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)
  • Mathematical Optimization (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Evolutionary Computation (AREA)
  • Medical Informatics (AREA)
  • Software Systems (AREA)
  • Algebra (AREA)
  • Mathematical Analysis (AREA)
  • Health & Medical Sciences (AREA)
  • Mathematical Physics (AREA)
  • Pure & Applied Mathematics (AREA)
  • Artificial Intelligence (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (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 (en) 2000-05-30 2001-05-30 Method, apparatus and design procedure for controlling multi-input, multi-output (mimo) parameter dependent systems using feedback lti'zation

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 (xx)
EP (2) EP1290508B1 (xx)
JP (1) JP4570842B2 (xx)
KR (1) KR100804355B1 (xx)
AT (1) ATE292295T1 (xx)
AU (2) AU6348701A (xx)
CA (2) CA2410910C (xx)
DE (1) DE60109772T2 (xx)
ES (1) ES2238444T3 (xx)
IL (2) IL153172A0 (xx)
WO (1) WO2001092972A2 (xx)

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Also Published As

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

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