GB2073382B - Method of compensating for target location changes when firing ballistic missiles - Google Patents

Method of compensating for target location changes when firing ballistic missiles

Info

Publication number
GB2073382B
GB2073382B GB8110562A GB8110562A GB2073382B GB 2073382 B GB2073382 B GB 2073382B GB 8110562 A GB8110562 A GB 8110562A GB 8110562 A GB8110562 A GB 8110562A GB 2073382 B GB2073382 B GB 2073382B
Authority
GB
United Kingdom
Prior art keywords
compensating
target location
location changes
ballistic missiles
firing
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
GB8110562A
Other versions
GB2073382A (en
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.)
GRS RAKETEN SYSTEME GmbH
Original Assignee
GRS RAKETEN SYSTEME 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 GRS RAKETEN SYSTEME GmbH filed Critical GRS RAKETEN SYSTEME GmbH
Publication of GB2073382A publication Critical patent/GB2073382A/en
Application granted granted Critical
Publication of GB2073382B publication Critical patent/GB2073382B/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
    • F41G7/34—Direction control systems for self-propelled missiles based on predetermined target position data
    • F41G7/343—Direction control systems for self-propelled missiles based on predetermined target position data comparing observed and stored data of target position or of distinctive marks along the path towards the target
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G7/00—Direction control systems for self-propelled missiles
    • F41G7/007—Preparatory measures taken before the launching of the guided missiles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
GB8110562A 1980-04-05 1981-04-03 Method of compensating for target location changes when firing ballistic missiles Expired GB2073382B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3013405A DE3013405C2 (en) 1980-04-05 1980-04-05 Method of avoiding messaging from ballistic missile launchers

Publications (2)

Publication Number Publication Date
GB2073382A GB2073382A (en) 1981-10-14
GB2073382B true GB2073382B (en) 1983-11-09

Family

ID=6099449

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8110562A Expired GB2073382B (en) 1980-04-05 1981-04-03 Method of compensating for target location changes when firing ballistic missiles

Country Status (6)

Country Link
DE (1) DE3013405C2 (en)
ES (1) ES501035A0 (en)
FR (1) FR2479970A1 (en)
GB (1) GB2073382B (en)
IT (1) IT1170871B (en)
SE (1) SE8102157L (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2492966B1 (en) * 1980-10-29 1986-01-31 Serat IMPROVEMENTS IN PROJECTILES WITH CORRECTED PATH
DE3303763A1 (en) * 1983-02-04 1984-08-09 Diehl GmbH & Co, 8500 Nürnberg METHOD FOR TARGETING A PROJECTILE AND DETERMINING ITS BALLISTIC FLIGHT TRACK AND DEVICES FOR EXECUTING THE METHOD
DE3348136C2 (en) * 1983-02-04 1989-02-02 Diehl Gmbh & Co, 8500 Nuernberg, De Method for determining the ballistic trajectory (flight path) of a projectile, and a device for carrying out the method
DE3340625A1 (en) * 1983-11-10 1985-05-30 Bundesrepublik Deutschland, vertreten durch den Bundesminister der Verteidigung, dieser vertreten durch den Präsidenten des Bundesamtes für Wehrtechnik und Beschaffung, 5400 Koblenz Guided missile system
DE4321392A1 (en) * 1993-06-26 1995-01-05 Bayern Chemie Gmbh Flugchemie Method for trajectory (flight path) correction of a missile
DE4325218C2 (en) * 1993-07-28 1998-10-22 Diehl Stiftung & Co Artillery missile and method for increasing the performance of an artillery missile
DE19740888C2 (en) * 1997-09-17 1999-09-02 Rheinmetall W & M Gmbh Method for autonomously steering a spin-stabilized artillery projectile and autonomously guided artillery projectile for carrying out the method
DE19827168B4 (en) * 1998-06-18 2019-01-17 Dynamit Nobel Defence Gmbh Steering method for missiles
DE19906970C2 (en) 1999-02-19 2003-03-27 Rheinmetall W & M Gmbh reconnaissance probe
DE102008017975A1 (en) * 2008-04-10 2009-10-15 Lfk-Lenkflugkörpersysteme Gmbh Unmanned missile and method of flight guidance

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2056858A5 (en) * 1969-08-16 1971-05-14 Entwicklungsburo Poseido
GB1326791A (en) * 1970-08-17 1973-08-15 Entwicklungsbuero Poseidon Kie Device for shooting low targets from a submerged submarine

Also Published As

Publication number Publication date
GB2073382A (en) 1981-10-14
IT1170871B (en) 1987-06-03
DE3013405A1 (en) 1981-10-08
IT8148198A0 (en) 1981-04-03
DE3013405C2 (en) 1983-10-20
ES8202141A1 (en) 1982-01-01
SE8102157L (en) 1981-10-06
ES501035A0 (en) 1982-01-01
FR2479970A1 (en) 1981-10-09

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee