| 摘要 |
FIELD: weapons and ammunition.SUBSTANCE: proposed method comprises target ranging and input of measured magnitude to surface control system. Beam axis initial elevation Yis set relative to target point direction to launch the guided missile. Beam axis maximum elevation Yis set relative to target point direction. Missile flies at maximum elevation till the time set at surface control system in compliance with measured range to target, beam axis being aligned with target point direction. Note here that the elevation is serially changed in time interval from rocket launch moment to momentwhere ?is missile control system frequency cut-off, rad/s while initial elevation Yis kept variable. Note here that its magnitude is set by relationshipwhereis minimum possible vertical deviation of the missile from target point direction at this flight path section, m; Ris beam radius, m, while during period from moment tto momentwhere Vis the maximum tolerable beam elevation rate, m/s, elevation is increased to Y.EFFECT: higher accuracy of fire.2 dwg |
