BR7601556A - Aperfeicoamento em sistema para controlar o movimento de um elemento de controle de atitude posicionavel de aviao e em sistema automatico de controle de voo - Google Patents
Aperfeicoamento em sistema para controlar o movimento de um elemento de controle de atitude posicionavel de aviao e em sistema automatico de controle de vooInfo
- Publication number
- BR7601556A BR7601556A BR7601556A BR7601556A BR7601556A BR 7601556 A BR7601556 A BR 7601556A BR 7601556 A BR7601556 A BR 7601556A BR 7601556 A BR7601556 A BR 7601556A BR 7601556 A BR7601556 A BR 7601556A
- Authority
- BR
- Brazil
- Prior art keywords
- control
- positionable
- improvement
- movement
- automatic flight
- Prior art date
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
- 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)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Safety Devices In Control Systems (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Navigation (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/558,582 US4035705A (en) | 1975-03-17 | 1975-03-17 | Fail-safe dual channel automatic pilot with maneuver limiting |
Publications (1)
Publication Number | Publication Date |
---|---|
BR7601556A true BR7601556A (pt) | 1976-09-14 |
Family
ID=24230118
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR7601556A BR7601556A (pt) | 1975-03-17 | 1976-03-15 | Aperfeicoamento em sistema para controlar o movimento de um elemento de controle de atitude posicionavel de aviao e em sistema automatico de controle de voo |
Country Status (8)
Country | Link |
---|---|
US (1) | US4035705A (pt) |
JP (1) | JPS51116600A (pt) |
BR (1) | BR7601556A (pt) |
CA (1) | CA1050635A (pt) |
DE (1) | DE2611288A1 (pt) |
FR (1) | FR2304951A1 (pt) |
GB (1) | GB1534353A (pt) |
IT (1) | IT1074450B (pt) |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4078750A (en) * | 1977-03-08 | 1978-03-14 | United Technologies Corporation | Speed-variable limits in fail-safe actuators |
CA1118101A (en) * | 1977-06-02 | 1982-02-09 | Jerry Doniger | Digital flight guidance system |
US4094481A (en) * | 1977-06-30 | 1978-06-13 | Sperry Rand Corporation | Fail passive dual servo with continuous motor speed and acceleration and monitoring |
US4234833A (en) * | 1978-01-19 | 1980-11-18 | A. E. Moore Company, Inc. | Door operator system using counter circuit for determining limit positions |
US4159444A (en) * | 1978-03-21 | 1979-06-26 | Sperry Rand Corporation | Fail operational dual electromechanical servo actuator for aircraft with model monitoring |
US4162438A (en) * | 1978-03-27 | 1979-07-24 | Sperry Rand Corporation | Dual servo automatic pilot with improved failure monitoring |
US4209734A (en) * | 1978-03-27 | 1980-06-24 | Sperry Corporation | Dynamic equalization system for dual channel automatic pilot |
FR2430633A1 (fr) * | 1978-07-07 | 1980-02-01 | Sfena | Systeme de commande auto-surveille, d'un processus |
DE2831500A1 (de) * | 1978-07-14 | 1980-01-24 | Nash Frazer Ltd | Motorbetriebene betaetigungseinrichtung |
US4378518A (en) * | 1979-06-15 | 1983-03-29 | Edo-Aire Mitchell | Rate based autopilot system |
US4398242A (en) * | 1980-02-25 | 1983-08-09 | The Boeing Company | Electronic controller |
US4370706A (en) * | 1980-09-26 | 1983-01-25 | The Bendix Corporation | Controller for a dual servo system |
JPS6225608A (ja) * | 1985-07-26 | 1987-02-03 | Mitsui Kaiyo Kaihatsu Kk | 海洋構造物のラツク・アンド・ピニオン式昇降装置の過負荷防止装置 |
US4807516A (en) * | 1987-04-23 | 1989-02-28 | The Boeing Company | Flight control system employing three controllers operating a dual actuator |
DE3926705A1 (de) * | 1988-12-21 | 1990-06-28 | Gen Electric | Anordnung und vorrichtung zum regeln eines gasturbinentriebwerks |
US5331266A (en) * | 1992-06-24 | 1994-07-19 | Hughes Aircraft Company | Cooperative differential drive system |
US5502364A (en) * | 1993-07-26 | 1996-03-26 | The Boeing Company | Aircraft automatic throttle forward stop servo system and method |
US5587640A (en) * | 1994-09-28 | 1996-12-24 | Tetra Laval Holdings & Finance S.A. | Delayed safety braking apparatus for a servomotor control system |
JP3195918B2 (ja) | 1999-03-12 | 2001-08-06 | 株式会社コミュータヘリコプタ先進技術研究所 | ヘリコプタ用飛行制御装置 |
JP3012644B1 (ja) | 1999-03-18 | 2000-02-28 | 株式会社コミュータヘリコプタ先進技術研究所 | サ―ボアクチュエ―タ装置および航空機操縦制御装置 |
DE10064673B4 (de) * | 2000-12-22 | 2005-02-24 | Renk Ag | Fehlertolerante elektromechanische Stelleinrichtung |
US20040059474A1 (en) | 2002-09-20 | 2004-03-25 | Boorman Daniel J. | Apparatuses and methods for displaying autoflight information |
US6776376B2 (en) | 2002-10-18 | 2004-08-17 | Hamilton Sunstrand | Flight control surface actuation system |
US7188007B2 (en) * | 2003-12-24 | 2007-03-06 | The Boeing Company | Apparatuses and methods for displaying and receiving tactical and strategic flight guidance information |
US7549605B2 (en) * | 2005-06-27 | 2009-06-23 | Honeywell International Inc. | Electric flight control surface actuation system for aircraft flaps and slats |
DE102008022092A1 (de) * | 2008-05-05 | 2009-11-19 | Airbus Deutschland Gmbh | Fehlertolerantes Stellsystem zur Verstellung von Klappen eines Flugzeugs mit einer Verstell-Kinematik mit feststehender Drehachse |
US8180562B2 (en) * | 2008-06-04 | 2012-05-15 | The Boeing Company | System and method for taxi route entry parsing |
US8386167B2 (en) | 2008-11-14 | 2013-02-26 | The Boeing Company | Display of taxi route control point information |
US8583294B2 (en) | 2011-04-11 | 2013-11-12 | Hamilton Sundstrand Corporation | Actuation control system |
US9731837B2 (en) | 2015-02-17 | 2017-08-15 | Honeywell International Inc. | Servo transparency warning system and method |
CN110789737B (zh) * | 2019-10-29 | 2024-03-29 | 贵州航天控制技术有限公司 | 一种空间有源太阳翼展开机构驱动控制电路及其方法 |
US11733714B2 (en) * | 2021-01-14 | 2023-08-22 | Textron Innovations Inc. | Intelligent aircraft and rotorcraft load factor and stall protection |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1210071B (de) * | 1957-09-05 | 1966-02-03 | Smith & Sons Ltd S | Selbsttaetige Regelvorrichtung, bei der aus Sicherheitsgruenden mehrere parallele Steuerkanaele vorgesehen sind |
GB1081792A (en) * | 1965-01-25 | 1967-08-31 | Sperry Gyroscope Co Ltd | Electrical transmission system |
US3422327A (en) * | 1965-09-17 | 1969-01-14 | Sperry Rand Corp | Multiple channel fail functional system for discretely disconnecting malfunctioning sub-systems |
US3489889A (en) * | 1966-09-28 | 1970-01-13 | North American Rockwell | Redundant signalling apparatus having improved failure exclusion |
US3493836A (en) * | 1967-03-30 | 1970-02-03 | Sperry Rand Corp | Static and dynamic failure monitor for aircraft automatic pilots |
US3462662A (en) * | 1967-04-12 | 1969-08-19 | Lear Siegler Inc | Monitoring and fault correction system for a multiple channel servo actuator |
US3504248A (en) * | 1967-05-10 | 1970-03-31 | Sperry Rand Corp | Dual channel servo system having torque equalization |
US3679956A (en) * | 1970-02-02 | 1972-07-25 | Ltv Electrosystems Inc | Multiple servomotor actuator |
US3593092A (en) * | 1970-02-02 | 1971-07-13 | Ltv Electrosystems Inc | Multiple output multiplex actuator |
US3659173A (en) * | 1970-06-19 | 1972-04-25 | Bendix Corp | Aircraft control system including limiting means |
US3827659A (en) * | 1973-03-07 | 1974-08-06 | Bendix Corp | Control system monitoring apparatus having minimal nuisance alarm characteristics |
US3807666A (en) * | 1973-06-11 | 1974-04-30 | Sperry Rand Corp | Control wheel steering system for aircraft automatic pilots |
-
1975
- 1975-03-17 US US05/558,582 patent/US4035705A/en not_active Expired - Lifetime
-
1976
- 1976-02-10 CA CA245,361A patent/CA1050635A/en not_active Expired
- 1976-03-10 GB GB9460/76A patent/GB1534353A/en not_active Expired
- 1976-03-15 BR BR7601556A patent/BR7601556A/pt unknown
- 1976-03-16 IT IT48598/76A patent/IT1074450B/it active
- 1976-03-16 JP JP51028562A patent/JPS51116600A/ja active Pending
- 1976-03-16 FR FR7607434A patent/FR2304951A1/fr active Granted
- 1976-03-17 DE DE19762611288 patent/DE2611288A1/de not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
IT1074450B (it) | 1985-04-20 |
FR2304951A1 (fr) | 1976-10-15 |
US4035705A (en) | 1977-07-12 |
DE2611288A1 (de) | 1976-11-04 |
CA1050635A (en) | 1979-03-13 |
FR2304951B1 (pt) | 1983-10-21 |
GB1534353A (en) | 1978-12-06 |
JPS51116600A (en) | 1976-10-14 |
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