FR2694390B1 - Method for controlling a missile minimizing its passing distance relative to an agile target, and device for implementing it. - Google Patents

Method for controlling a missile minimizing its passing distance relative to an agile target, and device for implementing it.

Info

Publication number
FR2694390B1
FR2694390B1 FR929209291A FR9209291A FR2694390B1 FR 2694390 B1 FR2694390 B1 FR 2694390B1 FR 929209291 A FR929209291 A FR 929209291A FR 9209291 A FR9209291 A FR 9209291A FR 2694390 B1 FR2694390 B1 FR 2694390B1
Authority
FR
France
Prior art keywords
missile
minimizing
implementing
controlling
distance relative
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 - Fee Related
Application number
FR929209291A
Other languages
French (fr)
Other versions
FR2694390A1 (en
Inventor
Manuel Lopez Juan
Jean-Loup Durieux
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.)
Thales SA
Original Assignee
Thomson CSF SA
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 Thomson CSF SA filed Critical Thomson CSF SA
Priority to FR929209291A priority Critical patent/FR2694390B1/en
Publication of FR2694390A1 publication Critical patent/FR2694390A1/en
Application granted granted Critical
Publication of FR2694390B1 publication Critical patent/FR2694390B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
FR929209291A 1992-07-28 1992-07-28 Method for controlling a missile minimizing its passing distance relative to an agile target, and device for implementing it. Expired - Fee Related FR2694390B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR929209291A FR2694390B1 (en) 1992-07-28 1992-07-28 Method for controlling a missile minimizing its passing distance relative to an agile target, and device for implementing it.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR929209291A FR2694390B1 (en) 1992-07-28 1992-07-28 Method for controlling a missile minimizing its passing distance relative to an agile target, and device for implementing it.

Publications (2)

Publication Number Publication Date
FR2694390A1 FR2694390A1 (en) 1994-02-04
FR2694390B1 true FR2694390B1 (en) 1994-09-16

Family

ID=9432334

Family Applications (1)

Application Number Title Priority Date Filing Date
FR929209291A Expired - Fee Related FR2694390B1 (en) 1992-07-28 1992-07-28 Method for controlling a missile minimizing its passing distance relative to an agile target, and device for implementing it.

Country Status (1)

Country Link
FR (1) FR2694390B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5590850A (en) * 1995-06-05 1997-01-07 Hughes Missile Systems Company Blended missile autopilot

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5133520A (en) * 1969-11-13 1992-07-28 British Aerospace Public Limited Company Missile guidance systems
US5123610A (en) * 1989-07-21 1992-06-23 Hughes Aircraft Company Retrofit digital electronics unit for a tube-launched missile

Also Published As

Publication number Publication date
FR2694390A1 (en) 1994-02-04

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Legal Events

Date Code Title Description
CD Change of name or company name
AU Other action affecting the ownership or exploitation of an industrial property right
CL Concession to grant licences
ST Notification of lapse

Effective date: 20120330