ES8202141A1 - Method of compensation for target location changes when firing ballistic missiles - Google Patents

Method of compensation for target location changes when firing ballistic missiles

Info

Publication number
ES8202141A1
ES8202141A1 ES501035A ES501035A ES8202141A1 ES 8202141 A1 ES8202141 A1 ES 8202141A1 ES 501035 A ES501035 A ES 501035A ES 501035 A ES501035 A ES 501035A ES 8202141 A1 ES8202141 A1 ES 8202141A1
Authority
ES
Spain
Prior art keywords
firing
missile
trajectory
target
compensation
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
ES501035A
Other languages
Spanish (es)
Other versions
ES501035A0 (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 GES RAKETEN SYSTEME
Original Assignee
GRS GES RAKETEN SYSTEME
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 GES RAKETEN SYSTEME filed Critical GRS GES RAKETEN SYSTEME
Publication of ES501035A0 publication Critical patent/ES501035A0/en
Publication of ES8202141A1 publication Critical patent/ES8202141A1/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/34Direction control systems for self-propelled missiles based on predetermined target position data
    • F41G7/343Direction 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/007Preparatory 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)

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.
ES501035A 1980-04-05 1981-04-03 Method of compensation for target location changes when firing ballistic missiles Expired ES8202141A1 (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
ES501035A0 ES501035A0 (en) 1982-01-01
ES8202141A1 true ES8202141A1 (en) 1982-01-01

Family

ID=6099449

Family Applications (1)

Application Number Title Priority Date Filing Date
ES501035A Expired ES8202141A1 (en) 1980-04-05 1981-04-03 Method of compensation for target location changes when firing ballistic missiles

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
IT1170871B (en) 1987-06-03
DE3013405C2 (en) 1983-10-20
IT8148198A0 (en) 1981-04-03
ES501035A0 (en) 1982-01-01
SE8102157L (en) 1981-10-06
FR2479970A1 (en) 1981-10-09
DE3013405A1 (en) 1981-10-08
GB2073382B (en) 1983-11-09
GB2073382A (en) 1981-10-14

Similar Documents

Publication Publication Date Title
ES8503432A1 (en) Means for reducing spread of shots in a weapon system.
CA2195599A1 (en) Method and device for fire control of a high apogee trajectory weapon
ES8202141A1 (en) Method of compensation for target location changes when firing ballistic missiles
US4198015A (en) Ideal trajectory shaping for anti-armor missiles via time optimal controller autopilot
SE0004531L (en) Rocket weapon system and method of controlling a rocket weapon system
IL123905A0 (en) Method for increasing th probability of impact when combating airborne targets and a weapon designed in accordance with this method
ES480913A1 (en) Spin-stabilized sabot projectile for overcoming a heterogeneous resistance
CH607647A5 (en) Installation for destroying a target by one or more projectiles launched by a weapon
FR2326676A1 (en) Effective range increasing system for projectiles - guides projectile suddenly by sequence of pulses into target area
ES8309002A1 (en) Gun cartridge for flat trajectory or high angle firing.
GB2177213A (en) Determining the ballistic trajectory of a projectile
GB1422404A (en) Infantry protectile
DE3543938C1 (en) Method for preventing premature detonation of a destruction charge, and a detonator arrangement
RU2131573C1 (en) Method of delivery of shell
JPS6446595A (en) Antiaircraft protective car system
FR2422136A1 (en) Anti-tank missile explosive charge treatment - includes heating under reduced pressure for given time using mole firing ring
GB1155185A (en) Improvements in the Aiming of Weapons
Robinson Jr U. S. spurs strategic weapon advances.
RU2122703C1 (en) Method of optimization of anticraft guided missile systems of near and medium lines
ENGEBOS Effects of vertical wind on tactical rockets and artillery shells(Vertical wind effects in trajectory calculations and impact predictions for rockets and projectiles)[Research and Development Technical Report]
GB870608A (en) Improvements in electric devices for igniting the charge of a projectile, said devices being especially intended for use on anti-aircraft or anti-armour projectiles
JPS6036900A (en) Guided missile
JPS6457096A (en) Method of controlling guidance of parent and child type guided missile
SE8400347D0 (en) DEVICE FOR LAUGHTERING ARM
Matogawa Japanese Solid Rockets in World War II.