DE69706889D1 - Einrichtung zum Steuern der Höhe eines Flugzeuges - Google Patents

Einrichtung zum Steuern der Höhe eines Flugzeuges

Info

Publication number
DE69706889D1
DE69706889D1 DE69706889T DE69706889T DE69706889D1 DE 69706889 D1 DE69706889 D1 DE 69706889D1 DE 69706889 T DE69706889 T DE 69706889T DE 69706889 T DE69706889 T DE 69706889T DE 69706889 D1 DE69706889 D1 DE 69706889D1
Authority
DE
Germany
Prior art keywords
aircraft
height
controlling
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.)
Expired - Lifetime
Application number
DE69706889T
Other languages
English (en)
Other versions
DE69706889T2 (de
Inventor
Panxika Larramendy
Daniel Delgado
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Aerospatiale Matra
Original Assignee
Aerospatiale Matra
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Aerospatiale Matra filed Critical Aerospatiale Matra
Publication of DE69706889D1 publication Critical patent/DE69706889D1/de
Application granted granted Critical
Publication of DE69706889T2 publication Critical patent/DE69706889T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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
    • G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind
    • G05D1/0623—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind by acting on the pitch
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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
    • G05D1/0615—Rate of change of altitude or depth specially adapted for aircraft to counteract a perturbation, e.g. gust of wind

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (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)
  • Alarm Systems (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
  • Toys (AREA)
DE69706889T 1996-12-02 1997-11-13 Einrichtung zum Steuern der Höhe eines Flugzeuges Expired - Lifetime DE69706889T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9614736A FR2756634B1 (fr) 1996-12-02 1996-12-02 Procede et dispositif pour la detection de rafales de vent vertical et leur application au pilotage d'un aeronef en profondeur

Publications (2)

Publication Number Publication Date
DE69706889D1 true DE69706889D1 (de) 2001-10-25
DE69706889T2 DE69706889T2 (de) 2002-04-11

Family

ID=9498222

Family Applications (2)

Application Number Title Priority Date Filing Date
DE69709838T Expired - Lifetime DE69709838T2 (de) 1996-12-02 1997-11-13 Verfahren und Vorrichtung zur Detektion von Windstössen in einem Luftfahrzeug
DE69706889T Expired - Lifetime DE69706889T2 (de) 1996-12-02 1997-11-13 Einrichtung zum Steuern der Höhe eines Flugzeuges

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE69709838T Expired - Lifetime DE69709838T2 (de) 1996-12-02 1997-11-13 Verfahren und Vorrichtung zur Detektion von Windstössen in einem Luftfahrzeug

Country Status (4)

Country Link
US (1) US5995880A (de)
EP (2) EP0845726B1 (de)
DE (2) DE69709838T2 (de)
FR (1) FR2756634B1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2756541B1 (fr) * 1996-12-02 1999-01-22 Aerospatiale Procede pour la protection d'un aeronef contre les rafales de vent vertical et dispositif de pilotage en profondeur mettant en oeuvre ce procede
US7076292B2 (en) * 2002-04-25 2006-07-11 Medtronic, Inc. Optical communication of neurostimulation-system information
US20060017339A1 (en) * 2004-06-03 2006-01-26 Lalit Chordia Brushless canned motor
DE602006012808D1 (de) * 2006-05-05 2010-04-22 Saab Ab Wirbeldetektion und Messung der Turbulenz
US8508387B2 (en) 2007-05-24 2013-08-13 Aviation Communication & Surveillance Systems Llc Systems and methods for aircraft windshear detection
US8774987B2 (en) * 2007-12-17 2014-07-08 The Boeing Company Vertical gust suppression system for transport aircraft
DE102010026162A1 (de) * 2010-07-06 2012-01-12 Airbus Operations Gmbh Flugzeug mit Tragflügeln und einem System zur Minimierung des Einflusses von instationären Anströmzuständen
EP2615026B1 (de) * 2011-06-10 2018-04-04 Airbus Defence and Space GmbH Verfahren und Vorrichtung zur Minimierung der dynamischen Strukturbelastungen eines Flugzeugs
ES2543633T3 (es) * 2011-07-28 2015-08-20 Airbus Defence and Space GmbH Método y aparato para minimizar las cargas estructurales dinámicas de un avión
ES2633346T3 (es) * 2011-12-20 2017-09-20 Vestas Wind Systems A/S Método de control para una turbina eólica y turbina eólica
US9925846B2 (en) * 2015-05-01 2018-03-27 Fca Us Llc Method of using a glass-mounted humidity/temperature sensor in a vehicle to obtain sun load and control of HVAC system using sun load

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3814912A (en) * 1973-01-04 1974-06-04 Collins Radio Co Gust compensation for angle-of-attack reference aircraft speed control system
US4092716A (en) * 1975-07-11 1978-05-30 Mcdonnell Douglas Corporation Control means and method for controlling an object
FR2334110A1 (fr) * 1975-12-03 1977-07-01 Equip Navigation Aerienne Procede et systeme de detection rapide de gradient de vent
US4043526A (en) * 1976-02-23 1977-08-23 The United States Of America As Represented By The Secretary Of The Navy Autopilot hardover failure protection system
US4314341A (en) * 1980-01-24 1982-02-02 Sperry Corporation Aircraft automatic pilot with automatic emergency descent control apparatus
FR2616902B1 (fr) * 1987-06-18 1989-10-20 Aerospatiale Systeme pour l'elaboration d'un signal d'alarme a bord d'un aeronef en cas de minitornade
FR2624964B1 (fr) * 1987-12-22 1990-06-01 Aerospatiale Systeme de reference de vitesse pour le pilotage d'un aeronef
FR2664231B1 (fr) * 1990-07-04 1992-10-09 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.
FR2668750B1 (fr) * 1990-11-06 1993-01-22 Aerospatiale Systeme pour la commande integree en profondeur et en poussee d'un aeronef.

Also Published As

Publication number Publication date
FR2756634B1 (fr) 1999-01-22
EP0845726B1 (de) 2002-01-02
DE69709838D1 (de) 2002-02-28
EP1004951A3 (de) 2000-07-05
US5995880A (en) 1999-11-30
EP1004951A2 (de) 2000-05-31
FR2756634A1 (fr) 1998-06-05
EP0845726A2 (de) 1998-06-03
EP1004951B1 (de) 2001-09-19
DE69706889T2 (de) 2002-04-11
EP0845726A3 (de) 1999-02-03
DE69709838T2 (de) 2002-08-22

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition