ES2120206T3 - Regulador inercial de velocidad. - Google Patents

Regulador inercial de velocidad.

Info

Publication number
ES2120206T3
ES2120206T3 ES95919762T ES95919762T ES2120206T3 ES 2120206 T3 ES2120206 T3 ES 2120206T3 ES 95919762 T ES95919762 T ES 95919762T ES 95919762 T ES95919762 T ES 95919762T ES 2120206 T3 ES2120206 T3 ES 2120206T3
Authority
ES
Spain
Prior art keywords
aircraft
speed
inertial
flight path
stabilization mode
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
ES95919762T
Other languages
English (en)
Inventor
Phillip J Gold
Donald L Fogler Jr
James B Dryfoos
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.)
RTX Corp
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of ES2120206T3 publication Critical patent/ES2120206T3/es
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, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • 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
    • G05D1/60—Intended control result
    • G05D1/65—Following a desired speed profile
    • 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
    • B64C13/18—Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot
    • 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
    • G05D1/60—Intended control result
    • G05D1/644—Optimisation of travel parameters, e.g. of energy consumption, journey time or distance
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D2109/00—Types of controlled vehicles
    • G05D2109/20—Aircraft, e.g. drones

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)

Abstract

SE SUMINISTRA UN SISTEMA DE COMANDOS DE VELOCIDAD CON UN MODO DE ESTABILIZACION DE VELOCIDAD EN EL QUE LAS VELOCIDADES REFERENCIADAS DE LA TRAYECTORIA DE VUELO DE UN AVION SON DETERMINADAS CON RESPECTO AL MARCO INERCIAL DE REFERENCIA, LAS VELOCIDADES REFERENCIADAS DE LA TRAYECTORIA DE VUELO SE MANTIENEN CONSTANTES DURANTE LAS MANIOBRAS DE GUIÑADA COMANDADAS POR EL PILOTO DE MANERA QUE EL AVION MANTENGA UNA TRAYECTORIA DE VUELO REFERENCIADA INERCIAL FIJA A PESAR DE LA DIRECCION A LA QUE APUNTE EL AVION. EL CONTROL DE LA VELOCIDAD CON RESPECTO A UN MARCO INERCIAL DE REFERENCIA SE REALIZA CONTROLANDO LA TRAYECTORIA DE VUELO DEL AVION EN BASE A LA ACELERACION LATERAL Y LONGITUDINAL COMANDADA REFERENCIADA DEL FUSELAJE DEL AVION Y EN BASE A LA ACELERACION CENTRIFUGA LATERAL Y LONGITUDINAL REFERENCIADA DEL FUSELAJE DEL AVION. SE SUMINISTRA UN MODO DE FUNCIONAMIENTO DE ESTABILIZACION DE VELOCIDAD EN RESPUESTA A LA ACTIVACION MANUAL DEL MODO DE ESTABILIZACION DE VELOCIDAD POR EL PILOTO, TENIENDO ENCUENTA QUE EL AVION ESTE YA FUNCIONANDO EN EL MODO DE VELOCIDAD DE TIERRA Y EL AVION NO ESTE EN UN GIRO COORDINADO
ES95919762T 1994-06-03 1995-05-04 Regulador inercial de velocidad. Expired - Lifetime ES2120206T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/253,477 US5553812A (en) 1994-06-03 1994-06-03 Inertial velocity command system

Publications (1)

Publication Number Publication Date
ES2120206T3 true ES2120206T3 (es) 1998-10-16

Family

ID=22960437

Family Applications (1)

Application Number Title Priority Date Filing Date
ES95919762T Expired - Lifetime ES2120206T3 (es) 1994-06-03 1995-05-04 Regulador inercial de velocidad.

Country Status (9)

Country Link
US (1) US5553812A (es)
EP (1) EP0763222B1 (es)
JP (1) JPH10501198A (es)
KR (1) KR100369690B1 (es)
CA (1) CA2191861A1 (es)
DE (1) DE69503631T2 (es)
ES (1) ES2120206T3 (es)
IL (1) IL113699A (es)
WO (1) WO1995034029A1 (es)

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US6088653A (en) * 1996-12-31 2000-07-11 Sheikh; Suneel I. Attitude determination method and system
FR2777535B1 (fr) 1998-04-21 2000-06-16 Eurocopter France Systeme de commande de vol d'un aeronef, en particulier d'un helicoptere
US6246929B1 (en) 1999-06-16 2001-06-12 Lockheed Martin Corporation Enhanced stall and recovery control system
US6236914B1 (en) 1999-06-16 2001-05-22 Lockheed Martin Corporation Stall and recovery control system
US6751529B1 (en) * 2002-06-03 2004-06-15 Neural Robotics, Inc. System and method for controlling model aircraft
EP1642181A4 (en) * 2003-05-30 2007-07-11 Neural Robotics Inc SYSTEM AND METHOD FOR CONTROLLING AN AIRCRAFT
US7433765B2 (en) * 2005-05-03 2008-10-07 Sikorsky Aircraft Corporation Fly by wire static longitudinal stability compensator system
CN100519337C (zh) * 2005-09-12 2009-07-29 贝尔直升机泰克斯特龙公司 飞行器以及飞行器的自动速度控制系统和方法
KR100794375B1 (ko) * 2006-07-27 2008-01-15 한국항공대학교산학협력단 소형항공기의 비행데이터 분석시스템
FR2911689B1 (fr) * 2007-01-19 2009-04-03 Airbus Sas Procede et dispositif de controle de la vitesse d'un aeronef
US8694182B2 (en) * 2007-04-03 2014-04-08 Sikorsky Aircraft Corporation Altitude and acceleration command altitude hold algorithm for rotorcraft with large center of gravity range
US8339284B2 (en) * 2008-03-11 2012-12-25 Honeywell International Inc. Method and apparatus for displaying flight path information in rotocraft
US8271151B2 (en) 2008-03-31 2012-09-18 Sikorsky Aircraft Corporation Flight control system for rotary wing aircraft
US20110154837A1 (en) * 2008-10-02 2011-06-30 Taras Michael F Refrigerant system with adaptive hot gas reheat
KR101146748B1 (ko) 2010-07-22 2012-05-17 (주)마이크로인피니티 항체의 자세 제어 장치 및 방법
CN103314336B (zh) 2011-01-14 2016-08-10 贝尔直升机泰克斯特龙公司 用于控制竖直飞行航迹的飞行控制系统和方法
WO2012134460A1 (en) 2011-03-30 2012-10-04 Bell Helicopter Textron Inc. Flight control laws for constant vector flat turns
US9360869B1 (en) 2013-12-03 2016-06-07 Sikorsky Aircraft Corporation Vehicle heading error compensation
FR3023017B1 (fr) 2014-06-30 2016-06-10 Airbus Helicopters Systeme et procede de commande de vol d'un aeronef a voilure tournante en tenue de trajectoire ou tenue de cap selon sa vitesse d'avancement
FR3023016B1 (fr) 2014-06-30 2016-07-01 Airbus Helicopters Systeme et procede de commande de vol en tenue de trajectoire pour un aeronef a voilure tournante
FR3023018B1 (fr) 2014-06-30 2016-06-10 Airbus Helicopters Procede et systeme de mise en vol stationnaire d'un aeronef a voilure tournante en tenue de trajectoire ou tenue de cap selon sa vitesse d'avancement
FR3030760B1 (fr) 2014-12-18 2017-12-22 Airbus Helicopters Procede et systeme de determination d'une vitesse angulaire en virage pour un aeronef a voilure tournante
FR3036805B1 (fr) 2015-05-28 2018-06-29 Airbus Helicopters Procede de determination de la vitesse air longitudinale et de la vitesse sol longitudinale d'un aeronef a voiture tournante selon son exposition au vent
US11288972B2 (en) 2019-12-19 2022-03-29 Textron Innovations Inc. Fleet controller
US11821998B2 (en) 2020-05-21 2023-11-21 Honeywell International Inc. Three-dimensional attitude determination system with multi-faceted integrity solution

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US3995144A (en) * 1966-09-14 1976-11-30 General Electric Company Banked bombing system
US4006871A (en) * 1972-06-19 1977-02-08 The Boeing Company Automatic pitch axis control system for aircraft
US4232313A (en) * 1972-09-22 1980-11-04 The United States Of America As Represented By The Secretary Of The Navy Tactical nagivation and communication system
US4070674A (en) * 1973-10-17 1978-01-24 The Singer Company Doppler heading attitude reference system
US4032759A (en) * 1975-10-24 1977-06-28 The Singer Company Shipboard reference for an aircraft navigation system
US4106094A (en) * 1976-12-13 1978-08-08 Turpin Systems Company Strap-down attitude and heading reference system
US4173784A (en) * 1977-08-29 1979-11-06 The Singer Company Inertial system having correction means for effects of gravitational anomalies
US4589616A (en) * 1984-01-24 1986-05-20 Sperry Corporation Cruise airspeed control of aircraft altitude capture
US4645141A (en) * 1984-05-23 1987-02-24 Rockwell International Corporation Automatic flight control system
US4849900A (en) * 1986-05-02 1989-07-18 The Boeing Company Flight control system and method
DE3634023A1 (de) * 1986-10-07 1988-04-21 Bodenseewerk Geraetetech Integriertes, redundantes referenzsystem fuer die flugregelung und zur erzeugung von kurs- und lageinformationen
US4882697A (en) * 1987-04-16 1989-11-21 Honeywell Inc. Stabilization control circuit for vertical position in an inertial navigator
US4924400A (en) * 1988-09-01 1990-05-08 United Technologies Corporation Arrangement for controlling the performance of bob-up/bob-down maneuvers by a helicopter
US5001646A (en) * 1988-12-19 1991-03-19 Mcdonnell Douglas Corporation Automated helicopter flight control system
US5008825A (en) * 1989-05-01 1991-04-16 Nadkarni Arun A Apparatus and methods for automatically maintaining aircraft track angle
US5195700A (en) * 1991-08-28 1993-03-23 United Technologies Corporation Low speed model following velocity command system for rotary wing aircraft
US5238203A (en) * 1991-08-28 1993-08-24 United Technologies Corporation High speed turn coordination for rotary wing aircraft

Also Published As

Publication number Publication date
KR970703553A (ko) 1997-07-03
US5553812A (en) 1996-09-10
EP0763222A1 (en) 1997-03-19
EP0763222B1 (en) 1998-07-22
DE69503631T2 (de) 1998-11-26
DE69503631D1 (de) 1998-08-27
KR100369690B1 (ko) 2003-05-09
CA2191861A1 (en) 1995-12-14
WO1995034029A1 (en) 1995-12-14
IL113699A0 (en) 1995-08-31
JPH10501198A (ja) 1998-02-03
IL113699A (en) 2000-02-29

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