GB1351279A - Target seeking gyro - Google Patents

Target seeking gyro

Info

Publication number
GB1351279A
GB1351279A GB2112358A GB1351279DA GB1351279A GB 1351279 A GB1351279 A GB 1351279A GB 2112358 A GB2112358 A GB 2112358A GB 1351279D A GB1351279D A GB 1351279DA GB 1351279 A GB1351279 A GB 1351279A
Authority
GB
United Kingdom
Prior art keywords
photo
missile
target
axis
gyro
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
GB2112358A
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.)
Bodenseewerk Geratetechnik GmbH
Original Assignee
Bodenseewerk Geratetechnik GmbH
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 Bodenseewerk Geratetechnik GmbH filed Critical Bodenseewerk Geratetechnik GmbH
Publication of GB1351279A publication Critical patent/GB1351279A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F41G7/2213—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
    • F41G7/2273—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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/78—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
    • G01S3/782—Systems for determining direction or deviation from predetermined direction
    • G01S3/785—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system
    • G01S3/786—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system the desired condition being maintained automatically

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Electromagnetism (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

1351279 Automatic control of course FLUGGER€TEWERK BODENSEE GmbH 1 July 1958 21123/58 Heading G3R Steering of an air-to-air missile to collide with a source of light or infrared energy, e.g. jet aircraft tailpipes, is effected photo-electrically. A gyroscope in the missile is precessed automatically by the photo-electric system to maintain the axis of rotation directed towards the target; the inclination of the gyro axis to the missile longitudinal axis is detected and the resultant signal adjusts the missile control fins to turn the missile into alignment with the gyro and hence towards the target. In the gyroscope precession sytem a mirror, mounted on the rotor and inclined at a small angle thereto, reflects light (or heat) rays from the target to a photo-cell. The cell output energizes a coil of which the field interacts with a permanent magnet mounted on the gyroscope to cause it to precess until the axis is directed towards the target. The mirror rotating with the rotor produces an image which traces a circular path round the photo-sensitive device. The inner diameter of the path is such that a small displacement of the image path due to an error between the gyro axis and line of sight causes the image circle to touch the photo-sensitive device to produce the correcting signal.
GB2112358A 1958-07-01 1958-07-01 Target seeking gyro Expired GB1351279A (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
GB2112358 1958-07-01
DEM0045104 1960-04-23
AU26107/63A AU455062B1 (en) 1958-07-01 1963-01-08 Target seeking gyro
CH1660773A CH565988A5 (en) 1958-07-01 1973-11-24

Publications (1)

Publication Number Publication Date
GB1351279A true GB1351279A (en) 1974-04-24

Family

ID=27422814

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2112358A Expired GB1351279A (en) 1958-07-01 1958-07-01 Target seeking gyro

Country Status (4)

Country Link
AU (1) AU455062B1 (en)
CH (1) CH565988A5 (en)
FR (1) FR1605370A (en)
GB (1) GB1351279A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0471919A2 (en) * 1990-07-14 1992-02-26 Daimler-Benz Aerospace Aktiengesellschaft Homokinetic actuator system

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2731785A1 (en) * 1978-09-26 1996-09-20 Bodenseewerk Geraetetech Target seeking head for automatic target tracking
USRE33228E (en) * 1981-11-06 1990-06-05 Ford Aerospace Corporation Optical scanning apparatus incorporating counter-rotation of elements about a common axis by a common driving source
US4427878A (en) * 1981-11-06 1984-01-24 Ford Aerospace & Communications Corporation Optical scanning apparatus incorporating counter-rotation of elements about a common axis by a common driving source
DE4339187C1 (en) † 1993-11-16 1995-04-13 Mafo Systemtech Gmbh & Co Kg Procedure for determining the line of sight rotation rate with a rigid search head

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0471919A2 (en) * 1990-07-14 1992-02-26 Daimler-Benz Aerospace Aktiengesellschaft Homokinetic actuator system
EP0471919A3 (en) * 1990-07-14 1992-04-22 Messerschmitt-Boelkow-Blohm Gmbh Homokinetic actuator system

Also Published As

Publication number Publication date
AU455062B1 (en) 1967-11-07
CH565988A5 (en) 1975-08-29
FR1605370A (en) 1975-02-28

Similar Documents

Publication Publication Date Title
US4093154A (en) Target seeking gyro for a missile
US4085910A (en) Dual mode optical seeker for guided missile control
US2404942A (en) Steering device
US3756538A (en) Guided missile
US3743217A (en) Infrared control system for missile teleguiding
GB831799A (en) Improvements in optical distance detecting devices and to devices controlled thereby
US3982714A (en) Proportional lead guidance
US3752998A (en) Linear scanning seeker with single axis rotation
GB1335539A (en) Balanced tiltable rotating mirror with its optical axis angularly offset from its axis of rotation
US3372890A (en) Data processor for circular scanning tracking system
US2963973A (en) Gyro optical system
US2948813A (en) Tracking system
US3320420A (en) Infrared detection system for use in early stages of missile launching
US2930545A (en) Automatic celestial navigation control system
GB1351279A (en) Target seeking gyro
US3406402A (en) Optical aiming device
GB1073446A (en) Gyro stabilised sight system
GB1164272A (en) Improvements in Guidance Systems for Projectiles or Missiles.
US3718293A (en) Dynamic lead guidance system for homing navigation
US3021096A (en) Infrared guidance system
CN108387151A (en) A kind of biasing measuring guided missile relative attitude angle follows laser measurement system
US4185797A (en) Target seeking gyro
US3494576A (en) Self-contained and automatic guidance system for directing a missile towards a radiation-emitting target
US4191346A (en) Target seeking gyro
US3653737A (en) Optical scanning seeker

Legal Events

Date Code Title Description
PS Patent sealed
PE Patent expired