GB8627186D0 - Two-axis adjusting mechanism of flying body - Google Patents

Two-axis adjusting mechanism of flying body

Info

Publication number
GB8627186D0
GB8627186D0 GB868627186A GB8627186A GB8627186D0 GB 8627186 D0 GB8627186 D0 GB 8627186D0 GB 868627186 A GB868627186 A GB 868627186A GB 8627186 A GB8627186 A GB 8627186A GB 8627186 D0 GB8627186 D0 GB 8627186D0
Authority
GB
United Kingdom
Prior art keywords
adjusting mechanism
flying body
axis adjusting
flying
axis
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.)
Granted
Application number
GB868627186A
Other versions
GB2183570A (en
GB2183570B (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.)
Diehl Verwaltungs Stiftung
Original Assignee
Diehl GmbH and Co
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 Diehl GmbH and Co filed Critical Diehl GmbH and Co
Publication of GB8627186D0 publication Critical patent/GB8627186D0/en
Publication of GB2183570A publication Critical patent/GB2183570A/en
Application granted granted Critical
Publication of GB2183570B publication Critical patent/GB2183570B/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
GB8627186A 1985-11-28 1986-11-13 A two-axis adjusting mechanism of a flying body Expired GB2183570B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19853542052 DE3542052A1 (en) 1985-11-28 1985-11-28 TWO-AXIS CONTROL DEVICE OF AN AIRCRAFT

Publications (3)

Publication Number Publication Date
GB8627186D0 true GB8627186D0 (en) 1986-12-10
GB2183570A GB2183570A (en) 1987-06-10
GB2183570B GB2183570B (en) 1989-04-26

Family

ID=6287070

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8627186A Expired GB2183570B (en) 1985-11-28 1986-11-13 A two-axis adjusting mechanism of a flying body

Country Status (3)

Country Link
DE (1) DE3542052A1 (en)
FR (1) FR2590662A1 (en)
GB (1) GB2183570B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4239589A1 (en) * 1992-11-25 1994-05-26 Deutsche Aerospace Guidance system for flying missiles - has guiding spoiler and adjuster comprising spring drive with controlled holding and release mechanism
DE19509346C2 (en) * 1995-03-15 1999-08-05 Rheinmetall W & M Gmbh Tail stabilized missile

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2584826A (en) * 1946-05-31 1952-02-05 Gulf Research Development Co Aerodynamic surface for dirigible bombs
FR1039689A (en) * 1951-04-25 1953-10-08 Improvements made to control systems for machines moving in a fluid, in particular those for aerodynes
US3081703A (en) * 1958-07-29 1963-03-19 Ewald A Kamp Spin-cone stabilized projectile
NL123704C (en) * 1960-04-05
US3225693A (en) * 1961-09-05 1965-12-28 Gen Motors Corp Rocket vehicle attitude control
US3200587A (en) * 1961-09-15 1965-08-17 Gen Motors Corp Rocket vehicle attitude control
DE1166010B (en) * 1961-10-25 1964-03-19 Contraves Ag Spoiler for bodies flooded
US4264907A (en) * 1968-04-17 1981-04-28 General Dynamics Corporation, Pomona Division Rolling dual mode missile
US3986683A (en) * 1974-03-27 1976-10-19 The United States Of America As Represented By The Secretary Of The Air Force Jet tab steerable missile
FR2321723A1 (en) * 1975-07-29 1977-03-18 Thomson Brandt ATTITUDE CONTROL SYSTEM AND MACHINE EQUIPPED WITH SUCH A SYSTEM
GB1523963A (en) * 1976-02-26 1978-09-06 Hawker Siddeley Dynamics Ltd Method and means for auxiliary control of vehicle direction
DE3267517D1 (en) * 1981-04-08 1986-01-02 Commw Of Australia Directional control device for airborne or seaborne missiles

Also Published As

Publication number Publication date
GB2183570A (en) 1987-06-10
DE3542052A1 (en) 1987-06-04
GB2183570B (en) 1989-04-26
FR2590662A1 (en) 1987-05-29

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee