DEVELOPMENT OF A FORCE CONTROL SOLUTION FOR SINGLE-CHANNEL AERIAL VEHICLES WITH A LINEAR ACTUATOR

Abstract

This paper presents the development of a mathematical foundation for synthesizing control commands and constructing the control force diagram for single-channel flying equipment (SCFV) equipped with linear actuators. A solution is proposed to enhance the control command gain for SCFV using linear actuators, along with a mathematical proof of its validity. The control force utilization coefficient can exceed 0.5 when the input control signal supplied to the actuator is shaped as a sinusoidal function with amplitude limitation. The research results extend existing domestic academic works and provide a foundational basis for the synthesis of autonomous flight control systems.