FIELD: systems of rockets guidance.
SUBSTANCE: control of rotating rocket with account of its longitudinal speed change, which is determined by the change in rotation period by list. Method includes formation of modulated radiation, formation of signal of mismatch between the rocket and the beam axis, summation of mismatch signal and signal, which is proportional to difference of mismatch signal and shifted by delay time mismatch signal, modulation of summary signal with signal periodical by angle of list and transformation of received signal into decline of rocket rudder. Summary signal is additionally modulated with alternating amplitude signal, which changes in accordance with measured period of rocket rotation by angle of list.
EFFECT: increases precision of shooting with rockets rotating along the list angle in different climate conditions.
1 dwg
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