METHOD FOR FORMING OF GUIDANCE COMMANDS OF GUIDED MISSILES Russian patent published in 2004 - IPC

Abstract RU 2229086 C1

FIELD: guided missile guidance systems. SUBSTANCE: in each control channel forming of the evaluations of linear error, rate of its variation and target acceleration, as well as of control commands is carried out for two evaluations of the "missile-target" range. These commands are formed by integration of the rate of closure in the initial condition decreased by the value of the supported error of determination of range for the first evaluation of range and for the second evaluation of range increased by this value. For control of the missile, the obtained guidance command that is the largest by modulus is selected. EFFECT: facilitated procedure. 9 dwg

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RU 2 229 086 C1

Authors

Akimov V.N.

Atasov V.A.

Dates

2004-05-20—Published

2002-11-27—Filed