Impedance control is widely used as a main method to achieve active compliance control. However, the determination of impedance parameters mostly relies on empirical adjustments. the multi-subpopulation improved marin...
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An adaptive sliding mode fault-tolerant control (ASMC) based on the backstepping method is proposed for sensor and actuator failures that may occur in the redundant electro-mechanical actuation system on the flight co...
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In order to expand the soft-switching range of three-phase DAB under light load and improve the conversion efficiency, this paper analyzes the working principle and soft-switching characteristics of three-phase DAB, a...
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the propulsion system is the power source of a ship, and the controllable pitch propeller propulsion system is one of the main propulsion devices of modern ships. this paper describes an improved PID controller and it...
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the safety management of a water conservancy construction site faces difficulties. To effectively supervise all workers' operational activity, this study develops a human activity recognition model using a modifie...
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Starting permanent synchronous motor(PMSM) is a difficulty of sensor-loss control. When speed is low, common sensor-less control modes are not applicable. I/F mode is implemented. To deal withthe problem of susceptib...
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Objective: Both simulation and experimental studies show that human walking is a passive biped walking mode adapting to the gravity environment of the earth, and its energy consumption rate is much lower than that of ...
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In recent years, the demands on the performance and safety of turbofan engines for control systems have become increasingly stringent. Prioritizing safety over performance and limiting protection control is essential ...
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To address the issue of suboptimal control of pulse noise generated by the working apparatus inside the excavator cab, this study proposes an improved normalized filtering least mean square algorithm (NEFxatanSLMS). T...
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this paper focuses on the landing process of the 'Tianwen-1' Mars lander and discusses the dynamics models and PID control methods used during its atmospheric entry, parachute deceleration, and powered descent...
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