DE68919732T2 - Steuerungssystem eines Hubschraubers. - Google Patents

Steuerungssystem eines Hubschraubers.

Info

Publication number
DE68919732T2
DE68919732T2 DE68919732T DE68919732T DE68919732T2 DE 68919732 T2 DE68919732 T2 DE 68919732T2 DE 68919732 T DE68919732 T DE 68919732T DE 68919732 T DE68919732 T DE 68919732T DE 68919732 T2 DE68919732 T2 DE 68919732T2
Authority
DE
Germany
Prior art keywords
helicopter
control system
control
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
DE68919732T
Other languages
English (en)
Other versions
DE68919732D1 (de
Inventor
David Robert Haddon
Colin Peter Massey
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.)
AgustaWestland Ltd
Original Assignee
Westland Helicopters Ltd
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 Westland Helicopters Ltd filed Critical Westland Helicopters Ltd
Publication of DE68919732D1 publication Critical patent/DE68919732D1/de
Application granted granted Critical
Publication of DE68919732T2 publication Critical patent/DE68919732T2/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, 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
    • G05D1/0669—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for take-off specially adapted for vertical take-off
    • 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
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/506—Transmitting means with power amplification using electrical energy overriding of personal controls; with automatic return to inoperative position
    • 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)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Feedback Control In General (AREA)
  • Control Of Turbines (AREA)
DE68919732T 1988-03-31 1989-03-21 Steuerungssystem eines Hubschraubers. Expired - Lifetime DE68919732T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB888807676A GB8807676D0 (en) 1988-03-31 1988-03-31 Helicopter control systems

Publications (2)

Publication Number Publication Date
DE68919732D1 DE68919732D1 (de) 1995-01-19
DE68919732T2 true DE68919732T2 (de) 1995-07-20

Family

ID=10634423

Family Applications (1)

Application Number Title Priority Date Filing Date
DE68919732T Expired - Lifetime DE68919732T2 (de) 1988-03-31 1989-03-21 Steuerungssystem eines Hubschraubers.

Country Status (4)

Country Link
US (1) US4947334A (de)
EP (1) EP0335569B1 (de)
DE (1) DE68919732T2 (de)
GB (2) GB8807676D0 (de)

Cited By (1)

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US7769521B2 (en) * 2006-04-05 2010-08-03 Eurocopter Method and a device for performing a check on the state of health of a turbine engine of a twin-engined rotorcraft

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US5265826A (en) * 1991-08-27 1993-11-30 United Technologies Corporation Helicopter engine control having lateral cyclic pitch anticipation
US5314147A (en) * 1991-08-27 1994-05-24 United Technologies Corporation Helicopter engine speed enhancement during heavy rotor load and rapid descent rate maneuvering
US5315819A (en) * 1991-09-17 1994-05-31 Allied-Signal Inc. Power management system for turbine engines
US5274558A (en) * 1991-09-18 1993-12-28 Allied-Signal Inc. Apparatus for decoupling a torque loop from a speed loop in a power management system for turboprop engines
FR2689854B1 (fr) * 1992-04-14 1994-07-01 Eurocopter France Helicoptere monorotor a systeme anticouple mixte et procede pour contrecarrer le couple induit par ce monorotor.
US5850615A (en) * 1995-12-06 1998-12-15 Mcdonnell Douglas Helicopter Co. Rotor blade swashplate-axis rotation and gyroscopic moments componsator
WO1997020734A2 (en) * 1995-12-06 1997-06-12 Mc Donnell Douglas Corporation Flight control system for jet powered tri-mode aircraft
FR2777535B1 (fr) * 1998-04-21 2000-06-16 Eurocopter France Systeme de commande de vol d'un aeronef, en particulier d'un helicoptere
US6264146B1 (en) 1999-12-07 2001-07-24 The Boeing Company Portable controller for an aircraft
EP1296045A3 (de) * 2001-09-24 2004-07-14 Goodrich Control Systems Limited Elektronische Triebwerkssteuerung
GB0122956D0 (en) * 2001-09-24 2001-11-14 Lucas Industries Ltd Fire resistant electronic engine controller
EP1296046A3 (de) * 2001-09-24 2004-07-14 Goodrich Control Systems Limited Elektronische Triebwerkssteuerung
US6879885B2 (en) * 2001-11-16 2005-04-12 Goodrich Pump & Engine Control Systems, Inc. Rotor torque predictor
US6885917B2 (en) 2002-11-07 2005-04-26 The Boeing Company Enhanced flight control systems and methods for a jet powered tri-mode aircraft
FR2876468B1 (fr) * 2004-10-08 2007-08-17 Eurocopter France Systeme de pilotage automatique d'un helicoptere
US7467614B2 (en) 2004-12-29 2008-12-23 Honeywell International Inc. Pedal position and/or pedal change rate for use in control of an engine
US7367531B2 (en) * 2005-08-09 2008-05-06 Greene Leonard M Systems and methods for evading heat seeking missles
US7370836B2 (en) * 2005-08-09 2008-05-13 Greene Leonard M Missile defense system and methods for evading heat seeking missiles
US7389773B2 (en) 2005-08-18 2008-06-24 Honeywell International Inc. Emissions sensors for fuel control in engines
US8275500B2 (en) * 2008-03-11 2012-09-25 Honeywell International Inc. Gas turbine engine fixed collective takeoff compensation control system and method
US8060290B2 (en) 2008-07-17 2011-11-15 Honeywell International Inc. Configurable automotive controller
US20100133852A1 (en) * 2008-11-21 2010-06-03 Preus Robert W Vertical axis wind turbine with variable area
ITTO20090079U1 (it) * 2009-06-10 2010-12-11 Agusta Spa Sistema per la gestione ed il controllo della velocita' di uno o piu' rotori di un aeromobile atto a volare a punto fisso
US8620461B2 (en) 2009-09-24 2013-12-31 Honeywell International, Inc. Method and system for updating tuning parameters of a controller
US8566000B2 (en) 2010-02-23 2013-10-22 Williams International Co., L.L.C. System and method for controlling a single-spool turboshaft engine
US8504175B2 (en) 2010-06-02 2013-08-06 Honeywell International Inc. Using model predictive control to optimize variable trajectories and system control
US9677493B2 (en) 2011-09-19 2017-06-13 Honeywell Spol, S.R.O. Coordinated engine and emissions control system
US20130111905A1 (en) 2011-11-04 2013-05-09 Honeywell Spol. S.R.O. Integrated optimization and control of an engine and aftertreatment system
US9650934B2 (en) 2011-11-04 2017-05-16 Honeywell spol.s.r.o. Engine and aftertreatment optimization system
FR2982320B1 (fr) * 2011-11-08 2014-01-10 Thales Sa Systeme de regulation numerique a pleine autorite pour moteur d'aeronef
EP2814733B1 (de) 2012-02-15 2022-02-02 Rolls-Royce Corporation Optimierte steuerung für gasturbinenmotorleistung
US9193450B2 (en) * 2012-02-24 2015-11-24 Bell Helicopter Textron Inc. System and method for automation of rotorcraft entry into autorotation and maintenance of stabilized autorotation
US9248907B2 (en) * 2012-03-06 2016-02-02 Sikorsky Aircraft Corporation Engine starting system for rotorcraft in flight
JP5832352B2 (ja) * 2012-03-29 2015-12-16 三菱重工業株式会社 垂直離着陸機のトルク推定装置、垂直離着陸機、垂直離着陸機のトルク推定プログラム、及び垂直離着陸機のトルク推定方法
CN104238469B (zh) * 2013-06-13 2018-01-16 优利科技有限公司 飞行器控制系统
WO2016039834A2 (en) * 2014-08-29 2016-03-17 Sikorsky Aircraft Corporation Vector limiting of a rotor control volume
US10351230B2 (en) 2014-09-23 2019-07-16 Sikorsky Aircraft Corporation Initial rotor state compensation for a rotorcraft
WO2016054014A1 (en) * 2014-09-30 2016-04-07 Sikorsky Aircraft Corporation Enhanced engine load demand anticipation
EP3051367B1 (de) 2015-01-28 2020-11-25 Honeywell spol s.r.o. Ansatz und system zur handhabung von einschränkungen für gemessene störungen mit unsicherer vorschau
EP3056706A1 (de) 2015-02-16 2016-08-17 Honeywell International Inc. Ansatz zur nachbehandlungssystemmodellierung und modellidentifizierung
CN104765309A (zh) * 2015-04-08 2015-07-08 何春旺 遥控器、遥控行驶装置、遥控行驶装置控制系统及其方法
EP3091212A1 (de) 2015-05-06 2016-11-09 Honeywell International Inc. Identifikationsansatz für verbrennungsmotor-mittelwertmodelle
EP3734375B1 (de) 2015-07-31 2023-04-05 Garrett Transportation I Inc. Quadratischer programmlöser für mpc mit variabler anordnung
US10272779B2 (en) 2015-08-05 2019-04-30 Garrett Transportation I Inc. System and approach for dynamic vehicle speed optimization
US10415492B2 (en) 2016-01-29 2019-09-17 Garrett Transportation I Inc. Engine system with inferential sensor
US10124750B2 (en) 2016-04-26 2018-11-13 Honeywell International Inc. Vehicle security module system
US10036338B2 (en) 2016-04-26 2018-07-31 Honeywell International Inc. Condition-based powertrain control system
US10309330B2 (en) 2016-10-27 2019-06-04 Rolls-Royce Corporation Model reference adaptive controller
US10240544B2 (en) 2016-10-27 2019-03-26 Rolls-Royce Corporation Adaptive controller using unmeasured operating parameter
WO2018101918A1 (en) 2016-11-29 2018-06-07 Honeywell International Inc. An inferential flow sensor
US20190005826A1 (en) * 2017-06-28 2019-01-03 Ge Aviation Systems, Llc Engine load model systems and methods
US11057213B2 (en) 2017-10-13 2021-07-06 Garrett Transportation I, Inc. Authentication system for electronic control unit on a bus
RU179074U1 (ru) * 2017-11-14 2018-04-25 Акционерное общество "Аэроприбор - Восход" Система управления общевертолетным оборудованием
US11092136B2 (en) * 2018-05-04 2021-08-17 Raytheon Technologies Corporation Systems and methods for optimal speed protection for power turbine governing
US10843791B2 (en) * 2018-05-16 2020-11-24 Textron Innovations Inc. System and method for controlling rotorcraft
US11119507B2 (en) * 2018-06-27 2021-09-14 Intel Corporation Hardware accelerator for online estimation

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GB1011055A (en) * 1960-12-22 1965-11-24 Dehavilland Aircraft Improved engine fuel control system
CA1050633A (en) * 1974-12-19 1979-03-13 Ronald J. Miller Semi-automatic flight control system utilizing limited authority stabilization system
CA1118101A (en) * 1977-06-02 1982-02-09 Jerry Doniger Digital flight guidance system
US4313201A (en) * 1980-03-05 1982-01-26 United Technologies Corporation Tested, dissimilar helicopter stability augmentation
US4500966A (en) * 1982-05-26 1985-02-19 Chandler Evans Inc. Super contingency aircraft engine control
CA1246717A (en) * 1983-08-01 1988-12-13 James J. Howlett Rotorcraft load factor enhancer
GB2185951B (en) * 1986-02-04 1989-07-05 Rolls Royce Helicopter rotor and engine control

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7769521B2 (en) * 2006-04-05 2010-08-03 Eurocopter Method and a device for performing a check on the state of health of a turbine engine of a twin-engined rotorcraft

Also Published As

Publication number Publication date
DE68919732D1 (de) 1995-01-19
GB8807676D0 (en) 1988-05-05
GB2216860A (en) 1989-10-18
EP0335569B1 (de) 1994-12-07
GB2216860B (en) 1991-11-06
EP0335569A3 (en) 1990-03-21
GB8906454D0 (en) 1989-05-04
US4947334A (en) 1990-08-07
EP0335569A2 (de) 1989-10-04

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Legal Events

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