FR2118504A5 - - Google Patents

Info

Publication number
FR2118504A5
FR2118504A5 FR7144167A FR7144167A FR2118504A5 FR 2118504 A5 FR2118504 A5 FR 2118504A5 FR 7144167 A FR7144167 A FR 7144167A FR 7144167 A FR7144167 A FR 7144167A FR 2118504 A5 FR2118504 A5 FR 2118504A5
Authority
FR
France
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
Application number
FR7144167A
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.)
Unisys Group Services Ltd
Sperry Corp
Original Assignee
Sperry Rand Ltd
Sperry Rand Corp
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 Sperry Rand Ltd, Sperry Rand Corp filed Critical Sperry Rand Ltd
Application granted granted Critical
Publication of FR2118504A5 publication Critical patent/FR2118504A5/fr
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06G—ANALOGUE COMPUTERS
    • G06G7/00—Devices in which the computing operation is performed by varying electric or magnetic quantities
    • G06G7/48—Analogue computers for specific processes, systems or devices, e.g. simulators
    • G06G7/78—Analogue computers for specific processes, systems or devices, e.g. simulators for direction-finding, locating, distance or velocity measuring, or navigation systems
    • 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
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06G—ANALOGUE COMPUTERS
    • G06G7/00—Devices in which the computing operation is performed by varying electric or magnetic quantities
    • G06G7/48—Analogue computers for specific processes, systems or devices, e.g. simulators
    • G06G7/70—Analogue computers for specific processes, systems or devices, e.g. simulators for vehicles, e.g. to determine permissible loading of ships, centre of gravity, necessary fuel

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Computer Hardware Design (AREA)
  • General Physics & Mathematics (AREA)
  • Mathematical Physics (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Traffic Control Systems (AREA)
  • Gyroscopes (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Control Of Velocity Or Acceleration (AREA)
FR7144167A 1970-12-10 1971-12-09 Expired FR2118504A5 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US9679670A 1970-12-10 1970-12-10

Publications (1)

Publication Number Publication Date
FR2118504A5 true FR2118504A5 (fr) 1972-07-28

Family

ID=22259112

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7144167A Expired FR2118504A5 (fr) 1970-12-10 1971-12-09

Country Status (6)

Country Link
US (1) US3691356A (fr)
CA (1) CA972463A (fr)
DE (1) DE2161401C2 (fr)
FR (1) FR2118504A5 (fr)
GB (3) GB1374101A (fr)
IT (1) IT945368B (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2435392A1 (fr) * 1978-09-11 1980-04-04 Lockheed Corp Systeme de commande de la vitesse de croisiere d'un avion
EP0427345A2 (fr) * 1989-11-10 1991-05-15 Fokker Aircraft B.V. Commande automatique de la vitesse d'approche pour un avion
FR2894045A1 (fr) * 2005-11-28 2007-06-01 Airbus France Sas Procede de controle de parametres de decollage ou d'atterrissage et dispositif associe

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US3813063A (en) * 1972-07-21 1974-05-28 United Aircraft Corp Automatic aircraft engine pressure ratio control system
US3822047A (en) * 1972-12-14 1974-07-02 Collins Radio Co Takeoff and go-around climb-out profile pitch command formulation for aircraft
US3927306A (en) * 1974-03-29 1975-12-16 Sperry Rand Corp Helicopter flight path control
US3981442A (en) * 1975-08-15 1976-09-21 Sperry Rand Corporation Aircraft engine automatic throttle control with automatic gain programming system
USRE31159E (en) * 1976-07-06 1983-02-22 Societe Francaise d'Equipement pour la Navigation Aerienne Flying method and system using total energy for an aircraft
US4071893A (en) * 1976-07-06 1978-01-31 Societe Francaise D'equipements Pour La Navigation Aerienne Flying method and system using total power for an aircraft
US4159088A (en) * 1977-01-03 1979-06-26 The Boeing Company System for reducing aircraft fuel consumption
US4110605A (en) * 1977-02-25 1978-08-29 Sperry Rand Corporation Weight and balance computer apparatus for aircraft
US4095271A (en) * 1977-04-20 1978-06-13 Sundstrand Data Control, Inc. Aircraft pitch attitude signal generator
US4155525A (en) * 1977-10-25 1979-05-22 The Boeing Company Maneuver detector circuit for use in autothrottle control systems having thrust and flight path control decoupling
US4189119A (en) * 1977-11-22 1980-02-19 The Boeing Company Turbulence compensated throttle control system
US4189118A (en) * 1977-11-22 1980-02-19 The Boeing Company Shear detection and compensation circuit for aircraft throttle control system
US4325123A (en) * 1978-07-28 1982-04-13 The Boeing Company Economy performance data avionic system
US4569021A (en) * 1978-08-07 1986-02-04 The Boeing Company Full flight regime autothrottle control system
US4220993A (en) * 1978-09-15 1980-09-02 Sperry Corporation Engine throttle control system
US4266743A (en) * 1979-02-28 1981-05-12 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Pitch attitude stabilization system utilizing engine pressure ratio feedback signals
US4347572A (en) * 1979-11-02 1982-08-31 The Boeing Company Method and apparatus for an aircraft climb-out guidance system
US4357663A (en) * 1979-12-03 1982-11-02 The Boeing Company Method and apparatus for aircraft pitch and thrust axes control
JPS57191198A (en) * 1981-03-02 1982-11-24 Sperry Rand Corp Detecting and alarming device for window shear
US4494210A (en) * 1981-12-21 1985-01-15 Sperry Corporation Enroute weight computer for aircraft
US4490793A (en) * 1981-12-21 1984-12-25 Sperry Corporation Cruise speed control for aircraft performance management system
US4471439A (en) * 1982-09-20 1984-09-11 The Boeing Company Method and apparatus for aircraft pitch and thrust axes control
US4536843A (en) * 1982-09-30 1985-08-20 The Boeing Company Total energy based flight control system
US4609988A (en) * 1983-03-17 1986-09-02 Sperry Corporation Automatic prediction and capture of a preselected altitude for aircraft
US4916447A (en) * 1983-05-13 1990-04-10 Sundstrand Data Control, Inc. Warning system for aircraft landing with landing gear up
US4951047A (en) * 1983-05-13 1990-08-21 Sunstrand Data Control, Inc. Negative climb after take-off warning system
US4939513A (en) * 1983-05-13 1990-07-03 Sundstrand Data Control, Inc. System for alerting a pilot of a dangerous flight profile during low level maneuvering
US4590475A (en) * 1983-10-24 1986-05-20 The United States Of America As Represented By The Secretary Of The Army Stall avoidance system for aircraft
US4594592A (en) * 1984-01-09 1986-06-10 Greene Leonard M Airplane safe take-off rotation indicator
US4589616A (en) * 1984-01-24 1986-05-20 Sperry Corporation Cruise airspeed control of aircraft altitude capture
US4672548A (en) * 1984-09-17 1987-06-09 Sperry Corporation Speed capture in climb for aircraft
US4723214A (en) * 1985-02-15 1988-02-02 Grumman Aerospace Corporation Automatic camber control
US4774670A (en) * 1985-04-29 1988-09-27 Lockheed Corporation Flight management system
US4728951A (en) * 1985-10-16 1988-03-01 Honeywell Inc. Vertical windshear detection for aircraft
US4764872A (en) * 1986-07-16 1988-08-16 Honeywell Inc. Vertical flight path and airspeed control system for aircraft
US5047942A (en) * 1987-08-06 1991-09-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Airplane takeoff and landing performance monitoring system
US5000404A (en) * 1987-08-13 1991-03-19 Grumman Aerospace Corporation Aircraft precision approach control system
US5039037A (en) * 1989-09-11 1991-08-13 The Boeing Company Throttle control system having manual and automatic modes of operation
US5103224A (en) * 1990-02-16 1992-04-07 Ady Arad Aircraft takeoff monitoring system
DE4036241A1 (de) * 1990-11-14 1992-05-21 Joerg Golombek Verfahren und vorrichtung zur ermittlung und verwertung der physikalischen daten eines im betrieb befindlichen fahrzeugmodells
US5315819A (en) * 1991-09-17 1994-05-31 Allied-Signal Inc. Power management system for turbine engines
US5337982A (en) * 1991-10-10 1994-08-16 Honeywell Inc. Apparatus and method for controlling the vertical profile of an aircraft
US5299765A (en) * 1991-12-23 1994-04-05 The Boeing Company Apparatus and methods for controlling aircraft thrust during a climb
US5330131A (en) * 1992-05-28 1994-07-19 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Engines-only flight control system
US6002972A (en) * 1992-11-18 1999-12-14 Aers/Midwest, Inc. Method and apparatus for measuring forces based upon differential pressure between surfaces of an aircraft
US5796612A (en) * 1992-11-18 1998-08-18 Aers/Midwest, Inc. Method for flight parameter monitoring and control
US5457630A (en) * 1992-11-18 1995-10-10 Aers/Midwest, Inc. System for onboard lift analysis and apparatus therefor
US5746392A (en) * 1995-05-15 1998-05-05 The Boeing Company Autopilot/flight director underspeed protection system
US5833177A (en) * 1995-05-15 1998-11-10 The Boeing Company Autopilot/flight director overspeed protection system
US6691004B2 (en) * 1995-07-31 2004-02-10 Honeywell International, Inc. Method for determining a currently obtainable climb gradient of an aircraft
US6186447B1 (en) * 1997-11-10 2001-02-13 The Boeing Company Autothrottle retard rate control system
US6169496B1 (en) * 1998-12-09 2001-01-02 Exigent International, Inc. Banked flight stall warning device and method
US6886786B1 (en) * 2003-10-10 2005-05-03 The Boeing Company Engine thrust management—new design architecture
FR2861198B1 (fr) * 2003-10-20 2006-01-20 Airbus France Procede et dispositif d'optimisation de la quantite de carburant transfere sur un aeronef, lors d'au moins un transfert de carburant en vol.
FR2869588B1 (fr) * 2004-04-28 2006-07-14 Airbus France Sas Procede d'aide au decollage d'un aeronef.
FR2869997B1 (fr) * 2004-05-04 2006-06-23 Commissariat Energie Atomique Accelerometre en boucle fermee avec detection d'erreur
GB0415618D0 (en) * 2004-07-13 2004-08-18 Rolls Royce Plc Aircraft takeoff
US7364121B2 (en) * 2005-03-14 2008-04-29 The Boeing Company Methods and systems for automatically controlling aircraft takeoff rolls
US7406369B2 (en) * 2005-04-18 2008-07-29 Greene Leonard M Ground effects compensated angle of attack command system and method
FR2894046B1 (fr) * 2005-11-28 2008-02-15 Airbus France Sas Procede de detection d'une erreur d'entree d'un des parametres de decollage dans un systeme de management de vol
US9085371B2 (en) * 2008-11-20 2015-07-21 The Boeing Company Automatic throttle roll angle compensation
US9058040B2 (en) * 2009-02-27 2015-06-16 The Boeing Company Automatic pilot pitch angle compensation
US20110040431A1 (en) * 2009-08-11 2011-02-17 Honeywell International Inc. Automated take off control system and method
FR2950165B1 (fr) * 2009-09-16 2012-08-17 Airbus Operations Sas Procede et systeme pour l'amelioration des performances d'un aeronef au decollage
JP5550398B2 (ja) * 2010-03-18 2014-07-16 三菱重工業株式会社 舵面故障・損傷検出装置
US9671783B2 (en) * 2010-05-25 2017-06-06 Airbus Operations (Sas) Automatic method and device for aiding the piloting of an airplane
US8729443B2 (en) * 2010-09-13 2014-05-20 Raytheon Company Projectile and method that include speed adjusting guidance and propulsion systems
RU2455201C1 (ru) * 2010-10-28 2012-07-10 Открытое акционерное общество "Российская самолетостроительная корпорация "МиГ" Способ управления самолетом с учетом стабилизации заданной скорости полета
US8742973B1 (en) * 2011-09-22 2014-06-03 Rockwell Collins, Inc. System and method of determining increased turbulence susceptibility with elapsed flight time
US8781653B2 (en) * 2012-01-11 2014-07-15 The Boeing Company Quiet landing attitude modifier for airplane
FR2996254B1 (fr) * 2012-10-03 2014-09-12 Snecma Methode de surveillance d'un defaut de poussee d'un turboreacteur d'aeronef
JP6114075B2 (ja) * 2013-03-07 2017-04-12 三菱航空機株式会社 航空機の警報システム、及び、航空機
FR3008499B1 (fr) * 2013-07-12 2015-08-07 Airbus Operations Sas Procede et dispositif d'affichage en temps reel d'une consigne d'assiette sur un aeronef lors d'un pilotage manuel.
US9828113B2 (en) 2013-11-05 2017-11-28 Safe Flight Instrument Corporation Tailstrike warning system
US9546003B2 (en) 2014-03-14 2017-01-17 Safe Flight Instrument Corporation Deflare pitch command
US9346552B2 (en) 2014-04-11 2016-05-24 Safe Flight Instrument Corporation Autothrottle retard control
WO2016048437A1 (fr) * 2014-09-23 2016-03-31 Sikorsky Aircraft Corporation Compensation d'état initial de rotor pour un giravion
US20170008639A1 (en) 2015-07-08 2017-01-12 Safe Flight Instrument Corporation Aircraft turbulence detection
US10261518B2 (en) * 2015-11-12 2019-04-16 Embraer S.A. Method and apparatus for protecting aircraft maximum lift capability
US9862499B2 (en) * 2016-04-25 2018-01-09 Airbus Operations (S.A.S.) Human machine interface for displaying information relative to the energy of an aircraft
US10302451B1 (en) * 2018-02-20 2019-05-28 The Boeing Company Optimizing climb performance during takeoff using variable initial pitch angle target
US11066189B2 (en) * 2018-12-07 2021-07-20 The Boeing Company Flight control system for determining estimated dynamic pressure based on lift and drag coefficients
US11029706B2 (en) 2018-12-07 2021-06-08 The Boeing Company Flight control system for determining a fault based on error between a measured and an estimated angle of attack
US11299285B2 (en) 2018-12-20 2022-04-12 Honeywell International Inc. Systems and methods for providing throttle guidance as a function of flight path acceleration
CN109976370B (zh) * 2019-04-19 2022-09-30 深圳市道通智能航空技术股份有限公司 立面环绕飞行的控制方法、装置、终端及存储介质
EP3798367B1 (fr) 2019-09-25 2022-03-09 BAUER Maschinen GmbH Élément d'ancrage sur une tranchée, son procédé de fonctionnement et procédé de construction souterraine
US11822352B2 (en) 2020-10-26 2023-11-21 Rockwell Collins, Inc. Engine out go around vertical clearance system and method
CN112859892B (zh) * 2020-12-10 2023-12-01 北京航天自动控制研究所 一种基于典型特征信息的动态过程稳定控制方法

Family Cites Families (2)

* Cited by examiner, † Cited by third party
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GB1086211A (en) * 1963-04-19 1967-10-04 Elliott Brothers London Ltd Director system for aircraft
US3522729A (en) * 1968-01-22 1970-08-04 Sperry Rand Corp Airspeed command system

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2435392A1 (fr) * 1978-09-11 1980-04-04 Lockheed Corp Systeme de commande de la vitesse de croisiere d'un avion
EP0427345A2 (fr) * 1989-11-10 1991-05-15 Fokker Aircraft B.V. Commande automatique de la vitesse d'approche pour un avion
EP0427345A3 (en) * 1989-11-10 1992-05-27 Fokker Aircraft B.V. Automated approach speed control for an airplane
FR2894045A1 (fr) * 2005-11-28 2007-06-01 Airbus France Sas Procede de controle de parametres de decollage ou d'atterrissage et dispositif associe
US7751951B2 (en) 2005-11-28 2010-07-06 Airbus France Method for checking takeoff or landing parameters, and associated device

Also Published As

Publication number Publication date
GB1374103A (en) 1974-11-13
US3691356A (en) 1972-09-12
DE2161401C2 (de) 1983-08-18
GB1374102A (en) 1974-11-13
GB1374101A (en) 1974-11-13
CA972463A (en) 1975-08-05
DE2161401A1 (de) 1972-06-29
IT945368B (it) 1973-05-10

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Legal Events

Date Code Title Description
ST Notification of lapse