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METHOD AND DEVICE FOR CONTROLLING A GUIDED MISSILE BY MEANS OF A DRIVE WHICH TRACKS ORIENTATION OF TRAJECTORY
METHOD AND DEVICE FOR CONTROLLING A GUIDED MISSILE BY MEANS OF A DRIVE WHICH TRACKS ORIENTATION OF TRAJECTORY
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机译:通过轨迹跟踪的驱动器来控制导弹的方法和装置
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摘要
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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