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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降落控制

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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功能,而不是传统的导出/拟合系统的分析模型。然后将映射实现为查找表以形成反馈控制器。致动器对控制也是具有挑战性的:由于存在用于保持永磁体的存在,并且由在不同的操作区域中有效的多个弹簧组成,在动态中产生不连续性。通过在状态空间和前馈控制信号中设计相应的不连续的轨迹来处理不连续动态,从而在弹簧之间切换时避免了不希望的瞬态。提出了模拟结果,示出了控制器在模型扰动和测量噪声存在下的鲁棒性,以及成功穿过没有瞬态的动态不连续性。

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