针对基于微系统阵列的变形翼控制问题,搭建了一种简易分布式的、电机致动的变形翼模型。针对此模型,提出了协同控制的算法,使翼型快速变形,且在变形过程中保持翼面平滑。用李雅普诺夫定理证明了协同控制算法的收敛性。利用了Matlab/Truetime工具箱,进行了无网络、网络无丢包以及有丢包情况下的系统仿真。仿真结果表明:协同控制算法能很成功地对基于微系统阵列的变形翼进行控制。
According to the control problem of morphing wings based on microsystems arrays, a simple, distributed motor actuated morphing wings are modeling. A coordinated control algorithm according to this model is proposed, which can deform the airfoil quickly and keep the wing surface smooth during the deformation. Lyapunov theorem is used to proof the convergence of the coordinated control algorithm. Simulations of the system without network, with and without network packet loss are carried out using Matlab/Truetime toolbox. The results show that the control algorithm is able to control the morphing wings successfully.