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A Novel Nonlinear Backstepping-Based Control Approach for Quadrotor Unmanned Aerial Vehicle Transportation Systems

机译:基于新的基于非线性反向的基于非线性的抗衡失置性控制方法,用于二核空中航空车辆运输系统

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摘要

In this paper, a novel control scheme is proposed for quadrotor unmanned aerial vehicle (UAV) transportation systems. The proposed control law successfully achieves efficient quadrotor transferring and rapid swing elimination simultaneously. Specially, by analyzing the interconnected form of the system, the virtual control input for the outer loop is constructed via an energy-based analysis method, so as to compute the applied thrust and the desired roll angle of the quadrotor. As for the inner loop, a backstepping control method is utilized without the introduction of the time-scale separation principle, and the equilibrium point of the overall close-loop system is proven to be asymptotically stable by Lyapunov techniques and LaSalle's invariance theorem. Simulation results demonstrate the proposed control law's superior performance and good robustness against various uncertainties.
机译:本文提出了一种新型控制方案,用于四轮车无人驾驶车辆(UAV)运输系统。拟议的控制法同时成功实现了高效的四轮运动转移和快速摆动。特别地,通过分析系统的互联形式,通过基于能量的分析方法构造外环的虚拟控制输入,从而计算施加的推力和Quadrotor的所需卷角。至于内圈,利用了一种反向控制方法,而不引入时间级分离原理,并且总体闭环系统的平衡点被Lyapunov技术和Lasalle的不变定理被证明是渐近的稳定性。仿真结果展示了拟议的控制法的卓越性能和对各种不确定性的良好稳健性。

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