FIELD: tool-making industry, possible use in onboard automatic control systems.
SUBSTANCE: to achieve the effect, at least for pitching (on horizontal axis) the control rule is predetermined. First order correction coefficients, transfer characteristics and corresponding parameters of the missile and external influences, orientation speed amplification coefficient are all corrected. Also, connections are set up which correlate the missile orientation speed amplification coefficient. In particular, depending on orientation amplification coefficient for one phase of missile flight, orientation amplification coefficient and speed corrections are selected, on basis of which control rule correction parameters are determined.
EFFECT: increased precision of control.
2 cl, 8 dwg
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