IL153172A0 - Method, apparatus and design procedure for controlling multi-input, multi-output (mimo) parameter dependent systems using feedback ltt'zation - Google Patents

Method, apparatus and design procedure for controlling multi-input, multi-output (mimo) parameter dependent systems using feedback ltt'zation

Info

Publication number
IL153172A0
IL153172A0 IL15317201A IL15317201A IL153172A0 IL 153172 A0 IL153172 A0 IL 153172A0 IL 15317201 A IL15317201 A IL 15317201A IL 15317201 A IL15317201 A IL 15317201A IL 153172 A0 IL153172 A0 IL 153172A0
Authority
IL
Israel
Prior art keywords
input
ltt
zation
coordinates
control laws
Prior art date
Application number
IL15317201A
Other languages
English (en)
Original Assignee
Dabulamanzi Holdings Llc
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 Dabulamanzi Holdings Llc filed Critical Dabulamanzi Holdings Llc
Publication of IL153172A0 publication Critical patent/IL153172A0/xx

Links

Classifications

    • 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
    • G05B24/00—Open-loop automatic control systems not otherwise provided for
    • 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
    • G05B9/00—Safety arrangements
    • G05B9/02—Safety arrangements electric
    • 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
    • G05B11/00—Automatic controllers
    • G05B11/01—Automatic controllers electric
    • G05B11/32—Automatic controllers electric with inputs from more than one sensing element; with outputs to more than one correcting element
    • 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
    • G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
    • G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
    • G05B13/04—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators
    • G05B13/042—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators in which a parameter or coefficient is automatically adjusted to optimise the performance
    • 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
    • G05B9/00—Safety arrangements
    • G05B9/02—Safety arrangements electric
    • G05B9/03—Safety arrangements electric with multiple-channel loop, i.e. redundant control systems
    • 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
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
    • G05D1/0825—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using mathematical models

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Health & Medical Sciences (AREA)
  • Evolutionary Computation (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Optimization (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Mathematical Analysis (AREA)
  • Algebra (AREA)
  • Artificial Intelligence (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Mathematical Physics (AREA)
  • Medical Informatics (AREA)
  • Software Systems (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Radio Transmission System (AREA)
  • Amplifiers (AREA)
  • Optical Communication System (AREA)
  • Electrotherapy Devices (AREA)
  • Networks Using Active Elements (AREA)
IL15317201A 2000-05-30 2001-05-30 Method, apparatus and design procedure for controlling multi-input, multi-output (mimo) parameter dependent systems using feedback ltt'zation IL153172A0 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/580,587 US6539290B1 (en) 1995-06-07 2000-05-30 Method, apparatus and design procedure for controlling multi-input, multi-output (MIMO) parameter dependent systems using feedback LTI'zation
PCT/US2001/017319 WO2001092972A2 (fr) 2000-05-30 2001-05-30 Procede, appareil et procedure de conception permettant de controler des systemes dependant de parametres a multiples entrees et sorties, (mimo) au moyen d'une invariance de temps lineaire (lti) de retroaction

Publications (1)

Publication Number Publication Date
IL153172A0 true IL153172A0 (en) 2003-06-24

Family

ID=24321695

Family Applications (2)

Application Number Title Priority Date Filing Date
IL15317201A IL153172A0 (en) 2000-05-30 2001-05-30 Method, apparatus and design procedure for controlling multi-input, multi-output (mimo) parameter dependent systems using feedback ltt'zation
IL153172A IL153172A (en) 2000-05-30 2002-11-28 Method, device and design procedures for control using LTI feedback Multiple input systems Dependent on variables

Family Applications After (1)

Application Number Title Priority Date Filing Date
IL153172A IL153172A (en) 2000-05-30 2002-11-28 Method, device and design procedures for control using LTI feedback Multiple input systems Dependent on variables

Country Status (11)

Country Link
US (2) US6539290B1 (fr)
EP (2) EP1290508B1 (fr)
JP (1) JP4570842B2 (fr)
KR (1) KR100804355B1 (fr)
AT (1) ATE292295T1 (fr)
AU (2) AU2001263487B2 (fr)
CA (2) CA2410910C (fr)
DE (1) DE60109772T2 (fr)
ES (1) ES2238444T3 (fr)
IL (2) IL153172A0 (fr)
WO (1) WO2001092972A2 (fr)

Families Citing this family (85)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6711476B2 (en) * 2001-09-27 2004-03-23 The Boeing Company Method and computer program product for estimating at least one state of a dynamic system
US7493470B1 (en) 2001-12-07 2009-02-17 Arc International, Plc Processor apparatus and methods optimized for control applications
US6694228B2 (en) * 2002-05-09 2004-02-17 Sikorsky Aircraft Corporation Control system for remotely operated vehicles for operational payload employment
WO2004101357A2 (fr) 2002-08-30 2004-11-25 Qaxu Technology Inc. Aeroglisseur volant homeostatique
US20040117043A1 (en) * 2002-09-07 2004-06-17 Igor Touzov Optimized calibration data based methods for parallel digital feedback, and digital automation controls
FR2844251B1 (fr) * 2002-09-09 2005-05-27 Airbus France Procede et systeme pour deplacer une gouverne d'un aeronef.
DE10246910B4 (de) * 2002-10-08 2004-11-04 Mtu Aero Engines Gmbh Mehrgrößenregelungssystem und Verfahren zum Regeln einer Mehrgrößenregelstrecke
US20050226727A1 (en) * 2004-03-03 2005-10-13 Dennis Brian D Methods and systems for controlling the pitch of a propeller
WO2006071258A2 (fr) * 2004-06-02 2006-07-06 Athena Technologies, Inc. Systemes et procedes de commande de systemes dynamiques
WO2006137869A2 (fr) * 2004-09-17 2006-12-28 Aurora Flight Sciences Systeme et procede pour le controle de la vitesse angulaire de roulis d'un aeronef a voilure libre desaccouplee en torsion
EP1796962A2 (fr) 2004-09-17 2007-06-20 Aurora Flight Sciences Commande d'approche destinee a un avion a decollage et a atterrissage vertical de type tail sitter (assis sur la queue)
US7559191B2 (en) 2004-09-17 2009-07-14 Aurora Flight Sciences Corporation Ducted spinner for engine cooling
WO2007001369A2 (fr) 2004-09-17 2007-01-04 Aurora Flight Sciences Systeme et methode pour commander le regime d'un moteur a soufflante canalisee
WO2007001371A2 (fr) 2004-09-17 2007-01-04 Aurora Flight Sciences Systeme d'attache reacteur antivibratile, et procede se rapportant a un aeronef a soufflante canalisee
EP1796961A2 (fr) * 2004-09-17 2007-06-20 Aurora Flight Sciences Train d'atterrissage adaptatif
FR2876468B1 (fr) * 2004-10-08 2007-08-17 Eurocopter France Systeme de pilotage automatique d'un helicoptere
US8948936B2 (en) 2004-11-08 2015-02-03 Textron Innovations Inc. Vehicle management system using finite state machines
CA2585105C (fr) * 2004-11-08 2015-04-21 Bell Helicopter Textron Inc. Systeme de commande de vol faisant appel a trois boucles de commande
US8942866B2 (en) * 2004-11-08 2015-01-27 Textron Innovations Inc. Extension of three loop control laws for system uncertainties, calculation time delay and command quickness
US9057627B2 (en) * 2005-03-15 2015-06-16 Fci Associates, Inc. Low cost flight instrumentation system
JP4728020B2 (ja) * 2005-03-17 2011-07-20 日立オートモティブシステムズ株式会社 車両制御用ソフトウェア及び車両制御装置
US7430460B2 (en) * 2005-03-23 2008-09-30 Price Ricardo A Method for determining roll rate gyro bias in an attitude heading reference system
US7861966B2 (en) * 2005-04-18 2011-01-04 Vehicle Research Corporation Supersonic aircraft footprint spreading control system and method
US7962252B2 (en) * 2005-06-20 2011-06-14 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Self-contained avionics sensing and flight control system for small unmanned aerial vehicle
JP4425193B2 (ja) * 2005-08-16 2010-03-03 三洋電機株式会社 モータの位置センサレス制御装置
KR100679860B1 (ko) 2005-08-19 2007-02-07 한국전자통신연구원 Ｍｉｍｏ 시스템을 위한 낮은 복잡도의 송/수신 안테나선택 방법
JP4480696B2 (ja) * 2005-08-26 2010-06-16 三洋電機株式会社 モータ制御装置
US7579942B2 (en) * 2006-10-09 2009-08-25 Toyota Motor Engineering & Manufacturing North America, Inc. Extra-vehicular threat predictor
US7961826B2 (en) * 2006-12-14 2011-06-14 Texas Instruments Incorporated Parameterized sphere detector and methods of using the same
JP4904589B2 (ja) * 2007-06-14 2012-03-28 富士通株式会社 フィードバック制御系の設計方法、設計プログラム、および設計支援装置
GB0717991D0 (en) * 2007-09-15 2007-10-24 Curvaceous Software Ltd Multi-variable operations
US8527118B2 (en) * 2007-10-17 2013-09-03 The Boeing Company Automated safe flight vehicle
US8255098B2 (en) * 2007-10-17 2012-08-28 The Boeing Company Variably manned aircraft
US8005563B2 (en) 2007-10-26 2011-08-23 The Boeing Company System for assembling aircraft
US8326587B2 (en) * 2007-12-13 2012-12-04 The Boeing Company System, method, and computer program product for predicting cruise orientation of an as-built airplane
US8733707B2 (en) * 2008-04-17 2014-05-27 The Boeing Company Line transfer system for airplane
NL2001844C2 (nl) * 2008-07-22 2010-01-25 Robertus Gerardus De Boer Besturingsinrichting voor een vliegtuig bij dwarswindoperaties.
EP2261116B1 (fr) * 2009-06-09 2019-05-22 Sikorsky Aircraft Corporation Système de compensation automatique pour avion à commandes électriques avec contrôleurs de compensation uniques
KR101177875B1 (ko) * 2009-09-16 2012-08-28 건국대학교 산학협력단 컨트롤러의 자세 변화를 이용한 무인비행체 비행 제어 시스템 및 비행 제어 시스템의 운영방법
US8082047B1 (en) * 2009-11-09 2011-12-20 The Boeing Company Adaptive control method that compensates for sign error in actuator response
US8209066B2 (en) * 2010-02-11 2012-06-26 Bae Systems Information And Electronic Systems Integration Inc. Environmental control system for precision airborne payloads
US8577535B2 (en) * 2010-03-31 2013-11-05 Massachusetts Institute Of Technology System and method for providing perceived first-order control of an unmanned vehicle
JP5916283B2 (ja) * 2010-07-01 2016-05-11 三菱重工業株式会社 表示装置、操縦支援システム、及び表示方法
US8265812B2 (en) * 2010-11-24 2012-09-11 William M Pease System and method for a marine vessel autopilot
US8816260B2 (en) * 2010-12-01 2014-08-26 Raytheon Company Flight-control system for canard-controlled flight vehicles and methods for adaptively limiting acceleration
CN102176160B (zh) * 2010-12-31 2012-09-26 北京控制工程研究所 基于偏量特征模型的高超声速飞行器自适应学习控制方法
WO2012134447A2 (fr) * 2011-03-29 2012-10-04 Bell Helicopter Textron Inc. Lois de commande de vol pour virages inclinés de pleine enveloppe
EP2673681B1 (fr) 2011-03-30 2016-09-07 Bell Helicopter Textron Inc. Lois de commande de vol pour virages à plat à vecteur constant
EP2511656A1 (fr) * 2011-04-14 2012-10-17 Hexagon Technology Center GmbH Système de mesure pour la détermination de coordonnées 3D d'une surface d'objet
KR101214018B1 (ko) * 2011-04-15 2013-01-09 주식회사 대한항공 무인 항공기 제어 시스템계 방법
KR101222544B1 (ko) * 2011-09-05 2013-01-16 한국항공우주산업 주식회사 다양한 고정익 형상을 갖는 비행체의 비행 제어 소프트웨어에 적용할 수 있는 프로그램을 기록한 컴퓨터로 판독가능한 기록 매체 및 이를 이용한 방법
US9011250B2 (en) 2012-10-05 2015-04-21 Qfo Labs, Inc. Wireless communication system for game play with multiple remote-control flying craft
DE202013012545U1 (de) 2012-11-15 2017-07-03 SZ DJI Technology Co., Ltd. Unbemanntes Luftfahrzeug mit mehreren Rotoren
KR101298793B1 (ko) * 2013-01-04 2013-08-22 한국항공우주산업 주식회사 비행 중 실시간 안정성 시험 방법
TWI584567B (zh) * 2013-08-12 2017-05-21 Ｉｄｔ歐洲有限公司 功率轉換器及用於功率轉換器的控制方法
US10240930B2 (en) 2013-12-10 2019-03-26 SZ DJI Technology Co., Ltd. Sensor fusion
DE102014204115A1 (de) * 2014-03-06 2015-09-10 Robert Bosch Gmbh Notlaufmodus für einen Kolbenmotor in einem Flugzeug
DE102014204354A1 (de) * 2014-03-10 2015-09-10 Robert Bosch Gmbh Verfahren zum Betreiben eines Fahrzeugs und Fahrerassistenzsystem
EP3428766B1 (fr) 2014-09-05 2021-04-07 SZ DJI Technology Co., Ltd. Cartographie environnementale à capteurs multiples
EP3399381A1 (fr) 2014-09-05 2018-11-07 SZ DJI Technology Co., Ltd. Sélection de mode de vol basée sur le contexte
JP6181300B2 (ja) 2014-09-05 2017-08-16 エスゼット ディージェイアイ テクノロジー カンパニー リミテッドＳｚ Ｄｊｉ Ｔｅｃｈｎｏｌｏｇｙ Ｃｏ．，Ｌｔｄ 無人航空機の速度を制御するシステム
CN104298109B (zh) * 2014-09-23 2017-04-19 南京航空航天大学 基于多控制器融合的无尾飞行器协调转弯控制方法
US9731813B2 (en) * 2014-11-12 2017-08-15 The Boeing Company Methods and apparatus to control aircraft horizontal stabilizers
US9893948B2 (en) 2015-03-26 2018-02-13 Utopus Insights, Inc. Network management using hierarchical and multi-scenario graphs
US9922282B2 (en) 2015-07-21 2018-03-20 Limitless Computing, Inc. Automated readiness evaluation system (ARES) for use with an unmanned aircraft system (UAS)
FR3040220B1 (fr) * 2015-08-19 2018-04-20 Safran Aircraft Engines Systeme de regulation d'un parametre regule
US10258888B2 (en) 2015-11-23 2019-04-16 Qfo Labs, Inc. Method and system for integrated real and virtual game play for multiple remotely-controlled aircraft
US9568915B1 (en) * 2016-02-11 2017-02-14 Mitsubishi Electric Research Laboratories, Inc. System and method for controlling autonomous or semi-autonomous vehicle
US10303184B1 (en) * 2017-12-08 2019-05-28 Kitty Hawk Corporation Autonomous takeoff and landing with open loop mode and closed loop mode
US11712637B1 (en) 2018-03-23 2023-08-01 Steven M. Hoffberg Steerable disk or ball
US11092136B2 (en) * 2018-05-04 2021-08-17 Raytheon Technologies Corporation Systems and methods for optimal speed protection for power turbine governing
US11591074B1 (en) * 2018-11-28 2023-02-28 Zunum Aero, Inc. System and methods for designing and building regional hybrid-to-electric systems and methods for designing and optimizing regional hybrid-to-electric aircraft
US11003196B2 (en) * 2018-12-07 2021-05-11 The Boeing Company Flight control system for determining a common mode pneumatic fault
CA3094757A1 (fr) 2019-09-30 2021-03-30 Bombardier Inc. Systemes et methodes de commande d`aeronef utilisant un controle sliding mode et la linearisation de reaction
RU2727612C1 (ru) * 2019-11-01 2020-07-22 Федеральное государственное бюджетное образовательное учреждение высшего образования "Московский авиационный институт (национальный исследовательский университет)" Способ формирования астатических быстродействующих демпферов летательных аппаратов
CN111007721B (zh) * 2019-12-11 2022-11-25 南通大学 一种线性定常系统中采样周期动态选择方法
CN111045441B (zh) * 2019-12-19 2022-04-08 南京航空航天大学 一种高超声速飞行器传感器复合故障自愈合控制方法
CN111142550B (zh) * 2020-01-09 2021-07-27 上海交通大学 民用飞机辅助驾驶控制方法、系统及飞行品质评估方法
CN111158386B (zh) * 2020-01-14 2021-02-02 北京航空航天大学 一种干扰自主免疫的无人机姿态控制系统及实现方法
CN112327922B (zh) * 2020-11-18 2022-04-22 南京航空航天大学 一种飞翼无人机自主起降综合控制方法
CN113110042B (zh) * 2021-03-22 2022-11-22 青岛科技大学 一种列车容错控制方法
US11592846B1 (en) 2021-11-10 2023-02-28 Beta Air, Llc System and method for autonomous flight control with mode selection for an electric aircraft
CN114415715B (zh) * 2021-12-17 2024-02-27 北京天玛智控科技股份有限公司 多无人机集成系统的控制方法及装置
KR102748340B1 (ko) * 2021-12-22 2024-12-31 주식회사 드론프릭 드론 시뮬레이션 장치
CN119759060B (zh) * 2024-12-25 2025-11-04 北京航空航天大学 一种异构无人机集群弹性安全控制方法、装置、设备及介质

Family Cites Families (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3848833A (en) * 1972-07-14 1974-11-19 Sperry Rand Corp Aircraft automatic flight control system
US3927306A (en) * 1974-03-29 1975-12-16 Sperry Rand Corp Helicopter flight path control
GB1502184A (en) * 1974-07-05 1978-02-22 Sperry Rand Corp Automatic flight control systems
CA1118101A (fr) * 1977-06-02 1982-02-09 Jerry Doniger Systeme digital de guidage en vol
US4308521A (en) * 1979-02-12 1981-12-29 The United States Of America As Represented By The Secretary Of The Air Force Multiple-invariant space-variant optical processing
US4373184A (en) * 1979-12-26 1983-02-08 The Boeing Company Vertical flight path steering system for aircraft
DE3279929D1 (en) 1982-06-16 1989-10-12 Boeing Co Autopilot flight director system
WO1984001345A1 (fr) * 1982-09-30 1984-04-12 Boeing Co Systeme de controle de vol base sur la puissance totale
US5016177A (en) * 1983-05-31 1991-05-14 The Boeing Company Aircraft flight path angle display system
US4649484A (en) 1983-08-01 1987-03-10 The Boeing Company Avionic control system
JPH0629039B2 (ja) * 1986-01-10 1994-04-20 日産自動車株式会社 車両運動状態量推定装置
US4922412A (en) * 1986-10-09 1990-05-01 The Babcock & Wilcox Company Apparatus and method using adaptive gain scheduling
US4980835A (en) * 1988-10-13 1990-12-25 United Technologies Corporation Control law system for X-Wing aircraft
US5001646A (en) * 1988-12-19 1991-03-19 Mcdonnell Douglas Corporation Automated helicopter flight control system
DE3929404A1 (de) 1989-09-05 1991-03-07 Bodenseewerk Geraetetech Verfahren und vorrichtung zum erkennen und identifizieren von fehlern an sensoren
US5297052A (en) 1989-10-16 1994-03-22 The Boeing Company Integrated fault-tolerant air data inertial reference system
JP2656637B2 (ja) * 1989-11-22 1997-09-24 株式会社日立製作所 プロセス制御システム及び発電プラントプロセス制御システム
US5025381A (en) * 1990-01-02 1991-06-18 General Electric Company Attitude control compensator for flexible spacecraft
US5274554A (en) 1991-02-01 1993-12-28 The Boeing Company Multiple-voting fault detection system for flight critical actuation control systems
US5497324A (en) * 1991-05-20 1996-03-05 General Motors Corporation Vehicle suspension system with gain scheduling
US5289377A (en) 1991-08-12 1994-02-22 Trw Inc. Fault-tolerant solid-state flight data recorder
US5493497A (en) 1992-06-03 1996-02-20 The Boeing Company Multiaxis redundant fly-by-wire primary flight control system
US5379210A (en) * 1992-07-24 1995-01-03 M&M Software Products, Inc. Natural tracking controller
US5581665A (en) * 1992-10-27 1996-12-03 Matsushita Electric Industrial Co., Ltd. Three-dimensional object movement and transformation processing apparatus for performing movement and transformation of an object in a three-diamensional space
US5416699A (en) * 1992-11-18 1995-05-16 United Technologies Corporation Propeller speed control having control parameters based on system dynamic characteristics
US5452865A (en) * 1993-06-28 1995-09-26 The Boeing Company Aircraft frequency adaptive modal suppression system
US5581666A (en) * 1993-08-04 1996-12-03 Anderson; Robert J. Modular architecture for robotics and teleoperation
US5446666A (en) * 1994-05-17 1995-08-29 The Boeing Company Ground state-fly state transition control for unique-trim aircraft flight control system
US5631830A (en) * 1995-02-03 1997-05-20 Loral Vought Systems Corporation Dual-control scheme for improved missle maneuverability
JP3422393B2 (ja) * 1995-02-24 2003-06-30 本田技研工業株式会社 内燃機関の空燃比制御装置
JPH08263143A (ja) * 1995-03-23 1996-10-11 Fanuc Ltd 外乱オブザーバを用いた制御ゲイン切り替え方式
US5615119A (en) * 1995-06-07 1997-03-25 Aurora Flight Sciences Corporation Fault tolerant automatic control system utilizing analytic redundancy
US6085127A (en) 1997-03-18 2000-07-04 Aurora Flight Sciences Corporation Fault tolerant automatic control system utilizing analytic redundancy
US5735134A (en) * 1996-05-30 1998-04-07 Massachusetts Institute Of Technology Set point optimization in vapor compression cycles
US6014598A (en) 1996-06-28 2000-01-11 Arcelik A.S. Model-based fault detection system for electric motors
DE19636443A1 (de) 1996-09-07 1998-03-12 Bosch Gmbh Robert Vorrichtung und Verfahren zur Überwachung von Sensoren in einem Fahrzeug
CA2243266C (fr) * 1996-12-12 2003-10-14 Shin Caterpillar Mitsubishi Ltd. Dispositif de commande d'engin de construction
US5944049A (en) * 1997-07-15 1999-08-31 Applied Materials, Inc. Apparatus and method for regulating a pressure in a chamber
US6115654A (en) 1997-12-23 2000-09-05 Simmonds Precision Products, Inc. Universal sensor interface system and method
US6046560A (en) * 1998-03-20 2000-04-04 Trw Inc. Electric assist steering system having an improved motor current controller with gain scheduler
US6014578A (en) 1998-08-06 2000-01-11 Meotronic, Inc. Ambulatory recorder having method of configuring size of data subject to loss in volatile memory

Also Published As

Publication number Publication date
DE60109772D1 (de) 2005-05-04
US6539290B1 (en) 2003-03-25
IL153172A (en) 2009-09-22
CA2748509C (fr) 2016-02-09
EP1526416A3 (fr) 2006-10-04
JP2003535412A (ja) 2003-11-25
US6859689B2 (en) 2005-02-22
WO2001092972A2 (fr) 2001-12-06
CA2410910A1 (fr) 2001-12-06
KR20030060776A (ko) 2003-07-16
AU6348701A (en) 2001-12-11
EP1290508A2 (fr) 2003-03-12
EP1290508B1 (fr) 2005-03-30
ES2238444T3 (es) 2005-09-01
CA2748509A1 (fr) 2001-12-06
US20030191561A1 (en) 2003-10-09
ATE292295T1 (de) 2005-04-15
JP4570842B2 (ja) 2010-10-27
WO2001092972A3 (fr) 2002-08-15
KR100804355B1 (ko) 2008-02-15
AU2001263487B2 (en) 2007-03-15
CA2410910C (fr) 2011-11-15
EP1526416A2 (fr) 2005-04-27
DE60109772T2 (de) 2006-02-16

Similar Documents

Publication Publication Date Title
AU6348701A (en) Method, apparatus and design procedure for controlling multi-input, multi-output(mimo) parameter dependent systems using feedback lti'zation
Spong Partial feedback linearization of underactuated mechanical systems
GB2378261B (en) System & method for controlling a laser
PL354504A1 (en) Method of effecting control in an input- and error-actuated control system and control device for actuating and stopping a processing component of an engineering process
EP2261759B8 (fr) Appareil de commande d'equipement
EP0379215A3 (fr) Procédé de conception de système de régulation et appareil d'assistance à la conception
EP0375731A4 (en) Micropositioner systems and methods
DE69637633D1 (de) Systeme zur Bewegungssteuerung
ES470846A1 (es) Un sistema de posicionamiento que responde a una orden de entrada de posicion para mover un miembro a lo largo de una trayectoria de desplazamiento predeterminada
IL139408A0 (en) Method and apparatus for user and device command and control in a network
AU2002333337A1 (en) Method and device for performing floor control
EP0659547A4 (fr) Amortisseur de per age destine a des presses et procede de commande.
ATE319234T1 (de) Verfahren und vorrichtung zur leistungskontrolle eines ubertragungs-elements
Leeraphan et al. Stable adaptive bilateral control of transparent teleoperation through time-varying delay.
AU2001272602A1 (en) Base station control in telecommunications system
WO2004072743A3 (fr) Automate programmable electrique et procede pour regler les fonctions de cet automate programmable electrique
TW332874B (en) Integral controller
EP0803988A3 (fr) Dispositifs et procédés de contrôle de traitement de données
IL161239A0 (en) Method for controlling electronic parcel compartment systems and an interface for carrying out said method
TW200520381A (en) Apparatus and method for adjusting the impedance of an output driver
KR20030022591A (ko) 시뮬레이션 장치의 반력제어 시스템
AU2000246261A1 (en) Method for controlling an active control system and system using such method
MARCOPOLI et al. Antiwindup analysis and design approaches for MIMO systems(Final Report)
MERWIN Control design of an unstable non-minimum phase aircraft subject to control surface saturation(M. S. Thesis)
BAKHASHWAIN Nonlinear stability analysis and control of dynamical robotic systems(Ph. D. Thesis)