ES8203757A1 - Perfeccionamientos en los dispositivos autopiloto de mante- nimiento de velocidad aerodinamica para helicopteros - Google Patents

Perfeccionamientos en los dispositivos autopiloto de mante- nimiento de velocidad aerodinamica para helicopteros

Info

Publication number
ES8203757A1
ES8203757A1 ES504441A ES504441A ES8203757A1 ES 8203757 A1 ES8203757 A1 ES 8203757A1 ES 504441 A ES504441 A ES 504441A ES 504441 A ES504441 A ES 504441A ES 8203757 A1 ES8203757 A1 ES 8203757A1
Authority
ES
Spain
Prior art keywords
airspeed
pitch
autopilot
cruise speeds
attitude
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
Application number
ES504441A
Other languages
English (en)
Other versions
ES504441A0 (es
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.)
Raytheon Technologies 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
Publication of ES8203757A1 publication Critical patent/ES8203757A1/es
Publication of ES504441A0 publication Critical patent/ES504441A0/es
Granted 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
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for transition from automatic pilot to manual pilot and vice versa
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/54—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement
    • B64C27/56—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated
    • B64C27/57—Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)
  • Toys (AREA)

Abstract

SISTEMA ELECTRICO DE ADQUISICION DE VELOCIDAD Y DE ORIENTACION Y DE CONTROL DE RETENCION DE UN HELICOPTERO. EL HELICOPTERO LLEVA INCORPORADA UNA PALANCA DE CONTROL DE PASO CICLICO LONGITUDINAL QUE COMPRENDE UN CONMUTADOR DE LIBERACION DE EQUILIBRIO EN VUELO RECTILINEO. ADEMAS, COMPRENDE UN ACTUADOR PARA EL EQUILIBRIO EN VUELO RECTILINEO QUE RESPONDE A SEÑALES ELECTRICAS APLICADAS AL MISMO PARA POSICIONAR LA CITADA PALANCA, MEDIOS DE VELOCIDAD AERODINAMICA QUE SUMINISTRAN UNA SEÑAL DE VELOCIDAD INDICATIVA DE LA VELOCIDAD REAL DEL HILICOPTERO.
ES504441A 1980-08-08 1981-07-30 Perfeccionamientos en los dispositivos autopiloto de mante- nimiento de velocidad aerodinamica para helicopteros Granted ES504441A0 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/176,832 US4382283A (en) 1980-08-08 1980-08-08 Helicopter attitude and airspeed acquisition and retention system

Publications (2)

Publication Number Publication Date
ES8203757A1 true ES8203757A1 (es) 1982-05-01
ES504441A0 ES504441A0 (es) 1982-05-01

Family

ID=22646030

Family Applications (1)

Application Number Title Priority Date Filing Date
ES504441A Granted ES504441A0 (es) 1980-08-08 1981-07-30 Perfeccionamientos en los dispositivos autopiloto de mante- nimiento de velocidad aerodinamica para helicopteros

Country Status (10)

Country Link
US (1) US4382283A (es)
JP (2) JPS57104496A (es)
AU (1) AU539602B2 (es)
CA (1) CA1166720A (es)
CH (1) CH654536A5 (es)
DE (1) DE3129547C2 (es)
ES (1) ES504441A0 (es)
FR (2) FR2490843A1 (es)
GB (1) GB2081474B (es)
IT (1) IT1137837B (es)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4385355A (en) * 1981-03-30 1983-05-24 United Technologies Corporation Automatic outer loop centering of aircraft inner loop
US4387432A (en) * 1981-03-30 1983-06-07 United Technologies Corporation Pulsed aircraft actuator
US4477876A (en) * 1981-03-30 1984-10-16 United Technologies Corporation Dual response aircraft reference synchronization
US4460964A (en) * 1981-08-31 1984-07-17 Sperry Corporation Multiaxis hardover protection apparatus for automatic flight control systems
US4481586A (en) * 1982-03-09 1984-11-06 Sperry Corporation Adaptive washout circuit for use in a stability augmentation system
US4740899A (en) * 1982-07-01 1988-04-26 Rockwell International Corporation Use of headwind and airspeed to achieve a transition to a hover in a helicopter or vtol aircraft
US4628455A (en) * 1983-05-06 1986-12-09 Sperry Corporation Cross axis torque limiter for helicopter autopilot
US4580223A (en) * 1983-11-07 1986-04-01 United Technologies Corporation Incorporation of pitch bias actuator function into an existing AFCS
US4645141A (en) * 1984-05-23 1987-02-24 Rockwell International Corporation Automatic flight control system
US4763285A (en) * 1985-10-04 1988-08-09 Semco Instruments, Inc. Helicopter low-g monitor, recorder and warning system
US5214596A (en) * 1986-06-14 1993-05-25 Duetsche Forchungs- Und Versuchsanstalt Fur Luft- Und Raumfahrt E.V. System for determining the airspeed of helicopters
FR2613078B1 (fr) * 1987-03-26 1990-12-28 Crouzet Sa Dispositif de mesure de la vitesse air d'un helicoptere
US5178307A (en) * 1991-08-28 1993-01-12 United Technologies Corporation High speed yaw control system for rotary wing aircraft
US5238203A (en) * 1991-08-28 1993-08-24 United Technologies Corporation High speed turn coordination for rotary wing aircraft
US5213283A (en) * 1991-08-28 1993-05-25 United Technologies Corporation Low speed turn coordination for rotary wing aircraft
US5222691A (en) * 1991-08-28 1993-06-29 United Technologies Corporation Automatic turn coordination trim control for rotary wing aircraft
DE69217229T2 (de) * 1991-08-28 1997-06-12 United Technologies Corp., Hartford, Conn. System zur vertikalen steuerung für drehflügelflugzeug
US5310136A (en) * 1992-05-19 1994-05-10 United Technologies Corporation Helicopter integrated fire and flight control having constraint limiting control
US5589749A (en) * 1994-08-31 1996-12-31 Honeywell Inc. Closed loop control system and method using back EMF estimator
US5596499A (en) * 1995-02-21 1997-01-21 The Boeing Company Control law mode switching between rate command and attitude command control systems
US7031811B2 (en) * 2003-05-30 2006-04-18 The Boeing Company Fuel efficient airspeed trim
US7108232B2 (en) * 2004-02-05 2006-09-19 Hoh Roger H Helicopter force-feel and stability augmentation system with parallel servo-actuator
US7970501B2 (en) * 2005-03-08 2011-06-28 Honeywell International Inc. Methods and systems utilizing true airspeed to improve vertical velocity accuracy
US7433765B2 (en) * 2005-05-03 2008-10-07 Sikorsky Aircraft Corporation Fly by wire static longitudinal stability compensator system
WO2013012408A1 (en) * 2011-07-15 2013-01-24 Bell Helicopter Textron Inc. Flight control laws for automatic hover hold
US10338090B2 (en) * 2014-09-04 2019-07-02 Sikorsky Aircraft Corporation Airspeed estimation system
WO2016178738A1 (en) 2015-05-05 2016-11-10 Sikorsky Aircraft Corporation Position hold override control
DE102015118030B4 (de) * 2015-10-22 2017-11-16 Deutsches Zentrum für Luft- und Raumfahrt e.V. Autopilot für atmosphärische Fluggeräte sowie Fluggerät und Verfahren zur Geschwindigkeitsregelung hierzu
US10101749B1 (en) * 2017-03-21 2018-10-16 Bell Helicopter Textron Inc. Combined airspeed and inertial data for rotorcraft longitudinal control
US10816971B2 (en) * 2018-02-12 2020-10-27 Textron Innovations Inc. Autopilot recoupling for rotorcraft

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5031870A (es) * 1973-07-20 1975-03-28
US4129275A (en) * 1974-11-22 1978-12-12 The Boeing Company Automatic flight control apparatus for aircraft
JPS5515359B2 (es) * 1974-11-22 1980-04-23
IL51185A (en) * 1976-02-03 1981-03-31 United Technologies Corp Method and apparatus for automatic aircraft heading control
US4003532A (en) * 1976-03-15 1977-01-18 United Technologies Corporation Heading hold logic
US4079905A (en) * 1977-02-07 1978-03-21 Safe Flight Instrument Corporation System for providing an indication of wind shear
US4095271A (en) * 1977-04-20 1978-06-13 Sundstrand Data Control, Inc. Aircraft pitch attitude signal generator
US4168045A (en) * 1978-02-28 1979-09-18 United Technologies Corporation Speed and collective pitch bias of helicopter longitudinal cyclic pitch
US4213584A (en) * 1978-10-04 1980-07-22 United Technologies Corporation Helicopter hover stability and cruise gust effect alleviation
US4206891A (en) * 1978-10-26 1980-06-10 United Technologies Corporation Helicopter pedal feel force proportional to side slip
US4300200A (en) * 1978-12-01 1981-11-10 Westland Aircraft Limited Helicopter airspeed indicating system

Also Published As

Publication number Publication date
CA1166720A (en) 1984-05-01
JPH03143800A (ja) 1991-06-19
US4382283A (en) 1983-05-03
AU7346981A (en) 1982-02-11
FR2490843A1 (fr) 1982-03-26
JPH0769338B2 (ja) 1995-07-26
DE3129547A1 (de) 1982-05-19
GB2081474B (en) 1984-10-10
AU539602B2 (en) 1984-10-04
FR2490843B1 (es) 1984-12-21
IT1137837B (it) 1986-09-10
ES504441A0 (es) 1982-05-01
IT8123426A0 (it) 1981-08-07
FR2497955B1 (es) 1985-03-22
GB2081474A (en) 1982-02-17
FR2497955A1 (fr) 1982-07-16
CH654536A5 (de) 1986-02-28
JPS57104496A (en) 1982-06-29
DE3129547C2 (de) 1994-03-03
JPH0415160B2 (es) 1992-03-17

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 19990503