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A Location Tracking Control for Unmanned Small Scale Helicopter Using Sliding Mode Controller

机译:基于滑模控制器的无人小型直升机位置跟踪控制

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Location tracking control system is developed for an unmanned small scale helicopter using sliding mode controller and cascade controller. The developed control system consists of an inner loop and outer loop. The inner loop control system determines the attitude of the helicopter based on the equation of motion with sliding mode controller. The outer loop control system based on the linear model of the helicopter generates the attitude reference according to the given position, heading references, altitude of the helicopter etc. The linear model for the outer loop control system is obtained by a linearization of the nonlinear helicopter dynamics during hover flight. A numerical simulation is performed on the nonlinear helicopter model to validate the effectiveness of the controller.
机译:使用滑模控制器和叶栅控制器为无人小型直升机开发了位置跟踪控制系统。开发的控制系统由一个内环和一个外环组成。内环控制系统基于带有滑模控制器的运动方程式来确定直升机的姿态。基于直升机线性模型的外环控制系统根据给定的位置,航向参考,直升机的高度等生成姿态参考。通过非线性直升机的线性化获得外环控制系统的线性模型悬停飞行过程中的动力学。在非线性直升机模型上进行了数值模拟,以验证控制器的有效性。

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