This research presents a method to enhance control command gain in single-channel flying equipment using linear actuators, suggesting improved flight stability.
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.
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Pham Hung Viet (2025) studied this question.
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