METHOD FOR COMMAND TELECONTROL OF MISSILE Russian patent published in 2002 - IPC

FIELD: rocketry, applicable mainly in the optical systems of telecontrol of missiles with an acceleration engine. SUBSTANCE: in the method consisting in missile launching at angle E to the target sight line and missile injection to the target sight line, measurement of missile deviation relative to sight line h, determination of evaluations of missile deviation and deviation derivative forming of the signal of correction for missile deviation relative to the sight line and calculation of missile acceleration U proportional to the corrective signal, corrective signal λ_F is generated according to a definite law. Launch angle E and function f(t) are so selected that an angle of not less than half the angular dimension of the missile smoke plume would be provided between the missile longitudinal axis and the missile sight line. EFFECT: enhanced accuracy and reliability of the control system, as well as reduced dead space of the missile complex. 2 cl, 5 dwg