METHOD TO CONTROL CHARACTERISTICS OF EFFECTIVE FIELD OF HIGH-EXPLOSIVE WARHEAD OF MISSILE AND DEVICE FOR ITS REALISATION Russian patent published in 2013 - IPC F42B15/01 

Abstract RU 2484419 C1

FIELD: weapons and ammunition.

SUBSTANCE: substance of invention consists in radiation by two contactless sensors of a target acting in different ranges of electromagnetic spectrum, fixation of the target and identification of the side of its flight at large misses, fixation of the target and identification of the side of its flight at small misses, identification of the target position relative to the axis of the missile on the basis of comparison of polarity of signals from sensors of azimuth and tilt angle of the missile homing head, comparison of the target position defined at one side by the missile homing head and at the other side - by a radar sensor of the target, and if target positions match, identification of the fact of interference absence, definition of the angular speed value and acceleration of target movements on the basis of comparison of angular coordinates of the target with the specified values, detection of dynamics of angular displacement of the target on the basis of analysis of angular speed values and acceleration of target movement, detection of forecasted angular position of the target on the basis of accounting of dynamics of its angular displacement and formation of the effective field of the missile warhead in direction of the target flight with account of its forecasted angular displacement, definition of the conditions of missile approaching to the target, definition of the target class, and on the basis of this information, generation of a time delay for exploding of the missile warhead.

EFFECT: increased efficiency of field use of missiles.

3 cl, 6 dwg

Similar patents RU2484419C1

Title Year Author Number
METHOD TO CONTROL ROCKET HIGH-EXPLOSIVE WARHEAD KILLABILITY FIELD CHARACTERISTICS AND DEVICE TO THIS END 2009
  • Efanov Vasilij Vasil'Evich
  • Muzhichek Sergej Mikhajlovich
RU2398183C1
METHOD TO CONTROL ROCKET HIGH-EXPLOSIVE WARHEAD KILLABILITY FIELD CHARACTERISTICS AND DEVICE TO THIS END 2009
  • Efanov Vasilij Vasil'Evich
  • Muzhichek Sergej Mikhajlovich
RU2398182C1
METHOD OF FUNCTIONING OF INFORMATION COMPUTATION SYSTEM OF MISSILE AND DEVICE THEREFOR 2007
  • Efanov Vasilij Vasil'Evich
  • Muzhichek Sergej Mikhajlovich
  • Gavrilov Nikolaj Vital'Evich
RU2332634C1
METHOD OPERATING MISSILE DATA PROCESSING SYSTEM AND DEVICE TO THIS END 2007
  • Efanov Vasilij Vasil'Evich
  • Muzhichek Sergej Mikhajlovich
  • Gavrilov Nikolaj Vital'Evich
RU2351889C2
METHOD FOR FUNCTIONING OF MISSILE INFORMATION-COMPUTING SYSTEM AT GUIDANCE TO TARGET AND DEVICE FOR ITS REALIZATION 2006
  • Efanov Vasilij Vasil'Evich
  • Muzhichek Sergej Mikhajlovich
RU2311605C2
MODE OF FUNCTIONING OF DATA-PROCESSING SYSTEMS OF ROCKET AND ARRANGEMENT FOR ITS EXECUTION 2004
  • Efanov Vasilij Vasil'Evich
  • Muzhichek Sergej Mikhajlovich
RU2292523C2
AIRCRAFT SIGHTING SYSTEM FOR CLOSE AIR COMBAT 2013
  • Efanov Vasilij Vasil'Evich
  • Vasil'Ev Valerij Aleksandrovich
  • Zhukov Aleksej Sergeevich
  • Savel'Ev Dmitrij Olegovich
RU2544281C1
CONTROL SYSTEM OF ARMY CLOSE AIR DEFENSE MISSILE COMPLEX 1985
  • Efremov V.P.
  • Drize I.M.
  • Rozhnov A.M.
  • Osipov V.V.
  • Chibisov S.I.
  • Vojskovskij E.I.
  • Chirkov V.I.
  • Tolkachev M.A.
  • Grabina I.P.
  • Berkovich G.M.
  • Bajdakov N.N.
RU2102772C1
SIMULATOR 2002
  • Bakhtina T.E.
  • Grigor'Ev R.N.
  • Samojlov D.V.
RU2208214C1
AUTOPILOT FOR ANTI-AIRCRAFT ROLL-STABILIZED GUIDED MISSILE 2005
  • Budilin Vsevolod Aleksandrovich
  • Domarev Valerij Aleksandrovich
  • Pavlova Galina Petrovna
RU2293686C1

RU 2 484 419 C1

Authors

Efanov Vasilij Vasil'Evich

Muzhichek Sergej Mikhajlovich

Gavrilov Nikolaj Vital'Evich

Marukhin Aleksandr Sergeevich

Makhno Igor' Vadimovich

Dates

2013-06-10Published

2011-11-02Filed