FIELD: automatic control systems.
SUBSTANCE: invention relates to automatic control systems, in particular, to guidance systems in two planes of launchers, actuators of mobile robotic systems, artillery and missile weapons, in which bypassing dangerous zones is required. Guidance system comprises a vertical guidance drive, including an adder, a key, an inverter, a reference voltage unit, a vertical guidance actuator, vertical guidance absolute position sensor and vertical guidance relative position sensor, and a horizontal guidance drive including an adder, a key, an inverter, a horizontal guidance actuator, a horizontal guidance absolute position sensor and a horizontal guidance relative position sensor. In addition, into the guidance system containing the vertical and horizontal guidance drives are introduced the first, second and third threshold devices, a comparator, the OR element, the first and second AND elements, first and second NOT elements, RS-trigger, switching unit is introduced into drive of vertical guidance.
EFFECT: improving guidance accuracy due to exclusion of self-oscillations of drives of vertical and horizontal guidance at the boundary of a dangerous zone and reducing time for bypassing this dangerous zone.
1 cl, 2 dwg
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Authors
Dates
2024-05-23—Published
2023-11-03—Filed