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Prototype multicopters demonstrate active aerodynamic control, enhancing stability in flight.
The goal is to develop a multicopter with active control of the aerodynamic surfaces relative to the horizontal flight axis, a high-speed electric drive for the deflecting surfaces, and an angular displacement sensor. A prototype sensor and aircraft models with high-speed deflecting surfaces for the rudder and elevator, located at the point of static instability, were developed.
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Zvonarev et al. (2025) studied this question.
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