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Controller design for a 3-DOF helicopter using multiple models with second level adaptation

机译:3-DOF直升机使用具有二级适配的多种型号的三维直升机的控制器设计

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In this article, an adaptive model following control of a nonlinear multi-input multi-output (MIMO) coupled system with unknown parameters is considered. The decoupling matrix of the system is assumed to be singular, so that the system can not be decoupled by static state feedback. A dynamic state feedback with nonlinear structure algorithm is applied to design the controller. An observer is used to estimate the unknown parameters of the system. A multiple model with second level adaptation is introduced for the nonlinear MIMO coupled system. A 3-DOF (degree-of-freedom) helicopter model is simulated to validate the theoretical establishments. The advantage of using second level adaptation is established by conducting simulation studies.
机译:在本文中,考虑了控制具有未知参数的非线性多输入多输出(MIMO)耦合系统之后的自适应模型。 假设系统的去耦矩阵是奇异的,使得系统不能通过静态反馈解耦。 应用具有非线性结构算法的动态状态反馈来设计控制器。 观察者用于估计系统的未知参数。 为非线性MIMO耦合系统引入了具有第二级自适应的多种模型。 模拟了3- DOF(自由度)直升机模型以验证理论场所。 通过进行仿真研究建立使用二级适应的优点。

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