AU568300B2 - Terminally guided weapon delivery system - Google Patents

Terminally guided weapon delivery system

Info

Publication number
AU568300B2
AU568300B2 AU15197/83A AU1519783A AU568300B2 AU 568300 B2 AU568300 B2 AU 568300B2 AU 15197/83 A AU15197/83 A AU 15197/83A AU 1519783 A AU1519783 A AU 1519783A AU 568300 B2 AU568300 B2 AU 568300B2
Authority
AU
Australia
Prior art keywords
weapon
target
projectile
antenna
missile
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.)
Ceased
Application number
AU15197/83A
Other languages
English (en)
Other versions
AU1519783A (en
Inventor
David Dillon Lynch
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.)
Raytheon Co
Original Assignee
Hughes Aircraft Co
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 Hughes Aircraft Co filed Critical Hughes Aircraft Co
Publication of AU1519783A publication Critical patent/AU1519783A/en
Application granted granted Critical
Publication of AU568300B2 publication Critical patent/AU568300B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • 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
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/661—Steering by varying intensity or direction of thrust using several transversally acting rocket motors, each motor containing an individual propellant charge, e.g. solid charge
    • 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
    • F41G7/305—Details for spin-stabilized missiles
AU15197/83A 1982-04-21 1983-04-21 Terminally guided weapon delivery system Ceased AU568300B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US37163682A 1982-04-21 1982-04-21
US371636 1982-04-21

Publications (2)

Publication Number Publication Date
AU1519783A AU1519783A (en) 1983-11-21
AU568300B2 true AU568300B2 (en) 1987-12-24

Family

ID=23464796

Family Applications (1)

Application Number Title Priority Date Filing Date
AU15197/83A Ceased AU568300B2 (en) 1982-04-21 1983-04-21 Terminally guided weapon delivery system

Country Status (5)

Country Link
EP (1) EP0105918B1 (de)
AU (1) AU568300B2 (de)
CA (1) CA1242516A (de)
DE (1) DE3380528D1 (de)
WO (1) WO1983003894A1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU619290B2 (en) * 1988-05-17 1992-01-23 Ab Bofors An apparatus for determining roll position

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4951901A (en) * 1985-11-22 1990-08-28 Ship Systems, Inc. Spin-stabilized projectile with pulse receiver and method of use
DE3608108C1 (de) * 1986-03-12 1990-06-07 Diehl Gmbh & Co Verfahren zur Abwehr von Flugobjekten
FR2660064B1 (fr) * 1990-03-12 1995-05-19 Telefunken Systemtechnik Procede de guidage pour projectiles et dispositifs pour la mise en óoeuvre du procede.
DE4036166A1 (de) * 1990-11-14 1992-05-21 Diehl Gmbh & Co Bahnkorrigierbares projektil
SE468726B (sv) * 1991-07-02 1993-03-08 Bofors Ab Anordning foer rollvinkelbestaemning
IL107707A (en) * 1993-11-22 1997-01-10 Israel State Means for upgrading existing missile control systems
US5647558A (en) * 1995-02-14 1997-07-15 Bofors Ab Method and apparatus for radial thrust trajectory correction of a ballistic projectile
NL1001556C2 (nl) * 1995-11-02 1997-05-13 Hollandse Signaalapparaten Bv Fragmenteerbaar projectiel, wapensysteem en werkwijze.
FR2761767B1 (fr) * 1997-04-03 1999-05-14 Giat Ind Sa Procede de programmation en vol d'un instant de declenchement d'un element de projectile, conduite de tir et fusee mettant en oeuvre un tel procede
US6614012B2 (en) 2001-02-28 2003-09-02 Raytheon Company Precision-guided hypersonic projectile weapon system
US6653972B1 (en) * 2002-05-09 2003-11-25 Raytheon Company All weather precision guidance of distributed projectiles
FR2857088B1 (fr) 2003-07-04 2005-09-16 Mbda France Missile tournant emettant des impulsions lumineuses.
US8324542B2 (en) 2009-03-17 2012-12-04 Bae Systems Information And Electronic Systems Integration Inc. Command method for spinning projectiles

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3374967A (en) * 1949-12-06 1968-03-26 Navy Usa Course-changing gun-launched missile
US4097007A (en) * 1974-10-15 1978-06-27 The United States Of America As Represented By The Secretary Of The Army Missile guidance system utilizing polarization

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3141635A (en) * 1953-02-16 1964-07-21 Marion F Davis Missile guidance system
BE683586A (de) * 1966-07-04 1966-12-16
US3843076A (en) * 1972-01-03 1974-10-22 Trw Projectile trajectory correction system
DE2543606C2 (de) * 1975-09-30 1986-11-06 Deutsch-Französisches Forschungsinstitut Saint-Louis, Saint-Louis Anordnung zur Flugbahnkorrektur eines rotierenden Geschosses
DE2650139C2 (de) * 1976-10-30 1982-04-22 Eltro GmbH, Gesellschaft für Strahlungstechnik, 6900 Heidelberg Verfahren und Vorrichtung zur Korrektur der Flugbahn eines Geschosses
DE2658167C2 (de) * 1976-10-30 1983-01-20 Eltro GmbH, Gesellschaft für Strahlungstechnik, 6900 Heidelberg Verfahren und Vorrichtung zur Korrektur der Flugbahn eines Geschosses
DE3024842A1 (de) * 1980-07-01 1982-01-28 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zur lenkung eines um seine laengsachse rotierenden flugkoerpers

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3374967A (en) * 1949-12-06 1968-03-26 Navy Usa Course-changing gun-launched missile
US4097007A (en) * 1974-10-15 1978-06-27 The United States Of America As Represented By The Secretary Of The Army Missile guidance system utilizing polarization

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU619290B2 (en) * 1988-05-17 1992-01-23 Ab Bofors An apparatus for determining roll position

Also Published As

Publication number Publication date
WO1983003894A1 (en) 1983-11-10
DE3380528D1 (en) 1989-10-12
AU1519783A (en) 1983-11-21
CA1242516A (en) 1988-09-27
EP0105918B1 (de) 1989-09-06
EP0105918A1 (de) 1984-04-25

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