MX2013008799A - Limitacion dinamica de las inclinaciones de las superficies de control de vuelo monobloque durante condiciones de susceptibilidad de entrada en perdida. - Google Patents
Limitacion dinamica de las inclinaciones de las superficies de control de vuelo monobloque durante condiciones de susceptibilidad de entrada en perdida.Info
- Publication number
- MX2013008799A MX2013008799A MX2013008799A MX2013008799A MX2013008799A MX 2013008799 A MX2013008799 A MX 2013008799A MX 2013008799 A MX2013008799 A MX 2013008799A MX 2013008799 A MX2013008799 A MX 2013008799A MX 2013008799 A MX2013008799 A MX 2013008799A
- Authority
- MX
- Mexico
- Prior art keywords
- aircraft
- fcs
- real
- time
- flight control
- Prior art date
Links
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title abstract 2
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
- 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
- B64C5/00—Stabilising surfaces
- B64C5/02—Tailplanes
-
- 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
- G05D1/0066—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for limitation of acceleration or stress
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)
- Traffic Control Systems (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Peptides Or Proteins (AREA)
Abstract
Se describe el método para limitar dinámicamente las inclinaciones de las superficies de control de vuelo (FCS, por sus siglas en inglés) monobloque en un avión. La limitación dinámica de las FCS se activa si una condición de susceptibilidad a la pérdida de sustentación se detecta en el ambiente actual del avión. Se obtiene la velocidad aérea calibrada en tiempo real del avión, el ángulo de incidencia (AQA, por sus siglas en inglés) en tiempo real del avión, y el ángulo de deslizamiento (AOS , por sus siglas en inglés) en tiempo real del avión. Los parámetros de los aviones se pueden obtener a través del cálculo si los valores medidos se juzgan como inadecuados. El ACA y el AOS locales en tiempo real de las FCS se calculan de acuerdo con los parámetros obtenidos del avión. La inclinación de cada una de las FCS, con relación a los valores críticos, es dinámicamente limitada de acuerdo con el AQA y el AOS locales en tiempo real calculados de las FCS. El avión pueden ser un vehículo aéreo sin tripulación (UA , por sus siglas en inglés) y/o un avión de cola en y. La condición de susceptibilidad a la pérdida de sustentación puede incluir las condiciones gélidas.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IL210961A IL210961A0 (en) | 2011-01-30 | 2011-01-30 | Uav dynamic v-tail angle limiter for icy conditions |
IL211060A IL211060A0 (en) | 2011-02-03 | 2011-02-03 | Uav dynamic v-taiol angle limiter for icy conditions |
IL213752A IL213752A (en) | 2011-06-23 | 2011-06-23 | Dynamic restriction of uneven surface gradients for flight control provided exposure to the upright |
PCT/IL2012/050030 WO2012101645A1 (en) | 2011-01-30 | 2012-01-30 | Dynamic limitation of monoblock flight control surfaces inclinations during stall susceptibility conditions |
Publications (1)
Publication Number | Publication Date |
---|---|
MX2013008799A true MX2013008799A (es) | 2014-04-30 |
Family
ID=45876834
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
MX2013008799A MX2013008799A (es) | 2011-01-30 | 2012-01-30 | Limitacion dinamica de las inclinaciones de las superficies de control de vuelo monobloque durante condiciones de susceptibilidad de entrada en perdida. |
Country Status (11)
Country | Link |
---|---|
US (1) | US8958930B2 (es) |
EP (1) | EP2668095B1 (es) |
AU (1) | AU2012210185B2 (es) |
BR (1) | BR112013019078A2 (es) |
CL (1) | CL2013002175A1 (es) |
CO (1) | CO6791574A2 (es) |
ES (1) | ES2569345T3 (es) |
MX (1) | MX2013008799A (es) |
PE (1) | PE20141399A1 (es) |
SG (1) | SG192204A1 (es) |
WO (1) | WO2012101645A1 (es) |
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JP6121663B2 (ja) * | 2012-07-10 | 2017-04-26 | 株式会社タダノ | 作業車両 |
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FR3002203B1 (fr) * | 2013-02-21 | 2015-02-27 | Airbus Operations Sas | Procede et dispositif de detection d'un blocage et/ou d'un embarquement d'une gouverne d'aeronef |
CN103192984B (zh) * | 2013-03-19 | 2015-01-21 | 北京航空航天大学 | 一种适用于跨海空两栖无人机的v型尾翼装置 |
US9506945B2 (en) | 2014-06-10 | 2016-11-29 | Sikorsky Aircraft Corporation | Rotorcraft flight parameter estimation |
US9821903B2 (en) | 2014-07-14 | 2017-11-21 | The Boeing Company | Closed loop control of aircraft control surfaces |
WO2016053408A1 (en) | 2014-10-01 | 2016-04-07 | Sikorsky Aircraft Corporation | Acoustic signature variation of aircraft utilizing a clutch |
CN104401503B (zh) * | 2014-10-23 | 2016-06-01 | 中国运载火箭技术研究院 | 一种适用于多舵面再入飞行器的配平舵偏角确定方法 |
US9650152B2 (en) * | 2014-10-24 | 2017-05-16 | King Abdullah University Of Science And Technology | Flight envelope protection system for unmanned aerial vehicles |
US10343774B2 (en) * | 2015-07-14 | 2019-07-09 | Jeremy Duque | Quad rotor aircraft with fixed wing and variable tail surfaces |
US11905000B2 (en) * | 2016-03-31 | 2024-02-20 | Nikon Corporation | Flying device, electronic device, and program |
US9969503B2 (en) * | 2016-07-21 | 2018-05-15 | Rockwell Collins, Inc. | Head-up display (HUD) stall recovery symbology |
CN106990739A (zh) * | 2017-05-19 | 2017-07-28 | 安徽师范大学 | 一种无人机控制系统 |
CN111874212B (zh) * | 2020-08-06 | 2023-03-10 | 西北工业大学 | 一种实用过失速v尾倾转角自适应控制方法 |
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-
2012
- 2012-01-30 PE PE2013001716A patent/PE20141399A1/es active IP Right Grant
- 2012-01-30 WO PCT/IL2012/050030 patent/WO2012101645A1/en active Application Filing
- 2012-01-30 AU AU2012210185A patent/AU2012210185B2/en not_active Ceased
- 2012-01-30 SG SG2013057708A patent/SG192204A1/en unknown
- 2012-01-30 MX MX2013008799A patent/MX2013008799A/es active IP Right Grant
- 2012-01-30 ES ES12710364.6T patent/ES2569345T3/es active Active
- 2012-01-30 US US13/982,450 patent/US8958930B2/en not_active Expired - Fee Related
- 2012-01-30 BR BR112013019078A patent/BR112013019078A2/pt not_active Application Discontinuation
- 2012-01-30 EP EP12710364.6A patent/EP2668095B1/en not_active Not-in-force
-
2013
- 2013-07-30 CL CL2013002175A patent/CL2013002175A1/es unknown
- 2013-08-23 CO CO13200522A patent/CO6791574A2/es active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
EP2668095A1 (en) | 2013-12-04 |
WO2012101645A4 (en) | 2012-10-26 |
AU2012210185B2 (en) | 2015-10-01 |
PE20141399A1 (es) | 2014-10-24 |
CL2013002175A1 (es) | 2014-04-25 |
EP2668095B1 (en) | 2016-03-30 |
WO2012101645A1 (en) | 2012-08-02 |
BR112013019078A2 (pt) | 2016-10-04 |
SG192204A1 (en) | 2013-09-30 |
CO6791574A2 (es) | 2013-11-14 |
US8958930B2 (en) | 2015-02-17 |
ES2569345T3 (es) | 2016-05-10 |
US20130311011A1 (en) | 2013-11-21 |
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Legal Events
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FG | Grant or registration |