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Abstract <p>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.</p>

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Multicopters with Morphological Shape Modification: Adaptation to Various Flight Conditions

  • 期刊论文

  • 发表日期：

    2025年12月1日

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  • D. A. Zvonarev,
  • T. Yu. Zhoraev

摘要

Abstract

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.