BR8602323A - Sistema automatico de controle de voo para aeronaves - Google Patents

Sistema automatico de controle de voo para aeronaves

Info

Publication number: BR8602323A
Authority: BR; Brazil
Prior art keywords: aircraft; control system; flight control; automatic flight; automatic
Prior art date: 1985-05-30

Application number

BR8602323A

Other languages

English (en)

Inventor

Dale Dean Davidson

Douglas Gene Endrud

Original Assignee

Sperry 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.)

1985-05-30

Filing date

1986-05-21

Publication date

1987-01-21

1986-05-21 Application filed by Sperry Corp filed Critical Sperry Corp

1987-01-21 Publication of BR8602323A publication Critical patent/BR8602323A/pt

Links

RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 title 1

Classifications

- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F11/00—Error detection; Error correction; Monitoring
- G06F11/07—Responding to the occurrence of a fault, e.g. fault tolerance
- G06F11/16—Error detection or correction of the data by redundancy in hardware
- 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
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls

Landscapes

Engineering & Computer Science (AREA)
General Physics & Mathematics (AREA)
Physics & Mathematics (AREA)
Theoretical Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
General Engineering & Computer Science (AREA)
Quality & Reliability (AREA)
Radar, Positioning & Navigation (AREA)
Remote Sensing (AREA)
Automation & Control Theory (AREA)
Safety Devices In Control Systems (AREA)
Feedback Control In General (AREA)
Ceramic Products (AREA)
Hardware Redundancy (AREA)

BR8602323A 1985-05-30 1986-05-21 Sistema automatico de controle de voo para aeronaves BR8602323A (pt)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US06/739,583 US4799159A (en)	1985-05-30	1985-05-30	Digital automatic flight control system with disparate function monitoring

Publications (1)

Publication Number	Publication Date
BR8602323A true BR8602323A (pt)	1987-01-21

Family

ID=24972957

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BR8602323A BR8602323A (pt)	1985-05-30	1986-05-21	Sistema automatico de controle de voo para aeronaves

Country Status (7)

Country	Link
US (1)	US4799159A (pt)
EP (1)	EP0207611B1 (pt)
JP (1)	JPS61276036A (pt)
BR (1)	BR8602323A (pt)
CA (1)	CA1262178A (pt)
DE (1)	DE3688265T2 (pt)
IL (1)	IL78896A (pt)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4713757A (en)	1985-06-11	1987-12-15	Honeywell Inc.	Data management equipment for automatic flight control systems having plural digital processors
US5184312A (en) *	1985-10-13	1993-02-02	The Boeing Company	Distributed built-in test equipment system for digital avionics
FR2628858B1 (fr) *	1988-03-15	1990-08-17	Aerospatiale	Systeme de commande de vol pour aeronef
DE3816254A1 (de) *	1988-05-11	1989-11-23	Siemens Ag	Steuereinheit zur lenkung der hinterraeder eines strassenfahrzeuges
US5448480A (en) *	1988-05-11	1995-09-05	Siemens Aktiengesellschaft	Fail-safe operation via controller redundancy for steering the back wheels of a road vehicle
US5377109A (en) *	1992-07-31	1994-12-27	Lear Astronics Corp.	Failsafe digital bus to analog protocol converter system
FR2706153B1 (fr) *	1993-06-07	1995-08-18	Sextant Avionique	Dispositif de pilotage automatique pour aérodynes.
JPH07262148A (ja) *	1994-03-22	1995-10-13	Nec Corp	コンピュータシステム
US5553237A (en) *	1994-12-13	1996-09-03	Base Ten Systems, Inc.	Safety critical monitoring of microprocessor controlled embedded systems
JPH08235006A (ja) *	1995-02-24	1996-09-13	Fujitsu Ltd	状態監視システム
FR2760109B1 (fr) *	1997-02-25	1999-05-28	Sextant Avionique	Procede et dispositif pour l'execution par un processeur unique de plusieurs fonctions de niveaux de criticite differents, avec une grande securite de fonctionnement
US6367031B1 (en) *	1998-12-17	2002-04-02	Honeywell International Inc.	Critical control adaption of integrated modular architecture
US6517396B1 (en) *	2000-07-03	2003-02-11	Stephen W. Into	Boat speed control
US6573672B2 (en) *	2001-06-29	2003-06-03	Honeywell International Inc.	Fail passive servo controller
GB2384313A (en) *	2002-01-18	2003-07-23	Qinetiq Ltd	An attitude sensor
CN100356281C (zh) *	2004-03-16	2007-12-19	清华大学	一种用于飞行器的自动驾驶仪
US7421526B2 (en) *	2005-08-24	2008-09-02	Honeywell International Inc.	Reconfigurable virtual backplane architecture
US7933696B2 (en) *	2006-08-31	2011-04-26	GM Global Technology Operations LLC	Distributed arithmetic logic unit security check
US8015390B1 (en)	2008-03-19	2011-09-06	Rockwell Collins, Inc.	Dissimilar processor synchronization in fly-by-wire high integrity computing platforms and displays
US7852235B1 (en)	2008-04-28	2010-12-14	Rockwell Collins, Inc.	High integrity computing via input synchronization systems and methods
DE102009007215A1 (de) *	2009-02-03	2010-08-05	Siemens Aktiengesellschaft	Automatisierungssystem mit einem programmierbaren Matrixmodul
US8682562B2 (en) *	2009-05-08	2014-03-25	Rolls-Royce Corporation	Turbine engine thrust scheduling
US8151024B2 (en) *	2009-05-28	2012-04-03	Honeywell International Inc.	Reconfigurable virtual backplane systems and methods
CN104123122A (zh) *	2013-04-24	2014-10-29	成都飞机设计研究所	一种非相似三余度飞控计算机的非相似余度软件开发方法
CA3045247A1 (en) *	2016-11-30	2018-06-07	Bombardier Inc.	Aircraft control system with residual error containment
FR3075997B1 (fr) *	2017-12-26	2020-01-10	Thales	Calculateur electronique de mise en oeuvre d'au moins une fonction critique, dispositif electronique, procede et programme d'ordinateur associes
WO2019217636A1 (en)	2018-05-09	2019-11-14	Abb Schweiz Ag	Turbine diagnostics
DE102020107172A1 (de) *	2020-03-16	2021-09-16	Volocopter Gmbh	Verfahren zur Steuerung eines Fluggeräts, Steuerungseinrichtung für ein Fluggerät und Fluggerät mit einer solchen Steuerungseinrichtung

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3688099A (en) *	1971-04-28	1972-08-29	Lear Siegler Inc	Automatic control system with a digital computer
CA1026850A (en) *	1973-09-24	1978-02-21	Smiths Industries Limited	Dual, simultaneously operating control system with fault detection
GB1502184A (en) *	1974-07-05	1978-02-22	Sperry Rand Corp	Automatic flight control systems
US3994456A (en) *	1975-05-29	1976-11-30	Sperry Rand Corporation	Steered lateral course transition control apparatus for aircraft area navigation systems
FR2344063A1 (fr) *	1976-03-10	1977-10-07	Smiths Industries Ltd	Circuit numerique de commande a deux voies au moins
US4342083A (en) *	1980-02-05	1982-07-27	The Bendix Corporation	Communication system for a multiple-computer system
JPS56166562A (en) *	1980-05-23	1981-12-21	Mitsubishi Electric Corp	Data processor
US4370706A (en) *	1980-09-26	1983-01-25	The Bendix Corporation	Controller for a dual servo system
EP0096510B1 (en) *	1982-06-03	1988-07-27	LUCAS INDUSTRIES public limited company	Control system primarily responsive to signals from digital computers
DE3279929D1 (en) *	1982-06-16	1989-10-12	Boeing Co	Autopilot flight director system
US4622667A (en) *	1984-11-27	1986-11-11	Sperry Corporation	Digital fail operational automatic flight control system utilizing redundant dissimilar data processing

1985
- 1985-05-30 US US06/739,583 patent/US4799159A/en not_active Expired - Lifetime
1986
- 1986-01-15 CA CA000499630A patent/CA1262178A/en not_active Expired
- 1986-05-15 JP JP61111764A patent/JPS61276036A/ja active Pending
- 1986-05-19 DE DE8686303800T patent/DE3688265T2/de not_active Expired - Fee Related
- 1986-05-19 EP EP86303800A patent/EP0207611B1/en not_active Expired - Lifetime
- 1986-05-21 BR BR8602323A patent/BR8602323A/pt not_active IP Right Cessation
- 1986-05-23 IL IL78896A patent/IL78896A/xx not_active IP Right Cessation

Also Published As

Publication number	Publication date
EP0207611A3 (en)	1989-03-29
JPS61276036A (ja)	1986-12-06
IL78896A (en)	1990-11-29
DE3688265D1 (de)	1993-05-19
DE3688265T2 (de)	1993-09-09
IL78896A0 (en)	1986-09-30
EP0207611B1 (en)	1993-04-14
EP0207611A2 (en)	1987-01-07
US4799159A (en)	1989-01-17
CA1262178A (en)	1989-10-03

Legal Events

Date	Code	Title	Description
1995-02-21	KD	Notifcation of receipt (letter patent)
1995-03-28	HO	Change of classification	Free format text: INT. CL. 4 G06F 15/50
1995-05-30	FG	Letter patent granted
2008-07-22	B21A	Patent or certificate of addition expired [chapter 21.1 patent gazette]	Free format text: PATENTE EXTINTA EM 21/05/2001
2018-03-27	B15K	Others concerning applications: alteration of classification	Ipc: G06F 11/16 (2006.01), G05D 1/00 (2006.0

Publication	Publication Date	Title
BR8602323A (pt)	1987-01-21	Sistema automatico de controle de voo para aeronaves
BR8803502A (pt)	1989-01-31	Conjunto de controle para um sistema de elevadores
IL76953A0 (en)	1986-04-29	Aircraft airfoil camber automatic control system
BR8406279A (pt)	1985-10-01	Sistema de controle para veiculo
BR8606575A (pt)	1987-10-20	Sistema de controle de embreagem
DE3462866D1 (en)	1987-05-07	Aircraft flight control system
BR8405631A (pt)	1985-09-10	Sistema de controle de inclinacao para helice de inclinacao variavel
DE3480879D1 (de)	1990-02-01	Flugkontrollsystem fuer hubschrauber.
BR8901806A (pt)	1989-11-28	Sistema de controle de velocidade para um elevador
BR8504628A (pt)	1986-07-15	Sistema de controle para um aparelho ministrador
BR8601026A (pt)	1987-01-13	Aparelho de gerenciamento de dados para sistema automatico de controle de voo
DE3687278D1 (de)	1993-01-28	Sink-flugbahnregelung fuer flugzeuge.
GB8525631D0 (en)	1985-11-20	Aircraft flying control systems
EP0084447A3 (en)	1984-11-07	Aircraft automatic flight control systems
BR8306823A (pt)	1984-07-31	Sistema de controle de inclinacao para helice de inclinacao variavel
ES2017738B3 (es)	1991-03-01	Sistema de mando de vuelo electrico con proteccion en incidencia para aeronave.
IL84785A0 (en)	1988-05-31	Flight control optimization system for multi-control surface aircraft
IT8620545A0 (it)	1986-05-23	Controllo per eliche da aereo
BR8602135A (pt)	1987-01-13	Sistema de controle de combustivel
BR8201663A (pt)	1983-02-16	Sistema para posicionamento automatico de superficies aerodinamicas em um eixo de controle de uma aeronave
BR8201662A (pt)	1983-02-16	Sistema para posicionamento automatico de superficies aerodinamicas em eixo de controle de aeronave
BR8703463A (pt)	1988-03-22	Sistema de controle para embreagem automatica
DE3275665D1 (en)	1987-04-16	Aircraft flight control system
GB2131363B (en)	1986-01-08	Aircraft flying control systems
BR8108974A (pt)	1983-01-11	Sistema de controle de combustao