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Experimentally Validated Sliding Mode Control of Multi-rotor UAV with Control Signal Constraints

机译:用控制信号约束的多转子UAV进行实验验证的滑动模式控制

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摘要

This paper proposes a cascade control strategy for multi-rotor unmanned aerial vehicle, where the inner-loop system is regulated by a sliding mode controller with disturbance observer and the outer-loop controller is a PID controller. Operational constraints are incorporated in the implementation for safety protection of the electronics. Experimental results are obtained to demonstrate the efficacy of the proposed design in comparison to a traditional cascade PID control system.
机译:本文提出了一种用于多转子无人空中车辆的级联控制策略,其中内环系统由具有干扰观察者的滑动模式控制器调节,外环控制器是PID控制器。操作系统在实施方面纳入了电子设备的安全保护。获得实验结果以证明所提出的设计与传统的级联PID控制系统相比的功效。

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