Abstract <p>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.</p>

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Designing Multicopters with Active Attitude Control: A Thrust Vectoring and Angular Sensor Approach

  • V. A. Zvonarev,
  • A. V. Leont’ev

摘要

Abstract

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.