论文部分内容阅读
搭建了一个基于相互作用的智能体阵列的变形翼模型。针对该模型,提出了一种分布式协同控制方案,以驱动翼面准确平滑地变形至期望翼型。分析变形翼系统在采样通信约束下的稳定性,给出了基于Lyapunov-Krasovskii稳定性理论的稳定性判据。利用锥补线性化方法,提出了控制器设计的算法。最后使用Matlab进行变形翼的仿真,结果证明了提出方法的可行性。
A deformable wing model of an agent-based agent array is constructed. Aiming at this model, a distributed cooperative control scheme is proposed to drive the airfoil to accurately and smoothly deform to the desired airfoil. The stability of the deformation wing system under the sampling and communication constraints is analyzed, and the stability criterion based on the Lyapunov-Krasovskii stability theory is given. The algorithm of controller design is proposed by using the method of cone-compensating linearization. Finally, the deformation wing simulation using Matlab, the results prove the feasibility of the proposed method.