FR2421416A1 - Systeme de servo-commande a deux canaux pour pilote automatique - Google Patents
Systeme de servo-commande a deux canaux pour pilote automatiqueInfo
- Publication number
- FR2421416A1 FR2421416A1 FR7907544A FR7907544A FR2421416A1 FR 2421416 A1 FR2421416 A1 FR 2421416A1 FR 7907544 A FR7907544 A FR 7907544A FR 7907544 A FR7907544 A FR 7907544A FR 2421416 A1 FR2421416 A1 FR 2421416A1
- Authority
- FR
- France
- Prior art keywords
- channel
- control system
- servo
- automatic pilot
- channel servo
- Prior art date
- 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.)
- Withdrawn
Links
- 238000012806 monitoring device Methods 0.000 abstract 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
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B9/00—Safety arrangements
- G05B9/02—Safety arrangements electric
- G05B9/03—Safety arrangements electric with multiple-channel loop, i.e. redundant control systems
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Safety Devices In Control Systems (AREA)
- Control Of Multiple Motors (AREA)
Abstract
L'invention concerne un système de servo-commande à deux canaux pour pilote automatique. Ledit système comporte un servo-moteur dans chaque canal produisant un mouvement identique de sortie en réponse à un signal de commande. Des tachymètres délivrent des signaux proportionnels à la vitesse des servo-moteurs respectifs. Un différentiel alimenté par les servo-moteurs est accouplé à la gouverne et commande un dispositif de réaction délivrant des signaux aux canaux respectifs pour permettre de détecter une panne éventuelle de l'un de ces derniers. Un dispositif de surveillance interrompt le fonctionnement du canal défaillant. Application au pilotage automatique d'engins aériens.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/890,745 US4162438A (en) | 1978-03-27 | 1978-03-27 | Dual servo automatic pilot with improved failure monitoring |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2421416A1 true FR2421416A1 (fr) | 1979-10-26 |
Family
ID=25397091
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7907544A Withdrawn FR2421416A1 (fr) | 1978-03-27 | 1979-03-26 | Systeme de servo-commande a deux canaux pour pilote automatique |
Country Status (9)
Country | Link |
---|---|
US (1) | US4162438A (fr) |
JP (1) | JPS54132998A (fr) |
BR (1) | BR7901764A (fr) |
CA (1) | CA1114477A (fr) |
DE (1) | DE2912107A1 (fr) |
FR (1) | FR2421416A1 (fr) |
GB (1) | GB2017342B (fr) |
IL (1) | IL56798A (fr) |
IT (1) | IT1206961B (fr) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4916612A (en) * | 1987-11-02 | 1990-04-10 | The Boeing Company | Dual channel signal selection and fault detection system |
FR2624964B1 (fr) * | 1987-12-22 | 1990-06-01 | Aerospatiale | Systeme de reference de vitesse pour le pilotage d'un aeronef |
US4858491A (en) * | 1988-01-21 | 1989-08-22 | Plessey Incorporated | Fail-free actuator assembly |
US5274554A (en) * | 1991-02-01 | 1993-12-28 | The Boeing Company | Multiple-voting fault detection system for flight critical actuation control systems |
FR2679077B1 (fr) * | 1991-07-09 | 1993-09-24 | Thomson Csf | Dispositif motorise comportant une generatrice tachymetrique configurable en moteur de secours. |
US5790407A (en) * | 1994-07-08 | 1998-08-04 | Bandit Lites | Time-based control system |
US5670856A (en) * | 1994-11-07 | 1997-09-23 | Alliedsignal Inc. | Fault tolerant controller arrangement for electric motor driven apparatus |
US5919267A (en) * | 1997-04-09 | 1999-07-06 | Mcdonnell Douglas Corporation | Neural network fault diagnostics systems and related method |
US5929549A (en) * | 1998-04-02 | 1999-07-27 | Pacific Scientific Company | Fault tolerant electric machine |
US6437529B1 (en) * | 1998-05-04 | 2002-08-20 | Comair Rotron, Inc. | Multi-stator motor with independent stator circuits |
US6013996A (en) * | 1998-07-27 | 2000-01-11 | The United States Of America As Represented By The Administrator Of National Aeronautics And Space Adminstration | Precision stop control for motors |
JP4096481B2 (ja) * | 2000-01-21 | 2008-06-04 | 株式会社Ihi | サーボ制御装置 |
DE10064673B4 (de) * | 2000-12-22 | 2005-02-24 | Renk Ag | Fehlertolerante elektromechanische Stelleinrichtung |
US6573672B2 (en) * | 2001-06-29 | 2003-06-03 | Honeywell International Inc. | Fail passive servo controller |
US6776376B2 (en) | 2002-10-18 | 2004-08-17 | Hamilton Sunstrand | Flight control surface actuation system |
FR2852683B1 (fr) * | 2003-03-19 | 2005-05-20 | Airbus France | Procede et dispositif d'aide au pilotage d'un aeronef lors d'une approche de non precision pendant une phase d'atterrissage. |
US8070091B2 (en) * | 2008-10-08 | 2011-12-06 | Honeywell International Inc. | Electromechanical actuation system and method |
EP3005005A2 (fr) * | 2013-05-30 | 2016-04-13 | Eaton Corporation | Architecture de commande électronique tolérante aux pannes destinée au système de fonctionnement d'un aéronef |
US10101194B2 (en) * | 2015-12-31 | 2018-10-16 | General Electric Company | System and method for identifying and recovering from a temporary sensor failure |
CN110745255B (zh) * | 2019-10-25 | 2023-03-03 | 中国航空工业集团公司沈阳飞机设计研究所 | 一种飞机伺服作动系统开车前自检方法 |
US11939042B2 (en) | 2020-09-09 | 2024-03-26 | Eaton Intelligent Power Limited | Control surface actuation synchronization system |
FR3113889A1 (fr) | 2020-09-09 | 2022-03-11 | Eaton Intelligent Power Limited | Système de synchronisation d'actionnement de gouverne |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1548718A (fr) * | 1965-12-06 | 1968-12-06 | ||
FR2304951A1 (fr) * | 1975-03-17 | 1976-10-15 | Sperry Rand Corp | Systeme de commande pour les engins dont la navigation peut etre commandee, notamment les engins aeriens |
US4078750A (en) * | 1977-03-08 | 1978-03-14 | United Technologies Corporation | Speed-variable limits in fail-safe actuators |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3504248A (en) * | 1967-05-10 | 1970-03-31 | Sperry Rand Corp | Dual channel servo system having torque equalization |
US3719878A (en) * | 1971-09-27 | 1973-03-06 | Sperry Rand Corp | Digital automatic control system with pseudo position feedback and monitor |
US4094481A (en) * | 1977-06-30 | 1978-06-13 | Sperry Rand Corporation | Fail passive dual servo with continuous motor speed and acceleration and monitoring |
-
1978
- 1978-03-27 US US05/890,745 patent/US4162438A/en not_active Expired - Lifetime
- 1978-12-21 CA CA318,339A patent/CA1114477A/fr not_active Expired
-
1979
- 1979-03-05 GB GB7907701A patent/GB2017342B/en not_active Expired
- 1979-03-06 IL IL56798A patent/IL56798A/xx unknown
- 1979-03-22 BR BR7901764A patent/BR7901764A/pt unknown
- 1979-03-26 IT IT48484/79A patent/IT1206961B/it active
- 1979-03-26 FR FR7907544A patent/FR2421416A1/fr not_active Withdrawn
- 1979-03-27 DE DE2912107A patent/DE2912107A1/de not_active Withdrawn
- 1979-03-27 JP JP3514579A patent/JPS54132998A/ja active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1548718A (fr) * | 1965-12-06 | 1968-12-06 | ||
FR2304951A1 (fr) * | 1975-03-17 | 1976-10-15 | Sperry Rand Corp | Systeme de commande pour les engins dont la navigation peut etre commandee, notamment les engins aeriens |
US4078750A (en) * | 1977-03-08 | 1978-03-14 | United Technologies Corporation | Speed-variable limits in fail-safe actuators |
Also Published As
Publication number | Publication date |
---|---|
US4162438A (en) | 1979-07-24 |
CA1114477A (fr) | 1981-12-15 |
DE2912107A1 (de) | 1979-10-04 |
BR7901764A (pt) | 1979-11-20 |
IL56798A (en) | 1982-07-30 |
JPS54132998A (en) | 1979-10-16 |
GB2017342A (en) | 1979-10-03 |
GB2017342B (en) | 1982-10-20 |
IT1206961B (it) | 1989-05-17 |
IT7948484A0 (it) | 1979-03-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CD | Change of name or company name | ||
ST | Notification of lapse |