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