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
Title | Year | Author | Number |
---|---|---|---|
METHOD TO CONTROL ROCKET HIGH-EXPLOSIVE WARHEAD KILLABILITY FIELD CHARACTERISTICS AND DEVICE TO THIS END | 2009 |
|
RU2398183C1 |
METHOD TO CONTROL ROCKET HIGH-EXPLOSIVE WARHEAD KILLABILITY FIELD CHARACTERISTICS AND DEVICE TO THIS END | 2009 |
|
RU2398182C1 |
METHOD OF FUNCTIONING OF INFORMATION COMPUTATION SYSTEM OF MISSILE AND DEVICE THEREFOR | 2007 |
|
RU2332634C1 |
METHOD OPERATING MISSILE DATA PROCESSING SYSTEM AND DEVICE TO THIS END | 2007 |
|
RU2351889C2 |
METHOD FOR FUNCTIONING OF MISSILE INFORMATION-COMPUTING SYSTEM AT GUIDANCE TO TARGET AND DEVICE FOR ITS REALIZATION | 2006 |
|
RU2311605C2 |
MODE OF FUNCTIONING OF DATA-PROCESSING SYSTEMS OF ROCKET AND ARRANGEMENT FOR ITS EXECUTION | 2004 |
|
RU2292523C2 |
AIRCRAFT SIGHTING SYSTEM FOR CLOSE AIR COMBAT | 2013 |
|
RU2544281C1 |
CONTROL SYSTEM OF ARMY CLOSE AIR DEFENSE MISSILE COMPLEX | 1985 |
|
RU2102772C1 |
SIMULATOR | 2002 |
|
RU2208214C1 |
AUTOPILOT FOR ANTI-AIRCRAFT ROLL-STABILIZED GUIDED MISSILE | 2005 |
|
RU2293686C1 |
Authors
Dates
2013-06-10—Published
2011-11-02—Filed