BR8201662A - Sistema para posicionamento automatico de superficies aerodinamicas em eixo de controle de aeronave - Google Patents

Sistema para posicionamento automatico de superficies aerodinamicas em eixo de controle de aeronave

Info

Publication number
BR8201662A
BR8201662A BR8201662A BR8201662A BR8201662A BR 8201662 A BR8201662 A BR 8201662A BR 8201662 A BR8201662 A BR 8201662A BR 8201662 A BR8201662 A BR 8201662A BR 8201662 A BR8201662 A BR 8201662A
Authority
BR
Brazil
Prior art keywords
automatic positioning
control axis
aircraft control
aerodynamic surfaces
aerodynamic
Prior art date
Application number
BR8201662A
Other languages
English (en)
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 BR8201662A publication Critical patent/BR8201662A/pt

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)
BR8201662A 1981-03-30 1982-03-24 Sistema para posicionamento automatico de superficies aerodinamicas em eixo de controle de aeronave BR8201662A (pt)

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 (1)

Publication Number Publication Date
BR8201662A true BR8201662A (pt) 1983-02-16

Family

ID=22942875

Family Applications (1)

Application Number Title Priority Date Filing Date
BR8201662A BR8201662A (pt) 1981-03-30 1982-03-24 Sistema para posicionamento automatico de superficies aerodinamicas em eixo de controle de aeronave

Country Status (6)

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

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
IT8220491A0 (it) 1982-03-30
DE3210867A1 (de) 1982-10-14
IT1151537B (it) 1986-12-24
JPS57178998A (en) 1982-11-04
JPH0641279B2 (ja) 1994-06-01
IT8220491A1 (it) 1983-09-30
DE3210867C2 (pt) 1993-06-09
GB2095869B (en) 1984-08-01
US4385355A (en) 1983-05-24
GB2095869A (en) 1982-10-06

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Legal Events

Date Code Title Description
B21A Patent or certificate of addition expired [chapter 21.1 patent gazette]

Free format text: PATENTE EXTINTA EM 24/03/97