DE69206805D1 - Selbstanpassende begrenzungsvorrichtung für die eingangsignale eines steuerungssystems - Google Patents

Selbstanpassende begrenzungsvorrichtung für die eingangsignale eines steuerungssystems

Info

Publication number
DE69206805D1
DE69206805D1 DE69206805T DE69206805T DE69206805D1 DE 69206805 D1 DE69206805 D1 DE 69206805D1 DE 69206805 T DE69206805 T DE 69206805T DE 69206805 T DE69206805 T DE 69206805T DE 69206805 D1 DE69206805 D1 DE 69206805D1
Authority
DE
Germany
Prior art keywords
self
control system
input signals
limiting device
adjusting limiting
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 - Fee Related
Application number
DE69206805T
Other languages
English (en)
Other versions
DE69206805T2 (de
Inventor
Donald Adams
Stuart Wright
David Verzella
Troy Lamontagne
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
Application granted granted Critical
Publication of DE69206805D1 publication Critical patent/DE69206805D1/de
Publication of DE69206805T2 publication Critical patent/DE69206805T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B5/00Anti-hunting arrangements
    • G05B5/01Anti-hunting arrangements electric
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0061Control 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
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S424/00Drug, bio-affecting and body treating compositions
    • Y10S424/819Viral vaccine for feline species, e.g. cats

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position Or Direction (AREA)
DE69206805T 1991-07-22 1992-07-09 Selbstanpassende begrenzungsvorrichtung für die eingangsignale eines steuerungssystems Expired - Fee Related DE69206805T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/733,793 US5224664A (en) 1991-07-22 1991-07-22 Adaptive control system input limiting
PCT/US1992/005742 WO1993002405A1 (en) 1991-07-22 1992-07-09 Adaptive control system input limiting

Publications (2)

Publication Number Publication Date
DE69206805D1 true DE69206805D1 (de) 1996-01-25
DE69206805T2 DE69206805T2 (de) 1996-05-23

Family

ID=24949140

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69206805T Expired - Fee Related DE69206805T2 (de) 1991-07-22 1992-07-09 Selbstanpassende begrenzungsvorrichtung für die eingangsignale eines steuerungssystems

Country Status (10)

Country Link
US (1) US5224664A (de)
EP (1) EP0595914B1 (de)
JP (1) JPH06509198A (de)
KR (1) KR100233345B1 (de)
AU (1) AU657157B2 (de)
CA (1) CA2113648C (de)
DE (1) DE69206805T2 (de)
ES (1) ES2083752T3 (de)
IL (1) IL102482A (de)
WO (1) WO1993002405A1 (de)

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EP0601000B1 (de) * 1991-08-28 1997-01-29 United Technologies Corporation System zur vertikalen steuerung für drehflügelflugzeug
US5377937A (en) * 1991-09-03 1995-01-03 The Boeing Company Aircraft flare control system utilizing an envelope limiter
US5264768A (en) * 1992-10-06 1993-11-23 Honeywell, Inc. Active hand controller feedback loop
FR2711257B1 (fr) * 1993-10-14 1995-12-22 Aerospatiale Système de commande de vol électrique pour avion avec protection en assiette au décollage.
DE4421105A1 (de) * 1993-11-02 1995-05-04 Hewlett Packard Co Reduzierung des elektrischen Motorstoßstroms durch nicht-lineare Begrenzung der Änderungsrate der Winkelgeschwindigkeit
US5826834A (en) * 1994-10-19 1998-10-27 Honeywell Inc. Self adaptive limiter for automatic control of approach and landing
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
FR2756252B1 (fr) * 1996-11-22 1999-01-22 Eurocopter France Systeme de commande de vol pour aeronef a voilure tournante, notamment pour un helicoptere
US6003811A (en) * 1997-03-24 1999-12-21 The Boeing Company Aircraft servovalve current rate limiter
US6021370A (en) * 1997-08-05 2000-02-01 Cummins Engine Company, Inc. Vehicle/engine acceleration rate management system
SE9704929L (sv) * 1997-12-30 1998-10-26 Saab Ab Anordning och metod för styrkraftreglering vid ett mekaniskt styrsystem för ett flygplan
JP3195918B2 (ja) * 1999-03-12 2001-08-06 株式会社コミュータヘリコプタ先進技術研究所 ヘリコプタ用飛行制御装置
US6422517B1 (en) 1999-12-02 2002-07-23 Boeing Company Aircraft tailstrike avoidance system
US6618631B1 (en) * 2000-04-25 2003-09-09 Georgia Tech Research Corporation Adaptive control system having hedge unit and related apparatus and methods
US6885917B2 (en) 2002-11-07 2005-04-26 The Boeing Company Enhanced flight control systems and methods for a jet powered tri-mode aircraft
AU2003304407A1 (en) 2002-12-09 2005-02-25 Georgia Tech Research Corp. Adaptive output feedback apparatuses and methods capable of controlling a non­minimum phase system
DE10323785B4 (de) * 2003-05-23 2009-09-10 Wobben, Aloys, Dipl.-Ing. Verfahren zum Erkennen eines Eisansatzes an Rotorblättern
US7463956B2 (en) * 2003-07-03 2008-12-09 The Boeing Company Constant vertical state maintaining cueing system
US7627403B2 (en) * 2006-03-23 2009-12-01 The Boeing Company Bias correcting phase compensating rate limiter
US7617024B2 (en) * 2006-09-22 2009-11-10 Bell Helicopter Textron Inc. Automatic heading control system for tiltrotor aircraft and helicopters
FR2920231B1 (fr) * 2007-08-20 2015-02-27 Airbus France Procede et dispositif de protection automatique d'un aeronef contre un atterissage dur
US8002220B2 (en) * 2007-10-25 2011-08-23 Honeywell International Inc. Rate limited active pilot inceptor system and method
US7988089B2 (en) * 2008-03-27 2011-08-02 Sikorsky Aircraft Corporation Swashplate trajectory control
JP5893890B2 (ja) * 2011-10-18 2016-03-23 三菱重工業株式会社 航空機及び航空機の制御方法
US10618645B2 (en) * 2015-08-25 2020-04-14 Aerovironment, Inc. Ganged servo flight control system for an unmanned aerial vehicle
EP3653562A1 (de) * 2018-11-19 2020-05-20 B&R Industrial Automation GmbH Verfahren und schwingungsregler zum ausregeln von schwingungen eines schwingfähigen technischen systems

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3201675A (en) * 1962-11-01 1965-08-17 Bendix Corp Maximum command limiter device for an automatic flight control system
US3390612A (en) * 1965-07-06 1968-07-02 Chandler Evans Inc Dual stroke actuator
US3429376A (en) * 1966-10-18 1969-02-25 Kurt H Hohenemser Automatic control system for aircraft lifting rotor
US3390614A (en) * 1967-06-23 1968-07-02 Newport News S & D Co Electrohydraulic servocontrol system
US3938762A (en) * 1974-05-20 1976-02-17 Textron, Inc. Rotor blade force track sensing system and automatic span tracking system
US4078750A (en) * 1977-03-08 1978-03-14 United Technologies Corporation Speed-variable limits in fail-safe actuators
US4133250A (en) * 1977-06-22 1979-01-09 Pneumo Corporation Combined feedback control system
US4094481A (en) * 1977-06-30 1978-06-13 Sperry Rand Corporation Fail passive dual servo with continuous motor speed and acceleration and monitoring
SE440129B (sv) * 1979-06-20 1985-07-15 Akermans Verkstad Ab Anordning for att reducera kolvhastigheten i en cylinder, da kolven nermar sig endlegena
US4420808A (en) * 1980-04-01 1983-12-13 United Technologies Corporation Multi-axis force stick, self-trimmed aircraft flight control system
US4305028A (en) * 1980-04-04 1981-12-08 Nordson Corporation System for evaluating the capability of a work-performing robot to reproduce a programmed series of motions
US4599698A (en) * 1983-05-02 1986-07-08 United Technologies Corporation Aircraft trim actuator shutdown monitor system and method
EP0128491B1 (de) * 1983-06-03 1989-12-13 Omron Tateisi Electronics Co. Zeitdiskret selbstanpassender Ein/Aus-Schaltregler
US4774651A (en) * 1985-06-03 1988-09-27 Vickers, Incorporated Power transmission
DE3612905C2 (de) * 1986-04-17 1993-11-18 Bosch Gmbh Robert Verfahren zum Auslösen einer Schaltfunktion
GB8629896D0 (en) * 1986-12-15 1987-01-28 Westland Plc Helicopter flight control system
US4866361A (en) * 1988-05-05 1989-09-12 The United States Of America As Represented By The Secretary Of The Navy Actuator rate saturation compensator
JPH0786776B2 (ja) * 1988-11-12 1995-09-20 三田工業株式会社 移動体の制御装置

Also Published As

Publication number Publication date
IL102482A0 (en) 1993-02-21
KR100233345B1 (ko) 1999-12-01
IL102482A (en) 1996-05-14
EP0595914B1 (de) 1995-12-13
JPH06509198A (ja) 1994-10-13
CA2113648C (en) 2000-05-23
AU2323592A (en) 1993-02-23
AU657157B2 (en) 1995-03-02
DE69206805T2 (de) 1996-05-23
US5224664A (en) 1993-07-06
EP0595914A1 (de) 1994-05-11
WO1993002405A1 (en) 1993-02-04
ES2083752T3 (es) 1996-04-16
CA2113648A1 (en) 1993-02-04

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee