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Proposal of a Feedback Control System for a Thermally Driven High-Power-Density Actuator

机译:热驱动大功率密度执行器反馈控制系统的建议

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摘要

Shape memory alloy (SMA) actuators can generate force via the phase transition of the SMA, related to its temperature variations. The amount of force and the response duration length are approximately proportional to the SMA's volume and mass. The higher-power actuator, which consists of a single SMA tube, has mechanical simplicity and high reliability; however, it has a relatively long driving duration, and actuation timing uncertainties caused by the environmental temperature variations. Because of its huge heat capacity, the environment temperature variations affect the actuator's temperature, the phase transformation uncertainties, and force generation profiles, resulting in differences in the actuation timing that are tens of seconds. This paper proposes a suitable feedback control system consisting of two methods. One is the construction of a physical model for SMA tube thermomechanical coupling response that has suitable complexity for the real-time control system design by the limited application condition. The other is a reference trajectory generation and tracking method by using the model predictive control method with a constructed physical model, resulting in a possible drive timing uncertainty reduction. The effectiveness of the proposed methods was verified by specific test piece system identification and control simulations performed both numerically and experimentally. In addition, the effectiveness of the online control system itself was confirmed by comparing the results of a traditional control system using the proportional integral derivative method. The result indicates the potential of the possible application system for SMA actuators.
机译:形状记忆合金(SMA)执行器可以通过SMA的相变产生力,这与温度变化有关。力的大小和响应持续时间的长度大约与SMA的体积和质量成正比。高功率执行器由单个SMA管组成,具有机械简单性和高可靠性。然而,它具有相对较长的驱动持续时间,并且由环境温度变化引起的致动正时不确定性。由于其巨大的热容量,环境温度变化会影响执行器的温度,相变不确定性和力产生曲线,从而导致启动时间的差异为数十秒。本文提出了一种由两种方法组成的合适的反馈控制系统。一种是构建SMA管热机械耦合响应的物理模型,该模型在有限的应用条件下具有适合实时控制系统设计的复杂度。另一种是通过将模型预测控制方法与构建的物理模型一起使用来进行参考轨迹生成和跟踪的方法,从而可能降低驱动时序的不确定性。通过特定的试件系统识别以及数值和实验执行的控制仿真,验证了所提出方法的有效性。此外,通过使用比例积分微分法比较传统控制系统的结果,可以确认在线控制系统本身的有效性。结果表明了SMA执行器可能的应用系统的潜力。

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  • 来源
    《Journal of Spacecraft and Rockets 》 |2020年第1期| 99-108| 共10页
  • 作者单位

    Nagoya Univ Grad Sch Engn Dept Aerosp Engn Chikusa Ku Furo Cho Nagoya Aichi 4648603 Japan;

    Nagoya Univ Grad Sch Engn Dept Aerosp Engn Chikusa Ku Furo Cho Nagoya Aichi 4648603 Japan|AIAA Reston VA USA;

    Japan Aerosp Explorat Agcy Inst Space & Astronaut Sci Dept Spacecraft Engn Chuo Ku Sagamihara Kanagawa 2525210 Japan;

    Chubu Univ Dept Aeronaut & Astronaut 1200 Matsumoto Cho Kasugai Aichi 4878501 Japan|AIAA Reston VA USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
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