An optimal switching plane design for the third order system subject to state constraints

A. Bartoszewicz, A. Nowacka
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引用次数: 3

Abstract

In this paper the design of a time-varying switching plane for the sliding mode control of the third order system subject to the velocity and acceleration constraints is considered. Initially the plane passes through the system representative point in the error state space and then it moves with a constant velocity to the origin of the space. Having reached the origin the plane stops and remains motionless. The plane parameters (determining angles of inclination and the velocity of its motion) are selected to ensure the minimum integral absolute error without violating velocity and acceleration constraints. The optimal parameters of the plane for the system subject to the acceleration constraint are derived analytically, and it is strictly proved that when both the system velocity and acceleration are limited, the optimal parameters can be easily found using any standard numerical procedure for solving nonlinear equations. The equation to be solved is derived and the starting points for the numerical procedure are given
考虑状态约束的三阶系统的最优开关平面设计
本文考虑了三阶系统在速度和加速度约束下滑模控制的时变切换平面的设计。首先,平面通过误差状态空间中的系统代表点,然后以恒定速度移动到空间的原点。到达原点后,飞机停了下来,一动不动。平面参数(决定倾角和运动速度)的选择,在不违反速度和加速度约束的情况下,保证积分绝对误差最小。解析导出了系统在加速度约束下的平面最优参数,并严格证明了当系统速度和加速度都有限制时,用任何标准数值方法求解非线性方程都可以很容易地找到最优参数。导出了待解方程,并给出了数值计算的起始点
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