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首页> 外文期刊>Transactions of the Canadian Society for Mechanical Engineering >QUASIFASSIVITY-BASED ROBUST NONLINEAR FLAP POSITIONING CONTROL USING SHAPE MEMORY ALLOY MICRO-ACTUATORS
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QUASIFASSIVITY-BASED ROBUST NONLINEAR FLAP POSITIONING CONTROL USING SHAPE MEMORY ALLOY MICRO-ACTUATORS

机译:使用形状记忆合金微执行器的基于拟能度的鲁棒非线性襟翼定位控制

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摘要

This paper proposes a quasipassivity-based robust nonlinear control law ensuring position control of a rotary flap by means of an antagonist-type shape memory alloy microactuator. The control system employs variable-structure control to obtain robust performance, phase-lead compensation to quasipassivate the shape memory alloy dynamics and quasipassivity-based analysis to warrant robust ultimate boundedness of system trajectories. The feedback connection of the two paths leads to ultimate boundedness of tracking error trajectories of the plant despite uncertainties in the dynamic loads affecting the leading edge flap and in the friction found in the actuator. Since accurate numerical simulations and development of new concepts of microactuators based on shape memory alloys require a tractable, constitutive law accurately describing the relationship between force, displacement and temperature in the material, the paper also presents a hybrid micro-macro-mechanical shape memory alloy constitutive model. This model is based on a combination of structural modeling on a microscopic scale and transformation kinetics modeling on a macroscopic scale. The proposed control law and hybrid micro-macro-mechanical model are placed in closed-loop by means of numerical simulations that demonstrate the validity of the nonlinear control scheme.
机译:本文提出了一种基于准钝性的鲁棒非线性控制律,以利用对位型形状记忆合金微致动器来确保旋转襟翼的位置控制。该控制系统采用可变结构控制来获得鲁棒的性能,相位超前补偿来准钝化形状记忆合金动力学,并基于准钝化进行分析,以确保系统轨迹具有鲁棒的最终有界性。尽管影响前缘襟翼的动态负载和执行器中的摩擦存在不确定性,两条路径的反馈连接导致了设备跟踪误差轨迹的最终边界。由于精确的数值模拟和基于形状记忆合金的微致动器新概念的开发需要一种易处理的本构定律,以准确描述材料中力,位移和温度之间的关系,因此本文还提出了一种混合型微宏观机械形状记忆合金本构模型。该模型基于微观尺度上的结构建模和宏观尺度上的转换动力学建模的结合。通过数值模拟证明了非线性控制方案的有效性,将提出的控制律和混合微宏力学模型置于闭环中。

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