METHOD OF GUIDANCE OF TELECONTROLLED MISSILE AND GUIDANCE SYSTEM FOR ITS REALIZATION Russian patent published in 1998 - IPC

FIELD: rocketry, applicable in guidance systems of telecontrolled missiles. SUBSTANCE: at missile guidance the time remaining to the missile impact with the target is determined, and additional correcting command is produced according to the value proportional to the available missile load factor and duration equal to the predicted time of missile coincidence with the target in the point of impact under the action of this correction command, the time remaining to the missile impact with the target and duration of the correction command are compared, and at the instant of their equality the correction command is memorized, then missile guidance is accomplished with due account made for the correction command. Due to employment of the guidance system, in the point of missile impact with the target missile guidance error compensation is assured irrespective of thew time of its origination and during the minimum probable time with the use of all available maneuvering capabilities of the missile. EFFECT: facilitated procedure. 2 cl, 5 dwg