FR2396348B2 - Systeme de commande pour les engins dont la navigation peut etre commandee notamment les engins aeriens - Google Patents

Systeme de commande pour les engins dont la navigation peut etre commandee notamment les engins aeriens

Info

Publication number
FR2396348B2
FR2396348B2 FR7818577A FR7818577A FR2396348B2 FR 2396348 B2 FR2396348 B2 FR 2396348B2 FR 7818577 A FR7818577 A FR 7818577A FR 7818577 A FR7818577 A FR 7818577A FR 2396348 B2 FR2396348 B2 FR 2396348B2
Authority
FR
France
Prior art keywords
controlled
control system
particularly aircraft
whose navigation
machinery whose
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.)
Expired
Application number
FR7818577A
Other languages
English (en)
Other versions
FR2396348A2 (fr
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sperry Corp
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.)
Filing date
Publication date
Application filed by Sperry Corp filed Critical Sperry Corp
Publication of FR2396348A2 publication Critical patent/FR2396348A2/fr
Application granted granted Critical
Publication of FR2396348B2 publication Critical patent/FR2396348B2/fr
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0077Control 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)
  • Retarders (AREA)
  • Valves And Accessory Devices For Braking Systems (AREA)
FR7818577A 1977-06-30 1978-06-21 Systeme de commande pour les engins dont la navigation peut etre commandee notamment les engins aeriens Expired FR2396348B2 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/811,653 US4094481A (en) 1977-06-30 1977-06-30 Fail passive dual servo with continuous motor speed and acceleration and monitoring

Publications (2)

Publication Number Publication Date
FR2396348A2 FR2396348A2 (fr) 1979-01-26
FR2396348B2 true FR2396348B2 (fr) 1986-02-28

Family

ID=25207163

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7818577A Expired FR2396348B2 (fr) 1977-06-30 1978-06-21 Systeme de commande pour les engins dont la navigation peut etre commandee notamment les engins aeriens

Country Status (6)

Country Link
US (1) US4094481A (fr)
JP (1) JPS5415299A (fr)
DE (1) DE2826467A1 (fr)
FR (1) FR2396348B2 (fr)
GB (1) GB1600444A (fr)
IT (1) IT1174313B (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4159444A (en) * 1978-03-21 1979-06-26 Sperry Rand Corporation Fail operational dual electromechanical servo actuator for aircraft with model monitoring
US4209734A (en) * 1978-03-27 1980-06-24 Sperry Corporation Dynamic equalization system for dual channel automatic pilot
US4162438A (en) * 1978-03-27 1979-07-24 Sperry Rand Corporation Dual servo automatic pilot with improved failure monitoring
US4398242A (en) * 1980-02-25 1983-08-09 The Boeing Company Electronic controller
JPS57105323A (en) * 1980-12-23 1982-06-30 Hashimoto Forming Co Ltd Method for molding synthetic resin
JPS57167224A (en) * 1981-04-09 1982-10-15 Hashimoto Forming Co Ltd Manufacture of synthetic resin molding with foamed layer
US4536689A (en) * 1984-05-17 1985-08-20 Sperry Corporation Servomotor feedback fault detector
JP2727315B2 (ja) * 1985-10-25 1998-03-11 ファナック 株式会社 射出成形機の保圧制御方法
US4826110A (en) * 1987-06-22 1989-05-02 The Boeing Company Oscillatory failure monitor
US4858491A (en) * 1988-01-21 1989-08-22 Plessey Incorporated Fail-free actuator assembly
US5224664A (en) * 1991-07-22 1993-07-06 United Technologies Corporation Adaptive control system input limiting
US5670856A (en) * 1994-11-07 1997-09-23 Alliedsignal Inc. Fault tolerant controller arrangement for electric motor driven apparatus
JP4323542B2 (ja) * 2007-10-22 2009-09-02 ファナック株式会社 学習制御機能を備えた電動機の制御装置
FR2995873B1 (fr) * 2012-09-27 2014-10-03 Airbus Operations Sas Procede et dispositif d'alerte contre un actionnement inapproprie d'un palonnier d'un aeronef.
US10106245B2 (en) 2015-10-19 2018-10-23 Honeywell International Inc. Automatic flight control actuator systems
US10030756B2 (en) 2016-06-02 2018-07-24 Honeywell International Inc. Automatic flight control actuator systems
CN108469834B (zh) * 2018-03-19 2021-07-13 上海歌尔泰克机器人有限公司 无人机控制方法、装置及计算机可读存储介质

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3143693A (en) * 1960-02-26 1964-08-04 Smiths America Corp Automatic trimming systems for the control surfaces of a moving craft
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
US3593092A (en) * 1970-02-02 1971-07-13 Ltv Electrosystems Inc Multiple output multiplex actuator
US4035705A (en) * 1975-03-17 1977-07-12 Sperry Rand Corporation Fail-safe dual channel automatic pilot with maneuver limiting

Also Published As

Publication number Publication date
DE2826467A1 (de) 1979-01-11
FR2396348A2 (fr) 1979-01-26
US4094481A (en) 1978-06-13
IT7850052A0 (it) 1978-06-27
DE2826467C2 (fr) 1989-01-19
IT1174313B (it) 1987-07-01
GB1600444A (en) 1981-10-14
JPS5415299A (en) 1979-02-05

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Legal Events

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