FIELD: weapons and ammunition.
SUBSTANCE: performed is topographic control of target indicator and launching facility to the terrain by ground satellite receiver, determined are coordinates of launching facility and location and ephemeris for each space vehicle of satellite positioning system, detected and measured are target coordinates, the coordinates are transmitted to artillery position control station, set is universal computer time in reconnaissanceman's console and artillery position control station, calculated and transmitted are shooting settings to launching facility automatic control unit, performed is missile launching procedure, the missile is launched from transporter-launcher container along the preset ballistic course, the missile is oriented by on-board navigation satellite receiver, when the missile approaches the target it is oriented by laser emitter.
EFFECT: providing higher probability of guided missile hitting the target.
Title | Year | Author | Number |
---|---|---|---|
GUIDED MISSILE FIRING METHOD | 2013 |
|
RU2534206C1 |
FIRING METHOD OF CONTROLLED MISSILE WITH LASER SEMI-ACTIVE SEEKER | 2012 |
|
RU2498190C1 |
METHOD TO FIRE GUIDED MISSILE | 2011 |
|
RU2495354C2 |
GUIDED MISSILE FIRING METHOD | 2016 |
|
RU2621361C1 |
FIRING METHOD WITH GUIDED MISSILES WITH LASER SEMI-ACTIVE SELF-GUIDANCE HEAD | 2019 |
|
RU2716462C1 |
METHOD OF FIRE WITH LASER SEMIACTIVE HOMING SHELL ON MOBILE TARGET (VERSIONS) | 2007 |
|
RU2347999C2 |
METHOD FOR FIRE OF GUIDED MISSILE WITH LASER SEMI-ACTIVE HOMING HEAD (MODIFICATIONS) | 2005 |
|
RU2291371C1 |
METHOD OF LAUNCHING MISSILE WITH LASER SEMI-ACTIVE-GUIDANCE HEAD | 2011 |
|
RU2468327C1 |
METHOD FOR FIRE BY GUIDED MISSILE WITH LASER SEMI-ACTIVE HOMING HEAD | 2005 |
|
RU2300726C1 |
METHOD FOR FIRE BY GUIDED PROJECTILES WITH LASER SEMI-ACTIVE HOMING HEAD AT SEVERAL TARGETS | 2006 |
|
RU2317504C1 |
Authors
Dates
2015-01-10—Published
2013-07-03—Filed