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GB1533011A - Device for damping pitch and yaw oscillations in a guidance system of a flying vehicle - Google Patents

Device for damping pitch and yaw oscillations in a guidance system of a flying vehicle

Info

Publication number
GB1533011A
GB1533011A GB508/76A GB50876A GB1533011A GB 1533011 A GB1533011 A GB 1533011A GB 508/76 A GB508/76 A GB 508/76A GB 50876 A GB50876 A GB 50876A GB 1533011 A GB1533011 A GB 1533011A
Authority
GB
United Kingdom
Prior art keywords
control
vehicle
flying vehicle
jan
output
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
GB508/76A
Other languages
English (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 GB1533011A publication Critical patent/GB1533011A/en
Expired 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)
GB508/76A 1975-01-14 1976-01-07 Device for damping pitch and yaw oscillations in a guidance system of a flying vehicle Expired GB1533011A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE7500342A SE396473B (sv) 1975-01-14 1975-01-14 Anordning for dempning av tipp- och girsvengar

Publications (1)

Publication Number Publication Date
GB1533011A true GB1533011A (en) 1978-11-22

Family

ID=20323396

Family Applications (1)

Application Number Title Priority Date Filing Date
GB508/76A Expired GB1533011A (en) 1975-01-14 1976-01-07 Device for damping pitch and yaw oscillations in a guidance system of a flying vehicle

Country Status (9)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5224667A (en) * 1991-01-29 1993-07-06 Societe Nationale Industrielle Et Aerospatiale System enabling the flutter behavior of an aircraft to be improved

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3037673C2 (de) * 1980-10-04 1983-12-08 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Antriebseinrichtung für die Steuerung des Ruders eines Flugkörpers mit einem Stellmotor
US5072893A (en) * 1987-05-28 1991-12-17 The Boeing Company Aircraft modal suppression system
WO2003051552A1 (en) * 2001-12-19 2003-06-26 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 (de) * 1964-03-05 1967-04-20 Bodenseewerk Perkin Elmer Co Daempfungseinrichtung fuer Flugregelanlagen von unbemannten Flugkoerpern
JPS4853500A (xx) * 1971-11-08 1973-07-27
DE2165894C2 (de) * 1971-12-31 1983-01-20 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Anordnung zur Steuerung und Stabilisierung eines Flugzeuges

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5224667A (en) * 1991-01-29 1993-07-06 Societe Nationale Industrielle Et Aerospatiale System enabling the flutter behavior of an aircraft to be improved

Also Published As

Publication number Publication date
JPS6164100U (xx) 1986-05-01
IT1052918B (it) 1981-08-31
SE396473B (sv) 1977-09-19
SE7500342L (sv) 1976-07-15
JPS6222480Y2 (xx) 1987-06-08
NL7600074A (nl) 1976-07-16
FR2298132B1 (xx) 1982-04-23
NO145215C (no) 1982-02-10
NO760032L (xx) 1976-07-15
CH601767A5 (xx) 1978-07-14
DE2600532A1 (de) 1976-07-15
NO145215B (no) 1981-10-26
FR2298132A1 (fr) 1976-08-13
DE2600532C2 (de) 1987-03-19
JPS5195400A (xx) 1976-08-20

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee