FIELD: on-board automatic control systems for flying vehicles of aircraft configuration.
SUBSTANCE: proposed system is used in various modes including turns in longitudinal channel at considerable pitch angles and coordinated turns in side channel at considerable bank and heading angles. Provision is made for optimal distribution of intensities (levels) in each channel. Proposed device includes kinematic layout unit, pitch angle and angular velocity sensors in pitching, heading angle and angular velocity sensors in heading, bank angle and angular velocity sensors in bank, pitch angle, heading angle and bank angle setters, three subtraction units, three summing-up amplifiers and three limitation units.
EFFECT: extended functional capabilities; enhanced accuracy of control.
2 cl, 3 dwg
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