FR2694822B1 - Circuit de commande de dispositif d'actionnement electromecanique. - Google Patents

Circuit de commande de dispositif d'actionnement electromecanique.

Info

Publication number
FR2694822B1
FR2694822B1 FR9307147A FR9307147A FR2694822B1 FR 2694822 B1 FR2694822 B1 FR 2694822B1 FR 9307147 A FR9307147 A FR 9307147A FR 9307147 A FR9307147 A FR 9307147A FR 2694822 B1 FR2694822 B1 FR 2694822B1
Authority
FR
France
Prior art keywords
control circuit
actuator control
electromechanical actuator
electromechanical
circuit
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
FR9307147A
Other languages
English (en)
Other versions
FR2694822A1 (fr
Inventor
Jeffrey R Ring
Matulenko Rheinhold
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.)
Honeywell Inc
Original Assignee
Honeywell Inc
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 Honeywell Inc filed Critical Honeywell Inc
Publication of FR2694822A1 publication Critical patent/FR2694822A1/fr
Application granted granted Critical
Publication of FR2694822B1 publication Critical patent/FR2694822B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B5/00—Anti-hunting arrangements
    • G05B5/01—Anti-hunting arrangements electric
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P6/00—Arrangements for controlling synchronous motors or other dynamo-electric motors using electronic commutation dependent on the rotor position; Electronic commutators therefor
    • H02P6/06—Arrangements for speed regulation of a single motor wherein the motor speed is measured and compared with a given physical value so as to adjust the motor speed
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P6/00—Arrangements for controlling synchronous motors or other dynamo-electric motors using electronic commutation dependent on the rotor position; Electronic commutators therefor
    • H02P6/34—Modelling or simulation for control purposes

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Power Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Electric Motors In General (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position Or Direction (AREA)
  • Control Of Motors That Do Not Use Commutators (AREA)
FR9307147A 1992-06-15 1993-06-14 Circuit de commande de dispositif d'actionnement electromecanique. Expired - Fee Related FR2694822B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/898,148 US5367237A (en) 1992-06-15 1992-06-15 Electromechanical actuator controller

Publications (2)

Publication Number Publication Date
FR2694822A1 FR2694822A1 (fr) 1994-02-18
FR2694822B1 true FR2694822B1 (fr) 1995-06-23

Family

ID=25409018

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9307147A Expired - Fee Related FR2694822B1 (fr) 1992-06-15 1993-06-14 Circuit de commande de dispositif d'actionnement electromecanique.

Country Status (3)

Country Link
US (1) US5367237A (fr)
JP (1) JPH06161561A (fr)
FR (1) FR2694822B1 (fr)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5589749A (en) * 1994-08-31 1996-12-31 Honeywell Inc. Closed loop control system and method using back EMF estimator
TW322655B (en) * 1996-11-22 1997-12-11 Ind Tech Res Inst The automatic adjust device for driving phase angle
DE59709154D1 (de) 1997-07-11 2003-02-20 Alstom Switzerland Ltd Regelsystem zur Regelung wenigstens einer Variablen eines Prozesses sowie Anwendung eines solchen Regelsystems
US20030089826A1 (en) * 2001-11-13 2003-05-15 Barba Valentin G. Flight lock actuator with dual energy sources
US6776376B2 (en) 2002-10-18 2004-08-17 Hamilton Sunstrand Flight control surface actuation system
US6791219B1 (en) 2003-06-18 2004-09-14 Bvr Technologies Company Contactless electro-mechanical actuator with coupled electronic motor commutation and output position sensors
EP1695906B1 (fr) * 2005-02-23 2012-11-21 Airbus Operations GmbH Dispositif destiné à la détermination d`un angle de rotation d`un arbre dans un aéronef
DE102005008331A1 (de) * 2005-02-23 2006-08-31 Airbus Deutschland Gmbh Einrichtung zur Bestimmung eines Rotationswinkels einer Welle in einem Luftfahrzeug
US7960934B2 (en) * 2008-09-23 2011-06-14 Honeywell International Inc. Fault-tolerant control system
FR2949921B1 (fr) * 2009-09-08 2013-08-23 Thales Sa Dispositif securise de surveillance et de commande pour actionneur de pilotage d'un aeronef
KR101147133B1 (ko) * 2011-02-17 2012-05-25 (주)엔티렉스 각도측정을 위한 상보필터 및 그 방법
US9546069B2 (en) 2015-04-09 2017-01-17 Microsoft Technology Licensing, Llc Drive for electromechanical control of lines
CN104865967A (zh) * 2015-06-01 2015-08-26 中国船舶重工集团公司第七0四研究所 海洋平台补偿集成冗余控制系统
CN104977943B (zh) * 2015-07-14 2018-12-18 崔汉文 一种动态稳定水平控制系统
EP3459844B1 (fr) * 2017-09-25 2022-07-13 Ratier-Figeac SAS Mécanisme de détection de position d'actionneur
CN109443314A (zh) * 2018-10-24 2019-03-08 庆安集团有限公司 一种高升力系统倾斜检测方法

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3035795A (en) * 1959-11-27 1962-05-22 Honeywell Regulator Co Control apparatus
JPS522074B1 (fr) * 1971-04-22 1977-01-19
JPS4835259A (fr) * 1971-09-10 1973-05-24
US4051423A (en) * 1976-02-10 1977-09-27 Sperry Rand Corporation Servo system with feedback signal compensation
US4059064A (en) * 1976-04-05 1977-11-22 Alpha Marine Systems, Inc. Marine auto pilot
US4096426A (en) * 1976-08-09 1978-06-20 Sperry Rand Corporation Non-linear error signal attenuator for servo system
US4338659A (en) * 1978-12-15 1982-07-06 Fujitsu Fanuc Ltd. Position control system for a closed loop type numerical-controlled machine tool
US4345194A (en) * 1980-12-01 1982-08-17 The United States Of America As Represented By The United States Department Of Energy Control system to reduce the effects of friction in drive trains of continuous-path-positioning systems
US4341986A (en) * 1981-01-22 1982-07-27 The United States Of America As Represented By The Secretary Of The Navy Servo control system for the positioning of an apparatus
US4479098A (en) * 1981-07-06 1984-10-23 Watson Industries, Inc. Circuit for tracking and maintaining drive of actuator/mass at resonance
US4463605A (en) * 1982-05-18 1984-08-07 The Boeing Company Simulator circuit for electrohydraulically controlled aircraft surfaces
US4506321A (en) * 1982-09-08 1985-03-19 Imec Corporation Motion control system with adaptive deceleration
US4608527A (en) * 1982-12-20 1986-08-26 Sundstrand Corporation Phase advance waveform generator for brushless DC actuator system controller
JPS606815A (ja) * 1983-06-24 1985-01-14 Mitsutoyo Mfg Co Ltd 微動送り装置
JP2694827B2 (ja) * 1985-10-17 1997-12-24 東芝機械株式会社 バックラッシュ補正方法
JPS6294251A (ja) * 1985-10-17 1987-04-30 Toshiba Mach Co Ltd 位置制御装置
US4697768A (en) * 1985-11-12 1987-10-06 Grumman Aerospace Corporation Flight control system employing complementary filter
US4797829A (en) * 1986-12-11 1989-01-10 Grumman Aerospace Corporation Flight control optimization system for multi-control surface aircraft
JPS6462710A (en) * 1987-09-02 1989-03-09 Fanuc Ltd Spindle control system and numerical controller
US5020125A (en) * 1988-03-28 1991-05-28 Losic Novica A Synthesis of load-independent DC drive system
JPH07120216B2 (ja) * 1988-10-21 1995-12-20 新技術事業団 位置制御方法
US5036266A (en) * 1989-01-17 1991-07-30 Tektronix, Inc. Mass velocity controller
US4914726A (en) * 1989-01-17 1990-04-03 Tektronix, Inc. Mass velocity controller
US5015934A (en) * 1989-09-25 1991-05-14 Honeywell Inc. Apparatus and method for minimizing limit cycle using complementary filtering techniques
JP2621665B2 (ja) * 1991-01-30 1997-06-18 日本電気株式会社 ヘッドの位置決め制御方式
US5155422A (en) * 1991-03-28 1992-10-13 Digital Equipment Corporation Self-tuning adaptive bandwidth regulator

Also Published As

Publication number Publication date
JPH06161561A (ja) 1994-06-07
US5367237A (en) 1994-11-22
FR2694822A1 (fr) 1994-02-18

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Legal Events

Date Code Title Description
ST Notification of lapse

Effective date: 20110228