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Model based landing control for a bistable electromagnetic actuator with discontinuous dynamics

机译:具有不连续动态的双稳态电磁执行器的基于模型的着陆控制

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A design approach is presented to address the soft landing problem for electromagnetic actuators with discontinuous dynamics. The approach uses finite-element-analysis to generate the static functions that make up the dynamic model, as opposed to traditional methods of deriving/fitting an analytical model of the system. The mappings are then implemented as look-up-tables to form a feedback controller. The actuator is also challenging for control: it is bistable due to the presence of a permanent magnet for holding, and consists of multiple springs that are active at different regions of operation, creating discontinuities in the dynamics. The discontinuous dynamics are handled by designing a corresponding discontinuous trajectory in state space and feed-forward control signals, thereby avoiding undesired transients when switching between the springs. Simulation results are presented showing the robustness of the controller in the presence of model perturbations and measurement noise, as well as successfully crossing the dynamic discontinuity without transients.
机译:提出了一种设计方法来解决具有不连续动态特性的电磁执行器的软着陆问题。该方法使用有限元分析来生成构成动态模型的静态函数,这与推导/拟合系统分析模型的传统方法相反。然后将映射实现为查找表以形成反馈控制器。执行器在控制方面也具有挑战性:由于存在用于固定的永久磁铁,因此它是双稳态的,并且由多个弹簧组成,这些弹簧在不同的操作区域起作用,从而导致动力学不连续。通过在状态空间和前馈控制信号中设计相应的不连续轨迹来处理不连续动力学,从而避免了在弹簧之间切换时发生不希望的瞬变。给出的仿真结果显示了在存在模型扰动和测量噪声的情况下控制器的鲁棒性,以及成功跨越动态不连续而没有瞬变的情况。

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