CN101171557A - 用于飞行器的辅助起飞方法 - Google Patents
用于飞行器的辅助起飞方法 Download PDFInfo
- Publication number
- CN101171557A CN101171557A CNA2006800159666A CN200680015966A CN101171557A CN 101171557 A CN101171557 A CN 101171557A CN A2006800159666 A CNA2006800159666 A CN A2006800159666A CN 200680015966 A CN200680015966 A CN 200680015966A CN 101171557 A CN101171557 A CN 101171557A
- Authority
- CN
- China
- Prior art keywords
- aircraft
- velocity
- vrref
- tailplane
- correction
- 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.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims description 36
- 238000012937 correction Methods 0.000 claims description 36
- 230000005484 gravity Effects 0.000 claims description 19
- 239000003381 stabilizer Substances 0.000 abstract 2
- 230000001105 regulatory effect Effects 0.000 description 5
- 230000001276 controlling effect Effects 0.000 description 3
- 238000013519 translation Methods 0.000 description 3
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 238000012797 qualification Methods 0.000 description 1
- 230000002269 spontaneous effect Effects 0.000 description 1
Images
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
- G05D1/0083—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots to help an aircraft pilot in the rolling phase
-
- 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
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0661—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off
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)
- Control Of Position Or Direction (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Control Of Electric Motors In General (AREA)
- Vehicle Body Suspensions (AREA)
- Bridges Or Land Bridges (AREA)
- Control And Safety Of Cranes (AREA)
- Attitude Control For Articles On Conveyors (AREA)
- Steering Controls (AREA)
- Macromonomer-Based Addition Polymer (AREA)
- Toys (AREA)
Abstract
Description
Claims (20)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0504662A FR2885706B1 (fr) | 2005-05-10 | 2005-05-10 | Procede d'aide au decollage d'un aeronef. |
FR0504662 | 2005-05-10 |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101171557A true CN101171557A (zh) | 2008-04-30 |
CN100501625C CN100501625C (zh) | 2009-06-17 |
Family
ID=35559480
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CNB2006800159666A Expired - Fee Related CN100501625C (zh) | 2005-05-10 | 2006-05-04 | 用于飞行器的辅助起飞方法 |
Country Status (11)
Country | Link |
---|---|
US (1) | US8014910B2 (zh) |
EP (1) | EP1880259B1 (zh) |
JP (1) | JP4932830B2 (zh) |
CN (1) | CN100501625C (zh) |
AT (1) | ATE406606T1 (zh) |
BR (1) | BRPI0613368A2 (zh) |
CA (1) | CA2607265C (zh) |
DE (1) | DE602006002511D1 (zh) |
FR (1) | FR2885706B1 (zh) |
RU (1) | RU2359867C1 (zh) |
WO (1) | WO2006120321A2 (zh) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102229357A (zh) * | 2011-05-12 | 2011-11-02 | 北京航空航天大学 | 具有安装角可调节平尾的尾翼 |
CN102421666A (zh) * | 2009-03-12 | 2012-04-18 | 空中客车西班牙运营有限责任公司 | 用于提高飞机可控性的系统 |
CN107463182A (zh) * | 2016-06-03 | 2017-12-12 | 空中客车运营简化股份公司 | 用于优化飞行器的起飞参数的方法 |
CN109515685A (zh) * | 2017-09-18 | 2019-03-26 | 波音公司 | 利用安定面和升降舵的飞机起飞配平 |
CN110069070A (zh) * | 2019-05-08 | 2019-07-30 | 成都高威节能科技有限公司 | 一种提高大型飞机起飞过程安全性的方法 |
CN117690332A (zh) * | 2024-02-02 | 2024-03-12 | 北京东方瑞丰航空技术有限公司 | 一种操纵指引方法、装置、设备及介质 |
Families Citing this family (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2942612B1 (fr) * | 2009-03-02 | 2012-09-28 | Airbus France | Procede et dispositif d'optimisation automatique au sol de la configuration aerodynamique d'un avion |
DE102009022602A1 (de) * | 2009-05-26 | 2010-12-02 | Airbus Deutschland Gmbh | Flugzeug mit einem Hochauftriebssystem |
FR2973840B1 (fr) * | 2011-04-07 | 2015-09-18 | Airbus Operations Sas | Procede et dispositif pour la commande du regime des moteurs d'un aeronef au cours d'une phase de decollage. |
US9529010B2 (en) * | 2013-06-17 | 2016-12-27 | Honeywell International Inc. | Flight deck display systems and methods for visually indicating low speed change conditions during takeoff and landing |
GB2516916B (en) * | 2013-08-06 | 2016-09-14 | Lacsop Ltd | Method and apparatus for determining the mass of a body |
US9878776B2 (en) * | 2014-05-15 | 2018-01-30 | The Boeing Company | System and method for optimizing horizontal tail loads |
US9506945B2 (en) | 2014-06-10 | 2016-11-29 | Sikorsky Aircraft Corporation | Rotorcraft flight parameter estimation |
US11001378B2 (en) | 2016-08-08 | 2021-05-11 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
IL257811B (en) | 2015-09-02 | 2022-08-01 | Jetoptera Inc | Pleoidal propulsion system |
US10464668B2 (en) | 2015-09-02 | 2019-11-05 | Jetoptera, Inc. | Configuration for vertical take-off and landing system for aerial vehicles |
EP3448749B1 (en) * | 2016-04-25 | 2020-07-01 | Bombardier Inc. | Aircraft pitch control system with electronically geared elevator |
US11226639B2 (en) * | 2016-09-23 | 2022-01-18 | Yaborã Indústria Aeronáutica S.A. | Enhanced take-off system |
US10479481B2 (en) * | 2016-09-28 | 2019-11-19 | The Boeing Company | Process and machine for reducing a drag component of a horizontal stabilizer on an aircraft |
WO2019005937A1 (en) | 2017-06-27 | 2019-01-03 | Jetoptera, Inc. | CONFIGURATION FOR A VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES |
EP3489140B1 (en) * | 2017-11-27 | 2022-02-23 | Airbus Operations, S.L. | Aircraft system with asisted taxi, take off, and climbing |
US11046418B2 (en) * | 2018-09-25 | 2021-06-29 | The Boeing Company | Articulated empennage with ruddervator |
US11292579B2 (en) | 2018-09-25 | 2022-04-05 | The Boeing Company | Articulated empennage with rudder and elevator |
US20210405658A1 (en) * | 2020-06-25 | 2021-12-30 | Embraer S.A. | Longitudinal trim control movement during takeoff rotation |
RU2761687C1 (ru) * | 2021-05-20 | 2021-12-13 | Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") | Способ управления самолётом при выводе на большие углы атаки |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3522729A (en) * | 1968-01-22 | 1970-08-04 | Sperry Rand Corp | Airspeed command system |
US4261533A (en) * | 1978-06-26 | 1981-04-14 | Dynamic Engineering, Inc. | All-axis control of aircraft in ultra deep stall |
US4825375A (en) * | 1985-12-23 | 1989-04-25 | Boeing Company | Apparatus and methods for apportioning commands between aircraft flight control surfaces |
FR2609545B1 (fr) * | 1987-01-08 | 1991-01-04 | Aerospatiale | Procede et systeme pour la determination de la position longitudinale du centre de gravite d'un aeronef pourvu d'un empennage horizontal reglable et application a la surveillance dudit centre de gravite au voisinage du foyer de l'aeronef |
FR2609546B1 (fr) * | 1987-01-08 | 1991-01-04 | Aerospatiale | Procede et systeme pour la determination de la position longitudinale du centre de gravite d'un aeronef pourvu d'un empennage horizontal reglable |
US5722620A (en) * | 1995-05-15 | 1998-03-03 | The Boeing Company | Aircraft pitch-axis stability and command augmentation |
FR2817535B1 (fr) | 2000-12-06 | 2003-03-21 | Eads Airbus Sa | Systeme pour commander automatiquement des dispositifs hypersustentateurs d'un aeronef durant le decollage |
FR2826469B1 (fr) | 2001-06-25 | 2003-10-24 | Eads Airbus Sa | Procede et dispositif pour commander au moins une surface aerodynamique de profondeur d'un avion lors d'un decollage |
FR2864023B1 (fr) * | 2003-12-19 | 2006-03-03 | Airbus France | Procede pour ameliorer la manoeuvrabilite d'un aeronef lors d'une ressource. |
FR2865999B1 (fr) * | 2004-02-06 | 2006-04-07 | Airbus France | Procede pour ameliorer l'atterrissage d'un aeronef. |
FR2868852B1 (fr) * | 2004-04-09 | 2006-06-30 | Airbus France Sas | Procede pour assurer la securite d'un aeronef volant horizontalement a faible vitesse |
FR2869588B1 (fr) * | 2004-04-28 | 2006-07-14 | Airbus France Sas | Procede d'aide au decollage d'un aeronef. |
ES2300184B1 (es) * | 2006-04-28 | 2009-05-01 | Airbus España, S.L. | Disposicion para acoplar un pivote de acoplamiento para un estabilizador horizontal trimable al fuselaje de cola de una aeronave. |
US7764201B2 (en) * | 2008-11-26 | 2010-07-27 | Red Hat, Inc. | Table management for LZW with fixed-size tables |
-
2005
- 2005-05-10 FR FR0504662A patent/FR2885706B1/fr not_active Expired - Fee Related
-
2006
- 2006-05-04 CA CA2607265A patent/CA2607265C/fr not_active Expired - Fee Related
- 2006-05-04 BR BRPI0613368-1A patent/BRPI0613368A2/pt not_active IP Right Cessation
- 2006-05-04 RU RU2007145478/11A patent/RU2359867C1/ru not_active IP Right Cessation
- 2006-05-04 EP EP06743759A patent/EP1880259B1/fr not_active Not-in-force
- 2006-05-04 CN CNB2006800159666A patent/CN100501625C/zh not_active Expired - Fee Related
- 2006-05-04 WO PCT/FR2006/001000 patent/WO2006120321A2/fr active IP Right Grant
- 2006-05-04 US US11/913,395 patent/US8014910B2/en not_active Expired - Fee Related
- 2006-05-04 JP JP2008510609A patent/JP4932830B2/ja not_active Expired - Fee Related
- 2006-05-04 DE DE602006002511T patent/DE602006002511D1/de active Active
- 2006-05-04 AT AT06743759T patent/ATE406606T1/de not_active IP Right Cessation
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102421666A (zh) * | 2009-03-12 | 2012-04-18 | 空中客车西班牙运营有限责任公司 | 用于提高飞机可控性的系统 |
CN102421666B (zh) * | 2009-03-12 | 2015-09-02 | 空中客车西班牙运营有限责任公司 | 用于提高飞机可控性的系统 |
CN102229357A (zh) * | 2011-05-12 | 2011-11-02 | 北京航空航天大学 | 具有安装角可调节平尾的尾翼 |
CN102229357B (zh) * | 2011-05-12 | 2013-07-03 | 北京航空航天大学 | 具有安装角可调节平尾的尾翼 |
CN107463182A (zh) * | 2016-06-03 | 2017-12-12 | 空中客车运营简化股份公司 | 用于优化飞行器的起飞参数的方法 |
CN107463182B (zh) * | 2016-06-03 | 2022-03-29 | 空中客车运营简化股份公司 | 用于优化飞行器的起飞参数的方法 |
CN109515685A (zh) * | 2017-09-18 | 2019-03-26 | 波音公司 | 利用安定面和升降舵的飞机起飞配平 |
TWI774802B (zh) * | 2017-09-18 | 2022-08-21 | 美商波音公司 | 用於利用安定面和升降舵進行飛機起飛配平之系統和方法 |
CN110069070A (zh) * | 2019-05-08 | 2019-07-30 | 成都高威节能科技有限公司 | 一种提高大型飞机起飞过程安全性的方法 |
CN110069070B (zh) * | 2019-05-08 | 2022-01-18 | 成都高威节能科技有限公司 | 一种提高大型飞机起飞过程安全性的方法 |
CN117690332A (zh) * | 2024-02-02 | 2024-03-12 | 北京东方瑞丰航空技术有限公司 | 一种操纵指引方法、装置、设备及介质 |
CN117690332B (zh) * | 2024-02-02 | 2024-04-26 | 北京东方瑞丰航空技术有限公司 | 一种操纵指引方法、装置、设备及介质 |
Also Published As
Publication number | Publication date |
---|---|
CN100501625C (zh) | 2009-06-17 |
ATE406606T1 (de) | 2008-09-15 |
CA2607265A1 (fr) | 2006-11-16 |
CA2607265C (fr) | 2013-10-22 |
RU2359867C1 (ru) | 2009-06-27 |
EP1880259B1 (fr) | 2008-08-27 |
JP4932830B2 (ja) | 2012-05-16 |
FR2885706A1 (fr) | 2006-11-17 |
EP1880259A2 (fr) | 2008-01-23 |
US8014910B2 (en) | 2011-09-06 |
JP2008540229A (ja) | 2008-11-20 |
DE602006002511D1 (de) | 2008-10-09 |
BRPI0613368A2 (pt) | 2011-01-11 |
WO2006120321A2 (fr) | 2006-11-16 |
US20080188999A1 (en) | 2008-08-07 |
FR2885706B1 (fr) | 2007-06-15 |
WO2006120321A3 (fr) | 2007-02-22 |
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Legal Events
Date | Code | Title | Description |
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C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
ASS | Succession or assignment of patent right |
Owner name: AIRBUS OPERATIONS GMBH Free format text: FORMER OWNER: AIRBUS FRANCE Effective date: 20120111 |
|
C41 | Transfer of patent application or patent right or utility model | ||
TR01 | Transfer of patent right |
Effective date of registration: 20120111 Address after: France Toulouse Patentee after: Airbus Operations S.A.S. Address before: Toulouse, France Patentee before: Airbus France Effective date of registration: 20120111 Address after: Toulouse, France Patentee after: Airbus France Address before: France Toulouse Patentee before: Airbus France |
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CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20090617 Termination date: 20200504 |
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CF01 | Termination of patent right due to non-payment of annual fee |