DE69006150T2 - Selbstadaptivverfahren zur steuerungsbetätigung eines physikalischen systems. - Google Patents

Selbstadaptivverfahren zur steuerungsbetätigung eines physikalischen systems.

Info

Publication number
DE69006150T2
DE69006150T2 DE90907100T DE69006150T DE69006150T2 DE 69006150 T2 DE69006150 T2 DE 69006150T2 DE 90907100 T DE90907100 T DE 90907100T DE 69006150 T DE69006150 T DE 69006150T DE 69006150 T2 DE69006150 T2 DE 69006150T2
Authority
DE
Germany
Prior art keywords
self
controlling
physical system
adaptive method
adaptive
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
DE90907100T
Other languages
English (en)
Other versions
DE69006150D1 (de
Inventor
Alain Martin
Joel Houdemont
Jean-Philippe Jahier
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.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of DE69006150D1 publication Critical patent/DE69006150D1/de
Application granted granted Critical
Publication of DE69006150T2 publication Critical patent/DE69006150T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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 or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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
    • 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
DE90907100T 1989-04-18 1990-04-13 Selbstadaptivverfahren zur steuerungsbetätigung eines physikalischen systems. Expired - Fee Related DE69006150T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR8905145A FR2645979B1 (de) 1989-04-18 1989-04-18
PCT/FR1990/000277 WO1990013077A1 (fr) 1989-04-18 1990-04-13 Procede auto-adaptatif de commande en pilotage d'un systeme physique

Publications (2)

Publication Number Publication Date
DE69006150D1 DE69006150D1 (de) 1994-03-03
DE69006150T2 true DE69006150T2 (de) 1994-05-05

Family

ID=9380865

Family Applications (1)

Application Number Title Priority Date Filing Date
DE90907100T Expired - Fee Related DE69006150T2 (de) 1989-04-18 1990-04-13 Selbstadaptivverfahren zur steuerungsbetätigung eines physikalischen systems.

Country Status (6)

Country Link
EP (1) EP0419644B1 (de)
JP (1) JPH03505645A (de)
CA (1) CA2031534A1 (de)
DE (1) DE69006150T2 (de)
FR (1) FR2645979B1 (de)
WO (1) WO1990013077A1 (de)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6244536B1 (en) * 1997-11-26 2001-06-12 The United States Of America As Represented By The Secretary Of The Air Force Air to air homing missile guidance
JP3281334B2 (ja) 1999-08-11 2002-05-13 株式会社豊田中央研究所 同定用信号の設定装置
CN106382853B (zh) * 2016-10-11 2017-12-15 北京航空航天大学 一种带终端弹道倾角和攻角约束奇异摄动次优制导律
CN108828946B (zh) * 2018-07-06 2021-04-27 合肥工业大学 一种用于火箭整流罩减震降噪的自适应控制方法
CN111176297A (zh) * 2020-01-21 2020-05-19 大连海事大学 一种基于多目标dmc预测控制算法的地铁列车跟踪控制方法及系统

Also Published As

Publication number Publication date
FR2645979B1 (de) 1991-11-15
WO1990013077A1 (fr) 1990-11-01
CA2031534A1 (en) 1990-10-19
JPH03505645A (ja) 1991-12-05
EP0419644A1 (de) 1991-04-03
FR2645979A1 (de) 1990-10-19
DE69006150D1 (de) 1994-03-03
EP0419644B1 (de) 1994-01-19

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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