FIELD: flight vehicle control systems, applicable in missile control systems.
SUBSTANCE: at the moment of missile take-off a single pulse is formed, which inhibits the passage of corrected control signals in each channel, the duration of the formed pulse should be not less than the summary value of the time of absence of the control signals from the moment of missile take-off. The use in the missile control system of the first and second inhibition circuits and series-connected launch device and timer, whose output is connected to the first inputs of the first and second inhibition circuits, with the outputs of the first and second correcting filters being connected to the second inputs respectively of the first and second inhibition circuits, whose outputs are connected to the first and second inputs of the command formation unit has improved the quality of control of the missile.
EFFECT: improved quality of missile control due to delay of the missile control for the time of the transient in the correcting filter.
2 cl, 1 dwg
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