FR2298132B1 - - Google Patents

Info

Publication number
FR2298132B1
FR2298132B1 FR7600741A FR7600741A FR2298132B1 FR 2298132 B1 FR2298132 B1 FR 2298132B1 FR 7600741 A FR7600741 A FR 7600741A FR 7600741 A FR7600741 A FR 7600741A FR 2298132 B1 FR2298132 B1 FR 2298132B1
Authority
FR
France
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
FR7600741A
Other languages
French (fr)
Other versions
FR2298132A1 (en
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.)
Saab Bofors AB
Original Assignee
Bofors AB
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 Bofors AB filed Critical Bofors AB
Publication of FR2298132A1 publication Critical patent/FR2298132A1/en
Application granted granted Critical
Publication of FR2298132B1 publication Critical patent/FR2298132B1/fr
Granted legal-status Critical Current

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

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)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Transmitters (AREA)
  • Pens And Brushes (AREA)
FR7600741A 1975-01-14 1976-01-13 FLYING VEHICLE'S TANGING AND LACING OSCILLATION DAMPING DEVICE Granted FR2298132A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE7500342A SE396473B (en) 1975-01-14 1975-01-14 DEVICE FOR DAMPING OF TIP AND GEAR SWITCHES

Publications (2)

Publication Number Publication Date
FR2298132A1 FR2298132A1 (en) 1976-08-13
FR2298132B1 true FR2298132B1 (en) 1982-04-23

Family

ID=20323396

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7600741A Granted FR2298132A1 (en) 1975-01-14 1976-01-13 FLYING VEHICLE'S TANGING AND LACING OSCILLATION DAMPING DEVICE

Country Status (9)

Country Link
JP (2) JPS5195400A (en)
CH (1) CH601767A5 (en)
DE (1) DE2600532C2 (en)
FR (1) FR2298132A1 (en)
GB (1) GB1533011A (en)
IT (1) IT1052918B (en)
NL (1) NL7600074A (en)
NO (1) NO145215C (en)
SE (1) SE396473B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3037673C2 (en) * 1980-10-04 1983-12-08 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Drive device for controlling the rudder of a missile with a servomotor
US5072893A (en) * 1987-05-28 1991-12-17 The Boeing Company Aircraft modal suppression system
FR2672028B1 (en) * 1991-01-29 1993-05-14 Aerospatiale SYSTEM FOR IMPROVING THE FLOATING BEHAVIOR OF AN AIRCRAFT.
AU2002353538A1 (en) * 2001-12-19 2003-06-30 Showa Denko K.K. Extrusion tool, method for manufacturing shaped article with fins, and heat sink

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3331951A (en) * 1963-02-20 1967-07-18 James E Webb Trigonometric vehicle guidance assembly which aligns the three perpendicular axes of two three-axes systems
DE1239200B (en) * 1964-03-05 1967-04-20 Bodenseewerk Perkin Elmer Co Damping device for flight control systems for unmanned aerial vehicles
JPS4853500A (en) * 1971-11-08 1973-07-27
DE2165894C2 (en) * 1971-12-31 1983-01-20 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Arrangement for controlling and stabilizing an aircraft

Also Published As

Publication number Publication date
GB1533011A (en) 1978-11-22
NO145215B (en) 1981-10-26
JPS6164100U (en) 1986-05-01
CH601767A5 (en) 1978-07-14
JPS6222480Y2 (en) 1987-06-08
IT1052918B (en) 1981-08-31
SE396473B (en) 1977-09-19
NL7600074A (en) 1976-07-16
FR2298132A1 (en) 1976-08-13
NO145215C (en) 1982-02-10
SE7500342L (en) 1976-07-15
JPS5195400A (en) 1976-08-20
DE2600532A1 (en) 1976-07-15
NO760032L (en) 1976-07-15
DE2600532C2 (en) 1987-03-19

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Legal Events

Date Code Title Description
ST Notification of lapse