FR2159084A5 - - Google Patents

Info

Publication number
FR2159084A5
FR2159084A5 FR7239408A FR7239408A FR2159084A5 FR 2159084 A5 FR2159084 A5 FR 2159084A5 FR 7239408 A FR7239408 A FR 7239408A FR 7239408 A FR7239408 A FR 7239408A FR 2159084 A5 FR2159084 A5 FR 2159084A5
Authority
FR
France
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
Application number
FR7239408A
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.)
Vereinigte Flugtechnische Werke Fokker GmbH
Original Assignee
Vereinigte Flugtechnische Werke Fokker GmbH
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 Vereinigte Flugtechnische Werke Fokker GmbH filed Critical Vereinigte Flugtechnische Werke Fokker GmbH
Application granted granted Critical
Publication of FR2159084A5 publication Critical patent/FR2159084A5/fr
Expired 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
FR7239408A 1971-12-31 1972-11-07 Expired FR2159084A5 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2165894A DE2165894C2 (de) 1971-12-31 1971-12-31 Anordnung zur Steuerung und Stabilisierung eines Flugzeuges

Publications (1)

Publication Number Publication Date
FR2159084A5 true FR2159084A5 (fr) 1973-06-15

Family

ID=5829883

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7239408A Expired FR2159084A5 (fr) 1971-12-31 1972-11-07

Country Status (4)

Country Link
US (1) US4243922A (fr)
DE (1) DE2165894C2 (fr)
FR (1) FR2159084A5 (fr)
GB (1) GB1415850A (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE396473B (sv) * 1975-01-14 1977-09-19 Bofors Ab Anordning for dempning av tipp- och girsvengar
GB2399425B (en) * 2003-03-11 2006-05-17 Rolls Royce Plc Improving stability and response of control systems
US7453228B2 (en) * 2006-04-07 2008-11-18 Asml Netherlands B.V. Method for controlling a positioning device, positioning device, and lithographic apparatus provided with a positioning device
CN110231774A (zh) * 2019-04-08 2019-09-13 天津大学 干扰观测变进气道高超声速飞行器模糊协调控制方法

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3109970A (en) * 1959-12-09 1963-11-05 North American Aviation Inc Self-adaptive servo system
US3216676A (en) * 1963-05-20 1965-11-09 Sperry Rand Corp Self-adaptive control system
US3283229A (en) * 1962-05-24 1966-11-01 Honeywell Inc Dual redundant, adaptive motor control with fail safe features
US3361394A (en) * 1966-02-24 1968-01-02 Bendix Corp Flight control system
DE1299453B (de) * 1958-08-18 1969-07-17 Honeywell Inc Regeleinrichtung zur selbstanpassenden Regelung einer Stoergroessen ausgesetzten physikalischen Groesse unter Verwendung eines die Regelstrecke nachbildenden Modells
DE1563883A1 (de) * 1966-04-06 1969-10-02 Ver Flugtechnische Werke Regler nach dem Operatorverstaerkerprinzip

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3001176A (en) * 1953-08-06 1961-09-19 Emi Ltd Message selection in electrical communication or control systems

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1299453B (de) * 1958-08-18 1969-07-17 Honeywell Inc Regeleinrichtung zur selbstanpassenden Regelung einer Stoergroessen ausgesetzten physikalischen Groesse unter Verwendung eines die Regelstrecke nachbildenden Modells
US3109970A (en) * 1959-12-09 1963-11-05 North American Aviation Inc Self-adaptive servo system
US3283229A (en) * 1962-05-24 1966-11-01 Honeywell Inc Dual redundant, adaptive motor control with fail safe features
US3216676A (en) * 1963-05-20 1965-11-09 Sperry Rand Corp Self-adaptive control system
US3361394A (en) * 1966-02-24 1968-01-02 Bendix Corp Flight control system
DE1481522B2 (de) * 1966-02-24 1970-11-26 The Bendix Corp., Detroit, Mich. (V.St.A.) Selbstanpassender Flugregler
DE1563883A1 (de) * 1966-04-06 1969-10-02 Ver Flugtechnische Werke Regler nach dem Operatorverstaerkerprinzip

Also Published As

Publication number Publication date
DE2165894A1 (de) 1973-07-05
DE2165894C2 (de) 1983-01-20
GB1415850A (en) 1975-11-26
US4243922A (en) 1981-01-06

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Legal Events

Date Code Title Description
ST Notification of lapse