For citations:
Do Q. Synthesis of a High-Precision Missile Homing System with an Permissible Stability Margin of the Normal Acceleration Stabilization System. Mekhatronika, Avtomatizatsiya, Upravlenie. 2021;22(7):365-373. (In Russ.) https://doi.org/10.17587/mau.22.365-373
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