GB1141999A - Installation for guiding missiles - Google Patents

Installation for guiding missiles

Info

Publication number
GB1141999A
GB1141999A GB10452/66A GB1045266A GB1141999A GB 1141999 A GB1141999 A GB 1141999A GB 10452/66 A GB10452/66 A GB 10452/66A GB 1045266 A GB1045266 A GB 1045266A GB 1141999 A GB1141999 A GB 1141999A
Authority
GB
United Kingdom
Prior art keywords
missile
signals
commutator
error signals
changer
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
GB10452/66A
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.)
Nord Aviation Societe Nationale de Constructions Aeronautiques
Original Assignee
Nord Aviation Societe Nationale de Constructions Aeronautiques
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 Nord Aviation Societe Nationale de Constructions Aeronautiques filed Critical Nord Aviation Societe Nationale de Constructions Aeronautiques
Publication of GB1141999A publication Critical patent/GB1141999A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/166Mechanical, construction or arrangement details of inertial navigation systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/20Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/30Command link guidance systems
    • F41G7/301Details
    • F41G7/305Details for spin-stabilized missiles
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • General Physics & Mathematics (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Automation & Control Theory (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Gyroscopes (AREA)
  • Sewing Machines And Sewing (AREA)
  • Navigation (AREA)
GB10452/66A 1965-03-16 1966-03-09 Installation for guiding missiles Expired GB1141999A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9361A FR1458137A (fr) 1965-03-16 1965-03-16 Procédé et dispositif de guidage d'un aérodyne

Publications (1)

Publication Number Publication Date
GB1141999A true GB1141999A (en) 1969-02-05

Family

ID=8574031

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10452/66A Expired GB1141999A (en) 1965-03-16 1966-03-09 Installation for guiding missiles

Country Status (4)

Country Link
US (1) US3360214A (de)
DE (1) DE1456161C3 (de)
FR (1) FR1458137A (de)
GB (1) GB1141999A (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NO130026B (de) * 1969-08-12 1974-06-24 Imp Metal Ind Kynoch Ltd
US3695555A (en) * 1970-06-12 1972-10-03 Us Navy Gun-launched glide vehicle with a mid-course and terminal guidance control system
US4054254A (en) * 1975-12-04 1977-10-18 General Dynamics Corporation Rolling airframe autopilot
FR2459955A1 (fr) * 1979-06-27 1981-01-16 Thomson Csf Nouveau systeme de pilotage de missile et missile pilote
DE3047280C2 (de) * 1980-12-16 1983-01-13 Messerschmitt-Bölkow-Blohm GmbH, 8000 München "Verfahren und Einrichtung zum Erzeugen von aus Lenkkommandos gebildeten Ansteuersignalen für Lenkorgane von rollenden Flugkörpern"
DE3738107C1 (en) * 1987-11-10 1989-06-22 Messerschmitt Boelkow Blohm Device for deflecting a fluid jet with the aid of a jet control surface
US6367735B1 (en) * 2000-02-10 2002-04-09 Quantic Industries, Inc. Projectile diverter
US20030197088A1 (en) * 2001-02-08 2003-10-23 Mark Folsom Projectile diverter
JP4285367B2 (ja) * 2003-10-29 2009-06-24 セイコーエプソン株式会社 視線誘導度算出システムおよび視線誘導度算出プログラム、並びに視線誘導度算出方法
CN103383213B (zh) * 2013-06-11 2015-03-18 魏伯卿 钟表旋针万变曲线飞行自动回位方向控制仪

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2824710A (en) * 1949-01-05 1958-02-25 Albert C Hall Control system for guided missiles
US2852208A (en) * 1950-04-11 1958-09-16 Carleton H Schlesman Method and apparatus for telemetering information from a missile in flight

Also Published As

Publication number Publication date
DE1456161B2 (de) 1973-09-06
US3360214A (en) 1967-12-26
DE1456161A1 (de) 1970-04-30
FR1458137A (fr) 1966-03-04
DE1456161C3 (de) 1974-05-22

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