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This research demonstrates enhanced flight response in unmanned aerial vehicles with adaptive structures, suggesting improved performance in varied conditions.
An unmanned aerial vehicle with a variable structure, as well as the actuators and sensors necessary for creating an optimal configuration and flight parameters, are considered. Membrane-type free-flow sensors, a sensor using a magnetic gap to monitor the load mass, and an optical laser sensor for detecting deformation of load-bearing elements were developed. A design with variable geometry and static instability for increased response time is proposed.
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Zvonarev et al. (2025) studied this question.
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