuelling during flight
-
- 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
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)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
- Le système (1) comprend au moins un élément générateur de portance (16A, 16B) qui est apte à modifier directement la portance de l'aéronef (AC) et des moyens (13, 14, 15, 9, 17A, 17B) pour, lors de l'actionnement par un pilote de l'aéronef d'un manche de commande (3) de l'aéronef (AC) générant une valeur de commande de facteur de charge vertical, définir un ordre de braquage et l'appliquer à une gouverne de profondeur (8) et simultanément définir un ordre de commande et l'appliquer à l'élément générateur de portance (16A, 16B) pour générer une portance directe.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1457145A FR3024249B1 (fr) | 2014-07-24 | 2014-07-24 | Procede et systeme de commande de vol d'un aeronef. |
US14/807,014 US9663219B2 (en) | 2014-07-24 | 2015-07-23 | Method and system for controlling the flight of an aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1457145A FR3024249B1 (fr) | 2014-07-24 | 2014-07-24 | Procede et systeme de commande de vol d'un aeronef. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3024249A1 FR3024249A1 (fr) | 2016-01-29 |
FR3024249B1 true FR3024249B1 (fr) | 2021-04-30 |
Family
ID=52130344
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1457145A Active FR3024249B1 (fr) | 2014-07-24 | 2014-07-24 | Procede et systeme de commande de vol d'un aeronef. |
Country Status (2)
Country | Link |
---|---|
US (1) | US9663219B2 (fr) |
FR (1) | FR3024249B1 (fr) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9878776B2 (en) * | 2014-05-15 | 2018-01-30 | The Boeing Company | System and method for optimizing horizontal tail loads |
FR3024249B1 (fr) * | 2014-07-24 | 2021-04-30 | Airbus Operations Sas | Procede et systeme de commande de vol d'un aeronef. |
US11001378B2 (en) | 2016-08-08 | 2021-05-11 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
AU2016338383A1 (en) | 2015-09-02 | 2018-03-22 | Jetoptera, Inc. | Fluidic propulsive system |
US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
FR3057370B1 (fr) * | 2016-10-11 | 2019-08-23 | Airbus Operations | Procede et systeme de commande de vol d'un aeronef. |
WO2018224565A2 (fr) | 2017-06-07 | 2018-12-13 | Turbulence Solutions Gmbh | Procédé et dispositif de commande pour commander un aéronef par une commande de portance directe améliorée |
CA3068569A1 (fr) | 2017-06-27 | 2019-01-03 | Jetoptera, Inc. | Configuration pour systeme de decollage et d'atterrissage vertical pour vehicules aeriens |
CN109144088A (zh) * | 2018-09-28 | 2019-01-04 | 浙江工业大学 | 一种考虑执行器受限问题的刚体飞行器非奇异固定时间姿态镇定方法 |
CN114167883B (zh) * | 2022-02-11 | 2022-04-15 | 中国空气动力研究与发展中心计算空气动力研究所 | 一种利用喷流进行高空飞行器姿态控制的方法 |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2958483A (en) * | 1953-08-03 | 1960-11-01 | Northrop Corp | Longitudinal stability augmenter |
US2973926A (en) * | 1956-06-19 | 1961-03-07 | Sheldon S L Chang | Control apparatus |
US3082979A (en) * | 1960-08-08 | 1963-03-26 | Honeywell Regulator Co | Control apparatus for dirigible craft |
US3399849A (en) * | 1966-05-11 | 1968-09-03 | Honeywell Inc | Lift and pitch control apparatus for aircraft |
US3653612A (en) * | 1970-09-21 | 1972-04-04 | Bendix Corp | Control wheel force sensor device |
US3658280A (en) * | 1970-10-29 | 1972-04-25 | Mc Donnell Douglas Corp | Altitude and glide slope track controller |
US4261537A (en) * | 1979-02-28 | 1981-04-14 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Velocity vector control system augmented with direct lift control |
US4617633A (en) * | 1984-05-29 | 1986-10-14 | The United States Of America As Represented By The Secretary Of The Air Force | Direct lift command blending |
US4825375A (en) * | 1985-12-23 | 1989-04-25 | Boeing Company | Apparatus and methods for apportioning commands between aircraft flight control surfaces |
US5722620A (en) * | 1995-05-15 | 1998-03-03 | The Boeing Company | Aircraft pitch-axis stability and command augmentation |
US6332105B1 (en) * | 1999-05-21 | 2001-12-18 | Georgia Tech Research Corporation | Neural network based automatic limit prediction and avoidance system and method |
FR2908107B1 (fr) * | 2006-11-06 | 2008-12-19 | Airbus France Sa | Procede et dispositif pour estimer les forces s'exercant sur une surface de controle d'un aeronef. |
DE102011102279A1 (de) * | 2011-05-23 | 2013-08-29 | Airbus Operations Gmbh | Flugzeug mit einer Betankungseinrichtung sowie Verfahren zur Bahnführung eines Flugzeugs bei der Betankung desselben |
US8798817B2 (en) * | 2012-01-31 | 2014-08-05 | Gulfstream Aerospace Corporation | Methods and systems for requesting and retrieving aircraft data during flight of an aircraft |
US9878776B2 (en) * | 2014-05-15 | 2018-01-30 | The Boeing Company | System and method for optimizing horizontal tail loads |
FR3024249B1 (fr) * | 2014-07-24 | 2021-04-30 | Airbus Operations Sas | Procede et systeme de commande de vol d'un aeronef. |
-
2014
- 2014-07-24 FR FR1457145A patent/FR3024249B1/fr active Active
-
2015
- 2015-07-23 US US14/807,014 patent/US9663219B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20160023749A1 (en) | 2016-01-28 |
US9663219B2 (en) | 2017-05-30 |
FR3024249A1 (fr) | 2016-01-29 |
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