BE689757A - - Google Patents

Info

Publication number
BE689757A
BE689757A BE35914A BE35914A BE689757A BE 689757 A BE689757 A BE 689757A BE 35914 A BE35914 A BE 35914A BE 35914 A BE35914 A BE 35914A BE 689757 A BE689757 A BE 689757A
Authority
BE
Belgium
Application number
BE35914A
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 filed Critical
Publication of BE689757A publication Critical patent/BE689757A/xx

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
    • G05D1/12—Target-seeking control
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2213—Homing guidance systems maintaining the axis of an orientable seeking head pointed at the target, e.g. target seeking gyro
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/222—Homing guidance systems for spin-stabilized missiles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2253—Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/20—Direction control systems for self-propelled missiles based on continuous observation of target position
    • F41G7/22—Homing guidance systems
    • F41G7/2273—Homing guidance systems characterised by the type of waves
    • F41G7/2293—Homing guidance systems characterised by the type of waves using electromagnetic waves other than radio waves
    • 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
    • F42B10/64—Steering by movement of flight surfaces of fins
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01—Arrangements thereon for guidance or control
    • 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
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/107—Simultaneous control of position or course in three dimensions specially adapted for missiles
    • G05D1/108—Simultaneous control of position or course in three dimensions specially adapted for missiles animated with a rolling movement

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Fluid Mechanics (AREA)
  • Electromagnetism (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Control Of Direct Current Motors (AREA)
BE35914A 1964-09-16 1966-11-16 BE689757A (xx)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
US05/397,674 US4037806A (en) 1964-09-16 1964-09-16 Control system for rolling missile with target seeker head
GB5212566A GB1477451A (en) 1964-09-16 1966-11-21 Servosystem
NL6616995A NL6616995A (nl) 1964-09-16 1966-12-02 Korte aanduiding: geheim.
AU14990/66A AU480173B2 (en) 1964-09-16 1966-12-07 Control system, particularly for missiles
DE1578144A DE1578144C2 (de) 1964-09-16 1966-12-16 Steuervorrichtung fur ein rotierendes Lenkgeschoß

Publications (1)

Publication Number Publication Date
BE689757A true BE689757A (xx) 1977-01-21

Family

ID=27506597

Family Applications (1)

Application Number Title Priority Date Filing Date
BE35914A BE689757A (xx) 1964-09-16 1966-11-16

Country Status (6)

Country Link
US (1) US4037806A (xx)
AU (1) AU480173B2 (xx)
BE (1) BE689757A (xx)
DE (1) DE1578144C2 (xx)
GB (1) GB1477451A (xx)
NL (1) NL6616995A (xx)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4234142A (en) * 1978-06-08 1980-11-18 The United States Of America As Represented By The Secretary Of The Navy High angle-of-attack missile control system for aerodynamically controlled missiles
US10488158B1 (en) * 1979-12-26 2019-11-26 Raytheon Company Infrared detection system
US5035376A (en) * 1981-07-31 1991-07-30 General Dynamics Corp., Pomona Division Mz 1-25 Actively damped steering rate sensor for rotating airframe autopilot
US4549707A (en) * 1982-12-27 1985-10-29 General Dynamics Pomona Division Torque optimizing neutral inertia device
DE3501156A1 (de) * 1985-01-16 1986-07-17 Diehl GmbH & Co, 8500 Nürnberg Sensor-fuehrbare stelleinrichtung fuer lenk-flugkoerper
US4779821A (en) * 1985-05-07 1988-10-25 Allied Signal Inc. Small vehicle roll control and steering
DE3645077C2 (de) * 1986-02-27 1996-06-27 Daimler Benz Aerospace Ag Vorrichtung zum Steuern von Flugkörpern
US4777861A (en) * 1987-01-16 1988-10-18 Recon/Optical, Inc. Missile aiming sight
DE4337850A1 (de) * 1993-11-05 1995-05-18 Fritz Hausser Flugkörper die an der vorderen Seite die Seitenruder, Querruder und Höhenruder plaziert haben als einzige oder als Verstärkung der hinteren Ruder
US5669581A (en) * 1994-04-11 1997-09-23 Aerojet-General Corporation Spin-stabilized guided projectile
DE4412687C2 (de) * 1994-04-13 1999-06-24 Diehl Stiftung & Co Mittels eines Laser-Leitstrahles fernsteuerbares Projektil
DE4438010A1 (de) * 1994-10-25 1996-05-02 Diehl Gmbh & Co Um seine Längsachse eine Rollbewegung ausführender Flugkörper
SE511986C2 (sv) * 1995-10-06 2000-01-10 Bofors Ab Sätt att korrigera projektilbanan för rotationsstabiliserande projektiler
US5826821A (en) * 1997-08-04 1998-10-27 The United States Of America As Represented By The Secretary Of The Army Drag control module for range correction of a spin stabil
DE19922693A1 (de) * 1999-05-18 2000-11-23 Diehl Stiftung & Co Stelleinrichtung für Ruder eines Flugkörpers
US6474594B1 (en) * 2001-05-11 2002-11-05 Raytheon Company Output shaft assembly for a missile control actuation unit
WO2007089243A2 (en) * 2005-02-07 2007-08-09 Bae Systems Information And Electronic Systems Integration Inc. Optically guided munition control system and method
WO2006088687A1 (en) * 2005-02-07 2006-08-24 Bae Systems Information And Electronic Systems Integration Inc. Optically guided munition
IL177527A (en) * 2006-08-16 2014-04-30 Rafael Advanced Defense Sys Missile survey targets
FR2925182B1 (fr) * 2007-12-18 2021-07-02 Airbus France Procede et dispositif de detection de pannes oscillatoires dans une chaine d'asservissement en position d'une gouverne d'aeronef.
US8319164B2 (en) * 2009-10-26 2012-11-27 Nostromo, Llc Rolling projectile with extending and retracting canards
CN112179216B (zh) * 2020-09-25 2022-12-02 北京惠风联合防务科技有限公司 调节工装及其使用方法
RU2761915C1 (ru) * 2020-12-29 2021-12-14 Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации Пассивная головка самонаведения
DE102022000529A1 (de) * 2022-02-11 2023-08-17 Diehl Defence Gmbh & Co. Kg Lenkung drallender Geschosse durch zyklischen Stellflächenausschlag
CN116753788B (zh) * 2023-08-09 2023-12-01 北京理工大学 一种基于线性自抗扰的敏捷转弯复合控制方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2714693A (en) * 1953-08-04 1955-08-02 Christiaan J Van Eyk Electric servo control circuit
US3018071A (en) * 1957-08-01 1962-01-23 Lear Inc Trim control system for autopilots
US3072365A (en) * 1957-09-16 1963-01-08 Missile Corp Pilotless craft guidance method and means
US2925966A (en) * 1957-10-08 1960-02-23 Kongelbeck Sverre Folding fin or wing for missiles
US3010677A (en) * 1957-11-12 1961-11-28 Gen Dynamics Corp Missile control system
US3003096A (en) * 1959-02-06 1961-10-03 Gen Precision Inc Pulse width motor control circuit
US3131340A (en) * 1962-02-19 1964-04-28 Collins Radio Co Proportional pulse servo system
US3241016A (en) * 1962-11-09 1966-03-15 Bendix Corp Transistor servo amplifier with dither
FR1415551A (fr) * 1964-06-04 1965-10-29 Telecommunications Sa Système de guidage optique automatique et autonome d'engins en autorotation

Also Published As

Publication number Publication date
AU480173B2 (en) 1977-02-10
US4037806A (en) 1977-07-26
DE1578144B1 (de) 1979-06-21
GB1477451A (en) 1977-06-22
DE1578144C2 (de) 1980-02-21
NL6616995A (nl) 1977-03-31
AU1499066A (en) 1977-02-10

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Legal Events

Date Code Title Description
RE20 Patent expired

Owner name: GENERAL DYNAMICS CORP.

Effective date: 19861116