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An integral sliding mode controller based disturbances rejection compound scheme for inertially stabilized platform in aerial remote sensing

机译:基于集成滑模控制器的惯性稳定平台航空遥感干扰抑制复合方案

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摘要

An integral sliding mode controller based disturbance rejection compound scheme is proposed to attenuate the influences of nonlinear disturbances and parameter uncertainties on stability accuracy of the three-axis inertially stabilized platform for the aerial remote sensing applications. The compound scheme is composed of an integral sliding mode controller and a disturbance measurement unit. The integral sliding mode controller is used to ensure robust stability against exterior nonlinear disturbances and parameter uncertainties, in which the saturation function is employed to reduce the chattering. The disturbance measurement unit is served as the disturbance measurement components of the rate loop and current loop of three closed-loop structure in the inertially stabilized platform control system, by which the interior high-frequency disturbances are compensated in real time. To verify the method, simulations and experiments are conducted. In simulations, the LuGre friction model is introduced to analyze the effects of disturbances. Further, a series of experiments are carried out. The results show that the compound scheme has excellent ability in both of disturbances rejection and robust stabilization, by which the stability accuracy of the inertially stabilized platform is improved significantly.
机译:提出了一种基于积分滑模控制器的干扰抑制复合方案,以减小非线性干扰和参数不确定性对航空遥感应用三轴惯性稳定平台稳定性精度的影响。复合方案由一个集成的滑模控制器和一个扰动测量单元组成。集成滑模控制器用于确保针对外部非线性干扰和参数不确定性的鲁棒稳定性,其中采用饱和函数来减少抖动。扰动测量单元作为惯性稳定平台控制系统中三个闭环结构的速率回路和电流回路的扰动测量组成部分,可以对内部高频扰动进行实时补偿。为了验证该方法,进行了仿真和实验。在仿真中,引入了LuGre摩擦模型来分析干扰的影响。此外,进行了一系列实验。结果表明,该组合方案具有良好的抗扰性和鲁棒稳定性,能够显着提高惯性稳定平台的稳定性。

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