GB2345952B - Missile guidance - Google Patents

Missile guidance

Info

Publication number
GB2345952B
GB2345952B GB8906778A GB8906778A GB2345952B GB 2345952 B GB2345952 B GB 2345952B GB 8906778 A GB8906778 A GB 8906778A GB 8906778 A GB8906778 A GB 8906778A GB 2345952 B GB2345952 B GB 2345952B
Authority
GB
United Kingdom
Prior art keywords
missile guidance
missile
guidance
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 - Lifetime
Application number
GB8906778A
Other versions
GB8906778D0 (en
GB2345952A (en
Inventor
Enoch James
Raymond John Paul Stafford
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.)
BAE Systems PLC
Matra Bae Dynamics UK Ltd
Original Assignee
British Aerospace PLC
Matra Bae Dynamics UK Ltd
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 British Aerospace PLC, Matra Bae Dynamics UK Ltd filed Critical British Aerospace PLC
Publication of GB8906778D0 publication Critical patent/GB8906778D0/en
Publication of GB2345952A publication Critical patent/GB2345952A/en
Application granted granted Critical
Publication of GB2345952B publication Critical patent/GB2345952B/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F41G7/30—Command link guidance systems
    • F41G7/301—Details
    • F41G7/303—Sighting or tracking devices especially provided for simultaneous observation of the target and of the missile
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/001—Devices or systems for testing or checking
    • 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
    • F41G7/24—Beam riding guidance systems
    • F41G7/26—Optical guidance systems
    • 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
    • G01S3/7864—T.V. type tracking systems
GB8906778A 1988-03-28 1989-03-23 Missile guidance Expired - Lifetime GB2345952B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB8807355.6A GB8807355D0 (en) 1988-03-28 1988-03-28 Missile guidance

Publications (3)

Publication Number Publication Date
GB8906778D0 GB8906778D0 (en) 2000-04-26
GB2345952A GB2345952A (en) 2000-07-26
GB2345952B true GB2345952B (en) 2001-01-17

Family

ID=10634239

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB8807355.6A Ceased GB8807355D0 (en) 1988-03-28 1988-03-28 Missile guidance
GB8906778A Expired - Lifetime GB2345952B (en) 1988-03-28 1989-03-23 Missile guidance

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GBGB8807355.6A Ceased GB8807355D0 (en) 1988-03-28 1988-03-28 Missile guidance

Country Status (1)

Country Link
GB (2) GB8807355D0 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19649735A1 (en) * 1996-11-30 2007-06-06 LFK Lenkflugkörpersysteme GmbH Steering for missile systems with target tracker and additional manual correction of the track point
FR2782811B1 (en) * 1998-09-02 2000-11-10 Aerospatiale METHOD AND DEVICE FOR GUIDING A FLYING MACHINE, ESPECIALLY A MISSILE, ON A TARGET
US7813888B2 (en) 2006-07-24 2010-10-12 The Boeing Company Autonomous vehicle rapid development testbed systems and methods
US7643893B2 (en) 2006-07-24 2010-01-05 The Boeing Company Closed-loop feedback control using motion capture systems
US7885732B2 (en) 2006-10-25 2011-02-08 The Boeing Company Systems and methods for haptics-enabled teleoperation of vehicles and other devices
ES2438976T3 (en) * 2007-05-11 2014-01-21 Saab Ab Device and procedure for a vision apparatus
US8068983B2 (en) 2008-06-11 2011-11-29 The Boeing Company Virtual environment systems and methods
US9012822B2 (en) 2012-07-18 2015-04-21 Thales Holdings Uk Plc Missile guidance
PL2687809T3 (en) * 2012-07-18 2018-05-30 Thales Holdings Uk Plc Missile guidance
IL249787B (en) 2016-12-26 2021-05-31 Israel Aerospace Ind Ltd Method and system of detemining miss-distance
CN112445230B (en) * 2019-08-27 2021-12-24 北京理工大学 High-dynamic aircraft multi-mode guidance system and guidance method under large-span complex environment

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3986682A (en) * 1974-09-17 1976-10-19 The United States Of America As Represented By The Secretary Of The Navy Ibis guidance and control system
US4106726A (en) * 1969-11-04 1978-08-15 Martin Marietta Corporation Prestored area correlation tracker
GB1597981A (en) * 1976-05-21 1981-09-16 Eltro Gmbh Method and apparatus for launching and guiding a misile

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4106726A (en) * 1969-11-04 1978-08-15 Martin Marietta Corporation Prestored area correlation tracker
US3986682A (en) * 1974-09-17 1976-10-19 The United States Of America As Represented By The Secretary Of The Navy Ibis guidance and control system
GB1597981A (en) * 1976-05-21 1981-09-16 Eltro Gmbh Method and apparatus for launching and guiding a misile

Also Published As

Publication number Publication date
GB8906778D0 (en) 2000-04-26
GB8807355D0 (en) 2000-03-15
GB2345952A (en) 2000-07-26

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Legal Events

Date Code Title Description
COOA Change in applicant's name or ownership of the application
PE20 Patent expired after termination of 20 years

Expiry date: 20090322