SE8102157L - SET FOR AVOIDING REVERSION OF BALLIST PROJECTLES - Google Patents

SET FOR AVOIDING REVERSION OF BALLIST PROJECTLES

Info

Publication number
SE8102157L
SE8102157L SE8102157A SE8102157A SE8102157L SE 8102157 L SE8102157 L SE 8102157L SE 8102157 A SE8102157 A SE 8102157A SE 8102157 A SE8102157 A SE 8102157A SE 8102157 L SE8102157 L SE 8102157L
Authority
SE
Sweden
Prior art keywords
firing
missile
trajectory
target
devices
Prior art date
Application number
SE8102157A
Other languages
Unknown language ( )
Swedish (sv)
Inventor
C Mathey
Roon G M Von
Original Assignee
Raketen Systeme Mbh Grs Ges
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 Raketen Systeme Mbh Grs Ges filed Critical Raketen Systeme Mbh Grs Ges
Publication of SE8102157L publication Critical patent/SE8102157L/en

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

Abstract

Changes in the location of targets when firing ballistic missiles from firing devices aligned with respect to a particular target position can be compensated for without the need to realign the firing devices by establishing trajectory correction values which take into account the relation between the firing direction of the firing device and the expected position of the target when a missile fired in the firing direction will reach the position the firing direction was set for the missile to reach. These correction values are introduced before or at firing into an electronic storage means of the missile and after a predetermined time of flight cause the trajectory of the missile to be altered so that it is redirected towards the target's expected position by release of signals from the electronic storage means to trajectory adjusting means of the missile, such as fins, auxiliary rockets or jet-deflecting devices.
SE8102157A 1980-04-05 1981-04-03 SET FOR AVOIDING REVERSION OF BALLIST PROJECTLES SE8102157L (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 (1)

Publication Number Publication Date
SE8102157L true SE8102157L (en) 1981-10-06

Family

ID=6099449

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8102157A SE8102157L (en) 1980-04-05 1981-04-03 SET FOR AVOIDING REVERSION OF BALLIST PROJECTLES

Country Status (6)

Country Link
DE (1) DE3013405C2 (en)
ES (1) ES8202141A1 (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
ES501035A0 (en) 1982-01-01
FR2479970A1 (en) 1981-10-09
DE3013405A1 (en) 1981-10-08
DE3013405C2 (en) 1983-10-20
GB2073382A (en) 1981-10-14
ES8202141A1 (en) 1982-01-01
IT8148198A0 (en) 1981-04-03
IT1170871B (en) 1987-06-03
GB2073382B (en) 1983-11-09

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