PE20141399A1 - Limitacion dinamica de inclinaciones de superficies de control de vuelo monobloque durante condiciones de susceptibilidad a entrada en perdida - Google Patents
Limitacion dinamica de inclinaciones de superficies de control de vuelo monobloque durante condiciones de susceptibilidad a entrada en perdidaInfo
- Publication number
- PE20141399A1 PE20141399A1 PE2013001716A PE2013001716A PE20141399A1 PE 20141399 A1 PE20141399 A1 PE 20141399A1 PE 2013001716 A PE2013001716 A PE 2013001716A PE 2013001716 A PE2013001716 A PE 2013001716A PE 20141399 A1 PE20141399 A1 PE 20141399A1
- Authority
- PE
- Peru
- Prior art keywords
- aircraft
- fcs
- susceptibility
- inclination
- 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)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Traffic Control Systems (AREA)
- Peptides Or Proteins (AREA)
Abstract
REFERIDO A UN METODO PARA LIMITAR DINAMICAMENTE LAS INCLINACIONES DE LAS SUPERFICIES DE CONTROL DE VUELO (FCS) MONOBLOQUE EN UNA AERONAVE. LA LIMITACION DINAMICA DE LAS FCS SE ACTIVA SI SE DETECTA UNA CONDICION DE SUSCEPTIBILIDAD A ENTRADA EN PERDIDA EN EL ENTORNO ACTUAL DE LA AERONAVE. SE OBTIENE LA VELOCIDAD ANEMOMETRICA CALIBRADA EN TIEMPO REAL DE LA AERONAVE, EL ANGULO DE ATAQUE (AOA) EN TIEMPO REAL DE LA AERONAVE Y EL ANGULO DE RESBALAMIENTO LATERAL (AOS). LOS PARAMETROS DE LA AERONAVE SE PUEDEN OBTENER POR MEDIO DE ESTIMACION SI LOS VALORES MEDIDOS SE CONSIDERAN INADECUADOS. EL AOA Y AOS LOCALES EN TIEMPO REAL DE LAS FCS SE CALCULAN CON BASE EN LOS PARAMETROS OBTENIDOS DE LA AERONAVE. LA INCLINACION DE LAS FCS RELATIVAS A LOS VALORES CRITICOS SE LIMITA DINAMICAMENTE DE ACUERDO AL AOA Y AOS LOCALES EN TIEMPO REAL DE LAS FCS. LA AERONAVE PUEDE SER UN VEHICULO AEREO NO TRIPULADO (UAV) O UNA AERONAVE CON COLA EN V. LA CONDICION DE SUSCEPTIBILIDAD A ENTRADA EN PERDIDA PUEDE INCLUIR CONDICIONES GELIDAS
Applications Claiming Priority (3)
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 |
Publications (1)
Publication Number | Publication Date |
---|---|
PE20141399A1 true PE20141399A1 (es) | 2014-10-24 |
Family
ID=45876834
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PE2013001716A PE20141399A1 (es) | 2011-01-30 | 2012-01-30 | Limitacion dinamica de inclinaciones de superficies de control de vuelo monobloque durante condiciones de susceptibilidad a 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) |
Families Citing this family (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6121663B2 (ja) * | 2012-07-10 | 2017-04-26 | 株式会社タダノ | 作業車両 |
US8949090B2 (en) * | 2013-01-28 | 2015-02-03 | The Boeing Company | Formation flight control |
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 |
US20170267338A1 (en) | 2014-10-01 | 2017-09-21 | 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 |
WO2016087949A1 (en) * | 2014-10-24 | 2016-06-09 | 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 |
JP7120002B2 (ja) * | 2016-03-31 | 2022-08-17 | 株式会社ニコン | 飛行装置 |
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 |
CN115719557A (zh) * | 2022-11-22 | 2023-02-28 | 安胜(天津)飞行模拟系统有限公司 | 一种飞机模拟机全失速改出训练方法 |
Family Cites Families (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5000404A (en) * | 1987-08-13 | 1991-03-19 | Grumman Aerospace Corporation | Aircraft precision approach control system |
US5083279A (en) * | 1990-05-09 | 1992-01-21 | Honeywell, Inc. | Canard based high angle of attack air data sensor |
US5299455A (en) * | 1992-03-27 | 1994-04-05 | Mangalam Siva M | Method and instrumentation system for measuring airspeed and flow angle |
US5796612A (en) * | 1992-11-18 | 1998-08-18 | Aers/Midwest, Inc. | Method for flight parameter monitoring and control |
US5595357A (en) * | 1994-07-05 | 1997-01-21 | The B. F. Goodrich Company | Aircraft stall warning system |
US5826834A (en) | 1994-10-19 | 1998-10-27 | Honeywell Inc. | Self adaptive limiter for automatic control of approach and landing |
US5746392A (en) * | 1995-05-15 | 1998-05-05 | The Boeing Company | Autopilot/flight director underspeed protection system |
US6169496B1 (en) * | 1998-12-09 | 2001-01-02 | Exigent International, Inc. | Banked flight stall warning device and method |
US6089503A (en) * | 1999-01-15 | 2000-07-18 | Northrop Grumman Corp | Selectively rotatable and torsionally flexible aerodynamic control apparatus |
US6246929B1 (en) * | 1999-06-16 | 2001-06-12 | Lockheed Martin Corporation | Enhanced stall and recovery control system |
US6273370B1 (en) * | 1999-11-01 | 2001-08-14 | Lockheed Martin Corporation | Method and system for estimation and correction of angle-of-attack and sideslip angle from acceleration measurements |
US6711477B1 (en) * | 2002-08-29 | 2004-03-23 | Lockheed Corp | Automatic flight envelope protection for uninhabited air vehicles: method for determining point in flight envelope |
US6928341B2 (en) * | 2003-05-13 | 2005-08-09 | The Boeing Company | Computational air data system for angle-of-attack and angle-of-sideslip |
JP4685866B2 (ja) * | 2004-06-02 | 2011-05-18 | ロックウェル コリンズ コントロール テクノロジーズ,インコーポレーテッド | 動的システムを制御するためのシステムおよび方法 |
DE102005020660B4 (de) * | 2005-05-03 | 2007-10-11 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren zur Reduzierung der Turbulenz- und Böeneinflüsse auf das Flugverhalten von Luftfahrzeugen und Steuerungseinrichtung hierfür |
DE102005032849B4 (de) * | 2005-07-14 | 2009-09-03 | Eads Deutschland Gmbh | Vorrichtung und Verfahren zum Überführen eines Flugzeugs von einem außerhalb eines zulässigen Flugzustandsbereichs in einen innerhalb des zulässigen Flugzustandsbereichs liegenden Flugzustand |
US7997528B2 (en) * | 2006-01-18 | 2011-08-16 | Aereon Corporation | Reducing runway requirement for aircraft |
US7706932B2 (en) * | 2006-11-30 | 2010-04-27 | Instituto Nacional de Tecnica Aeroespacial “Estaban Terradas” | Method for controlling control parameters in an air vehicle and system of controlling an air vehicle |
US8620495B2 (en) * | 2006-12-19 | 2013-12-31 | Rosemount Aerospace Inc. | Air data stall protection system |
US8014906B2 (en) * | 2006-12-19 | 2011-09-06 | The Boeing Company | Multi-axis trim processing |
US8113462B2 (en) * | 2007-01-08 | 2012-02-14 | Israel Aerospace Industries, Ltd. | Low-drag swept wings |
US7959111B1 (en) * | 2007-03-29 | 2011-06-14 | Rockwell Collins, Inc. | Angle of attack automated flight control system vertical control function |
US8165733B2 (en) * | 2007-09-04 | 2012-04-24 | Embraer S.A. | Stall, buffeting, low speed and high attitude protection system |
US20090090817A1 (en) * | 2007-10-09 | 2009-04-09 | Monka Gary H | Aircraft configuration, gas turbine engine, controller and trim system for neutralizing pitching moments with power changes |
FR2922301B1 (fr) * | 2007-10-11 | 2010-02-26 | Airbus | Dispositif et procede d'estimation d'un angle de derapage d'un aeronef |
US8774987B2 (en) * | 2007-12-17 | 2014-07-08 | The Boeing Company | Vertical gust suppression system for transport aircraft |
ES2356788B1 (es) * | 2007-12-18 | 2012-02-22 | Airbus Operations, S.L. | Método y sistema para un cálculo rápido de las fuerzas aerodinámicas en una aeronave. |
IT1392259B1 (it) * | 2008-12-11 | 2012-02-22 | Alenia Aeronautica Spa | Procedimento di stima dell'angolo di incidenza e dell'angolo di derapata di un aeromobile |
FR2951434B1 (fr) * | 2009-10-20 | 2012-03-09 | Airbus Operations Sas | Empennage horizontal d'aeronef muni d'un apex de bord d'attaque |
US8359128B1 (en) * | 2011-07-13 | 2013-01-22 | The Boeing Company | Solar energy collection flight path management system for aircraft |
FR2983965B1 (fr) * | 2011-12-12 | 2014-07-04 | Thales Sa | Sonde de mesure d'incidence locale et procede mettant en oeuvre la sonde |
-
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 MX MX2013008799A patent/MX2013008799A/es active IP Right Grant
- 2012-01-30 US US13/982,450 patent/US8958930B2/en not_active Expired - Fee Related
- 2012-01-30 EP EP12710364.6A patent/EP2668095B1/en not_active Not-in-force
- 2012-01-30 BR BR112013019078A patent/BR112013019078A2/pt not_active Application Discontinuation
- 2012-01-30 AU AU2012210185A patent/AU2012210185B2/en not_active Ceased
- 2012-01-30 ES ES12710364.6T patent/ES2569345T3/es active Active
- 2012-01-30 SG SG2013057708A patent/SG192204A1/en unknown
-
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 |
---|---|
WO2012101645A1 (en) | 2012-08-02 |
US20130311011A1 (en) | 2013-11-21 |
AU2012210185B2 (en) | 2015-10-01 |
ES2569345T3 (es) | 2016-05-10 |
SG192204A1 (en) | 2013-09-30 |
BR112013019078A2 (pt) | 2016-10-04 |
CL2013002175A1 (es) | 2014-04-25 |
EP2668095A1 (en) | 2013-12-04 |
CO6791574A2 (es) | 2013-11-14 |
WO2012101645A4 (en) | 2012-10-26 |
US8958930B2 (en) | 2015-02-17 |
MX2013008799A (es) | 2014-04-30 |
EP2668095B1 (en) | 2016-03-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
PE20141399A1 (es) | Limitacion dinamica de inclinaciones de superficies de control de vuelo monobloque durante condiciones de susceptibilidad a entrada en perdida | |
EP2390670A3 (en) | Wind estimation for an unmanned aerial vehicle | |
EP4006683A4 (en) | WIND SPEED MEASUREMENT AND CALCULATION METHODS, WIND SPEED ESTIMATOR AND UNMANNED AIRCRAFT | |
ATE391896T1 (de) | Verfahren und vorrichtung zur sollgeschwindigkeitsberechnung für ein luftfahrzeug | |
EP2474812A3 (en) | Flight management system with integrated tactical commands for use with an aircraft and method of operating same | |
ES2523701R1 (es) | Sistema y procedimiento de determinación de los parámetros operacionales de una aeronave y mejora de la operación de la aeronave | |
WO2009082785A8 (en) | A method and system of controlling air traffic | |
IN2012DE00463A (es) | ||
ES2720879T3 (es) | Sistema de gestión para vehículos aéreos no tripulados | |
WO2015073103A3 (en) | Unmanned vehicle searches | |
WO2016055589A3 (fr) | Détermination d'une vitesse optimale pour un véhicule automobile approchant d'un feu tricolore | |
ATE430352T1 (de) | Gleitanflugverfahren für maximale vorhersagbarkeit | |
WO2013131072A3 (en) | Real-time aircraft status detection system and method | |
EP2071542A3 (en) | Determination of an air traffic control delay factor | |
JP2013173522A5 (es) | ||
WO2018089071A3 (en) | Wireless communication enhancements for unmanned aerial vehicle communications | |
EP2177966A3 (en) | Systems and methods for unmanned aerial vehicle navigation | |
GB201116961D0 (en) | Fast calibration for lidars | |
EP2607872A3 (en) | Apparatus for determining an air temperature | |
MX359042B (es) | Dispositivo de cálculo de la ruta de desplazamiento. | |
EP2664484A3 (en) | Traveling range calculation apparatus, method and program | |
EP2492892A3 (en) | Aircraft systems and methods for providing exhaust warnings | |
EP3415868A3 (en) | Method and system for autonomous generation of shortest lateral paths for unmanned aerial systems | |
FR2948774B1 (fr) | Radar de detection de cibles aeriennes equipant un aeronef notamment pour l'evitement d'obstacles en vol | |
MY166204A (en) | Flat blade-shaped cutting blade and green sheet cutting blade |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG | Grant, registration |