FR2370312A1 - Procede de guidage de la phase finale du vol de projectiles balistiques - Google Patents

Procede de guidage de la phase finale du vol de projectiles balistiques

Info

Publication number
FR2370312A1
FR2370312A1 FR7733054A FR7733054A FR2370312A1 FR 2370312 A1 FR2370312 A1 FR 2370312A1 FR 7733054 A FR7733054 A FR 7733054A FR 7733054 A FR7733054 A FR 7733054A FR 2370312 A1 FR2370312 A1 FR 2370312A1
Authority
FR
France
Prior art keywords
projectile
guiding
final phase
flight
ballistic projectile
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.)
Granted
Application number
FR7733054A
Other languages
English (en)
Other versions
FR2370312B1 (fr
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.)
Licentia Patent Verwaltungs GmbH
Original Assignee
Licentia Patent Verwaltungs 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 Licentia Patent Verwaltungs GmbH filed Critical Licentia Patent Verwaltungs GmbH
Publication of FR2370312A1 publication Critical patent/FR2370312A1/fr
Application granted granted Critical
Publication of FR2370312B1 publication Critical patent/FR2370312B1/fr
Granted 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
    • F41G7/303—Sighting or tracking devices especially provided for simultaneous observation of the target and of the missile
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/12—Target-seeking control

Abstract

Procédé de guidage de la phase finale du vol de projectiles balistiques. Un système de pointage I est utilisé pour l'analyse simultanée des coordonnées angulaires de la position de l'objectif et du projectile. Il délivre continûment la valeur instantanée de la position du projectile, qui est comparée en permanence à la valeur de consigne déterminée par un calculateur directeur de tir, avec calcul de dérive. Cette dérive est transmise sans fil au projectile, sous forme d'un signal codé qui est converti, avec les valeurs mesurées des propriétés dynamiques du vol, en une impulsion d'allumage pour le déclenchement d'une correction de trajectoire.
FR7733054A 1976-11-03 1977-11-03 Procede de guidage de la phase finale du vol de projectiles balistiques Granted FR2370312A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19762650380 DE2650380A1 (de) 1976-11-03 1976-11-03 Verfahren zur endphasenlenkung von ballistischen geschossen

Publications (2)

Publication Number Publication Date
FR2370312A1 true FR2370312A1 (fr) 1978-06-02
FR2370312B1 FR2370312B1 (fr) 1983-05-20

Family

ID=5992357

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7733054A Granted FR2370312A1 (fr) 1976-11-03 1977-11-03 Procede de guidage de la phase finale du vol de projectiles balistiques

Country Status (7)

Country Link
US (1) US4220296A (fr)
AT (1) AT352587B (fr)
DE (1) DE2650380A1 (fr)
FR (1) FR2370312A1 (fr)
GB (1) GB1595951A (fr)
IT (1) IT1087845B (fr)
SE (1) SE7712457L (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2932428C2 (de) * 1979-08-10 1985-06-20 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zur Bekämpfung von Bodenzielen durch endphasengelenkte Flugkörper
US4300736A (en) * 1979-08-17 1981-11-17 Raytheon Company Fire control system
USRE33287E (en) * 1980-02-04 1990-08-07 Texas Instruments Incorporated Carrier tracking system
GB2302224B (en) * 1982-07-30 1997-07-02 Secr Defence Gun-launched guided projectile system
US5560567A (en) * 1983-09-06 1996-10-01 Loral Vought Systems Corporation Passive missile tracking and guidance system
GB2158269A (en) * 1984-05-01 1985-11-06 Electronic Automation Ltd Robot vision control system
SE462181B (sv) * 1987-10-22 1990-05-14 Bofors Ab Saett att oeka traeffsannolikheten foer automatkanonluftvaern
US5131602A (en) * 1990-06-13 1992-07-21 Linick James M Apparatus and method for remote guidance of cannon-launched projectiles
US5436832A (en) * 1993-11-05 1995-07-25 The United States Of America As Represented By The Secretary Of The Navy Fuzzy controller for beam rider guidance
US5647558A (en) * 1995-02-14 1997-07-15 Bofors Ab Method and apparatus for radial thrust trajectory correction of a ballistic projectile
SE517023C2 (sv) * 1999-08-18 2002-04-02 Saab Ab Förfarande för styrning av en robot och ett styrsystem för styrning av en robot
US6845938B2 (en) * 2001-09-19 2005-01-25 Lockheed Martin Corporation System and method for periodically adaptive guidance and control
DE102007018190B3 (de) * 2007-04-18 2009-01-22 Lfk-Lenkflugkörpersysteme Gmbh Verfahren Anordnung und Track-System zur Ermittlung und Vorhersage einer Bewegung eines Zielobjektes
US7795565B2 (en) * 2008-01-03 2010-09-14 Lockheed Martin Corporation Guidance system with varying error correction gain
US8471186B2 (en) * 2009-01-09 2013-06-25 Mbda Uk Limited Missile guidance system
EP2207003A1 (fr) * 2009-01-09 2010-07-14 Mbda Uk Limited Système de guidage de missiles
JP5863427B2 (ja) * 2011-12-05 2016-02-16 川崎重工業株式会社 飛しょう体の誘導システム
RU2571530C1 (ru) * 2014-08-12 2015-12-20 Сергей Петрович Мелющенок Способ повышения эффективности стрельбы из вооружения самоходных объектов
RU2604909C9 (ru) * 2015-09-21 2017-04-27 Открытое акционерное общество "Завод им. В.А. Дегтярева" Способ оценки эффективности стрельбы боевого дистанционно-управляемого модуля, размещенного на подвижном объекте
RU2747681C1 (ru) * 2020-06-30 2021-05-12 Юрий Иосифович Полевой Способ управления полетом реактивных снарядов

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1388782A (fr) * 1963-11-28 1965-02-12 Nord Aviation Ensemble lunette de visée-goniomètre i. r. dans un dispositif de téléguidage de missiles
US3567163A (en) * 1964-10-08 1971-03-02 Martin Marietta Corp Guidance system
US3733133A (en) * 1970-03-13 1973-05-15 Hughes Aircraft Co Balanced tiltable, rotating mirror with its optical axis angularly offset from its axis of rotation
FR2109488A5 (fr) * 1970-10-22 1972-05-26 Telecommunications Sa
DE2157672A1 (de) * 1971-11-20 1973-05-24 Messerschmitt Boelkow Blohm Anordnung zur lenkung von flugkoerpern mittels eines lasers
US3807658A (en) * 1972-10-20 1974-04-30 Us Army Rate transmittal method for beamrider missile guidance

Also Published As

Publication number Publication date
SE7712457L (sv) 1978-05-04
FR2370312B1 (fr) 1983-05-20
ATA780777A (de) 1979-02-15
US4220296A (en) 1980-09-02
DE2650380A1 (de) 1978-05-11
IT1087845B (it) 1985-06-04
GB1595951A (en) 1981-08-19
AT352587B (de) 1979-09-25

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Legal Events

Date Code Title Description
ST Notification of lapse