Output feedback second order sliding mode control design for a 3-DOF helicopter based on its simplified model

Jovan Merida-Rubio, L. Aguilar
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引用次数: 5

Abstract

This paper presents the solution to the tracking control problem for an underactuated scaled autonomous helicopter using variable structure control via output measurements. First, it is designed a state-feedback second order sliding mode controller to stabilize height and rotation positions. Controller is designed from a reduced model of the helicopter and the resulting control law is tested in its full model thus showing the robustness against unmodelled dynamics. Simulation results illustrate the performance the effectiveness of the controller.
基于简化模型的三自由度直升机输出反馈二阶滑模控制设计
针对欠驱动比例式自主直升机的跟踪控制问题,提出了一种基于输出测量的变结构控制方法。首先,设计了状态反馈二阶滑模控制器,实现高度和旋转位置的稳定。根据直升机的简化模型设计了控制器,并在其完整模型中对控制律进行了测试,从而显示了对未建模动力学的鲁棒性。仿真结果验证了该控制器的性能和有效性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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