IT8220491A0 - Sistema automatico ad anello esterno di centraggio degli azionatori ad anello interno di un aeromobile. - Google Patents

Sistema automatico ad anello esterno di centraggio degli azionatori ad anello interno di un aeromobile.

Info

Publication number
IT8220491A0
IT8220491A0 IT8220491A IT2049182A IT8220491A0 IT 8220491 A0 IT8220491 A0 IT 8220491A0 IT 8220491 A IT8220491 A IT 8220491A IT 2049182 A IT2049182 A IT 2049182A IT 8220491 A0 IT8220491 A0 IT 8220491A0
Authority
IT
Italy
Prior art keywords
centering
aircraft
actuators
outer ring
inner ring
Prior art date
Application number
IT8220491A
Other languages
English (en)
Other versions
IT8220491A1 (it
IT1151537B (it
Inventor
Stuart Cammett Wright
Don Luis Adams
William Christian Fischer
David John Verzella
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of IT8220491A0 publication Critical patent/IT8220491A0/it
Publication of IT8220491A1 publication Critical patent/IT8220491A1/it
Application granted granted Critical
Publication of IT1151537B publication Critical patent/IT1151537B/it

Links

Classifications

    • 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
    • G05D1/0833—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability using limited authority control

Landscapes

  • Engineering & Computer Science (AREA)
  • Computer Security & Cryptography (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)
IT20491/82A 1981-03-30 1982-03-30 Sistema automatico ad anello esterno di centraggio degli azionatori ad anello interno di un aeromobile IT1151537B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/249,299 US4385355A (en) 1981-03-30 1981-03-30 Automatic outer loop centering of aircraft inner loop

Publications (3)

Publication Number Publication Date
IT8220491A0 true IT8220491A0 (it) 1982-03-30
IT8220491A1 IT8220491A1 (it) 1983-09-30
IT1151537B IT1151537B (it) 1986-12-24

Family

ID=22942875

Family Applications (1)

Application Number Title Priority Date Filing Date
IT20491/82A IT1151537B (it) 1981-03-30 1982-03-30 Sistema automatico ad anello esterno di centraggio degli azionatori ad anello interno di un aeromobile

Country Status (6)

Country Link
US (1) US4385355A (it)
JP (1) JPH0641279B2 (it)
BR (1) BR8201662A (it)
DE (1) DE3210867A1 (it)
GB (1) GB2095869B (it)
IT (1) IT1151537B (it)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4460964A (en) * 1981-08-31 1984-07-17 Sperry Corporation Multiaxis hardover protection apparatus for automatic flight control systems
US4500967A (en) * 1981-11-27 1985-02-19 United Technologies Corporation Aircraft short-term roll attitude retention system
US4592055A (en) * 1983-05-02 1986-05-27 United Technologies Corporation Outer-loop monitor for aircraft automatic flight control system
US4580223A (en) * 1983-11-07 1986-04-01 United Technologies Corporation Incorporation of pitch bias actuator function into an existing AFCS
EP0183712A1 (en) * 1984-03-13 1986-06-11 R. DAKIN & COMPANY Sound responsive toy
US5446666A (en) * 1994-05-17 1995-08-29 The Boeing Company Ground state-fly state transition control for unique-trim aircraft flight control system
FR2787763B1 (fr) * 1998-12-24 2001-02-23 Eurocopter France Dispositif d'aide au recentrage d'un organe de commande d'un aeronef
JP5594996B2 (ja) 2009-09-14 2014-09-24 三菱重工業株式会社 航空機の操縦システム
FR2951330B1 (fr) * 2009-10-13 2013-03-08 Messier Bugatti Reseau de pilotage pour actionneurs mono ou multimoteurs, particulierement adapte a des applications aeronautiques telles que l'alimentation de moteurs de boitiers d'accrochage
US8712607B2 (en) * 2009-12-07 2014-04-29 Sikorsky Aircraft Corporation Systems and methods for velocity profile based approach to point control
US20220350347A1 (en) * 2021-04-30 2022-11-03 Bell Textron Inc. Nested-loop model-following control law

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5160397A (en) * 1974-11-22 1976-05-26 Kawasaki Heavy Ind Ltd Kaitenyokukokuki niokeru jidohikoseigyosochi
CA1050633A (en) * 1974-12-19 1979-03-13 Ronald J. Miller Semi-automatic flight control system utilizing limited authority stabilization system
US4029271A (en) * 1976-04-07 1977-06-14 United Technologies Corporation Automatic approach to hover system
US4078750A (en) * 1977-03-08 1978-03-14 United Technologies Corporation Speed-variable limits in fail-safe actuators
US4213584A (en) * 1978-10-04 1980-07-22 United Technologies Corporation Helicopter hover stability and cruise gust effect alleviation
US4279391A (en) * 1979-01-24 1981-07-21 United Technologies Corporation Desensitizing helicopter control response to inadvertent pilot inputs
US4382283A (en) * 1980-08-08 1983-05-03 United Technologies Corporation Helicopter attitude and airspeed acquisition and retention system

Also Published As

Publication number Publication date
DE3210867A1 (de) 1982-10-14
BR8201662A (pt) 1983-02-16
IT8220491A1 (it) 1983-09-30
IT1151537B (it) 1986-12-24
GB2095869A (en) 1982-10-06
JPS57178998A (en) 1982-11-04
JPH0641279B2 (ja) 1994-06-01
US4385355A (en) 1983-05-24
DE3210867C2 (it) 1993-06-09
GB2095869B (en) 1984-08-01

Similar Documents

Publication Publication Date Title
ES512305A0 (es) Sistema digital para la representacion visual de imagenes.
IT8223201A0 (it) Sospensione per giroscopio laserad anello.
IT1155701B (it) Differenziale particolarmente per autoveicoli con meccanismo di disimpegno ad anello
IT8205229A0 (it) Sistema di accoppiamento di elementi meccanici rotanti.
IT8220491A0 (it) Sistema automatico ad anello esterno di centraggio degli azionatori ad anello interno di un aeromobile.
IT8122722A0 (it) Anello di tenuta.
IT8221862A0 (it) Giroscopio laser ad anello con specchi doppler.
IT8222115A0 (it) Giroscopio laser ad anello con compensazione.
IT8221205A0 (it) Laser ad anello. trasduttore captatore di sovraeccitazione per giroscopio
IT1119377B (it) Contenitore per cartuccia con un dispositivo ad anello di centraggio e procedimento per la fabbricazione di tale dispositivo
IT1210931B (it) Metodo e sistema per la trasmissione di segnali ottici.
IT8220490A0 (it) Sistema azionatore ad impulsi per aeromobili.
IT1171927B (it) Comparatore ad anello per il controllo di dimensioni diametrali esterne
IT8220489A0 (it) Sistema di innesto e disinnesto automatico del controllo della velocita' relativa di un aeromobile.
IT8119316A0 (it) Anello interno per cuscinetto arotolamento.
ES268501Y (es) Brida para elementos tubulares.
NO156653C (no) Fremgangsmaate for fremstilling av et antibiotikum.
IT8220488A0 (it) Sistema di sincronizzazione dei segnali di riferimento dei parametri di un aeromobile a duplice risposta.
BR8203041A (pt) Tampao amovivel para selar temporariamente o interior de um membro anular
ES510972A0 (es) "sistema de revestimiento para un cateter masculino exterior".
IT8420761A0 (it) Sistema di sorveglianza dell'attivita' dell'anello esterno per sistemi di controllo automatici.
IT8219718A0 (it) Anello di tenuta.
IT8025885A0 (it) Anello di fissaggio.
IT7926987A0 (it) Anello interno per anello difilatura.
IT8222332A0 (it) Sistema di fissaggio di anelli difilatura sulla piattabanda porta anelli di una macchina di filatura.

Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19970228