METHOD shooting small targets revolve around the longitudinal axis homing on final flight on a ballistic trajectory correctable artillery shells

摘要

1. A method for firing small targets rotating about the longitudinal axis with a frequency ωx homing on the target portion of the flight on a ballistic trajectory correctable artillery projectile (CAS), comprising a body bezgiroskopny rigidly connected with the housing indicator coordinator target determining the position of the target relative speed vector CAS , a logic device with the timer of the flight time, the power supply system and the correction pulse jet engines (IIR), thrust vectors are perpendicular to the axis of the body K AU, characterized in that the CAS gives technical dispersion at conventional artillery shells and its guidance is performed with respect to inclusion of the system permits the logical device within no more than 3 seconds by multiple pulsed rocket correction, the maximum frequency ν missile correction pulse should satisfy the relation where τ - duration of exposure to the missile correction pulse as determined by the logic device as in this case the limit value chosen slip H, corresponding to the product N-unidirectional sum of increments of velocity CAS missile correction pulse, time T and guidance experienced average efficiency homing K≈0,7, i.e. Must be equal to or greater than twice the technical dispersion projectile (Bq range of deviation and on a side Wb) at maximum range, which is defined as RCIC-technology (Russian pulse correction concept). ! 2. A method according to claim 1, characterized in that the thrust vector of each point of application of the DCO is displaced from the center of mass in the direction