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Liquid Crystal Device with Reflective Microstructure for Attitude Control

机译:具有反射微结构的用于姿态控制的液晶装置

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摘要

Liquid crystal devices (LCDs) are proposed as fuel-free attitude control devices for spacecraft. The LCDs consist of multiple thin layers, including polymer-dispersed liquid crystal (PDLC) and a base film that has a microstructure with aluminum deposited onto it. When a voltage is applied to an LCD, the crystals in the PDLC align with the electric field, and incident light passes through the PDLC layer and is reflected by the aluminum coating, whereas it is dispersed by randomly arranged crystals when no voltage is applied. This means that arrangements of LCDs can control both the magnitude and direction of reflection electrically, and they can achieve three-degree-of-freedom attitude control using solar radiation pressure. Because light diffracted by the layers causes optical interference, the PDLC has a polarization effect, and the microstructure shape has manufacturing errors, reflection from LCDs is a complex phenomenon and it must be understood to realize the desired performance." The first sentence all means the reason for the second sentence.
机译:提出了液晶装置(LCD)作为航天器的无燃料姿态控制装置。 LCD由多个薄层组成,包括聚合物分散液晶(PDLC)和具有微结构且铝沉积在其上的基膜。当向LCD施加电压时,PDLC中的晶体与电场对齐,入射光穿过PDLC层并被铝涂层反射,而当不施加电压时,入射光会被无序排列的晶体所分散。这意味着LCD的布置可以同时控制反射的幅度和方向,并且可以利用太阳辐射压力实现三自由度的姿态控制。由于各层衍射的光会引起光学干涉,PDLC具有偏振效应,并且微结构形状具有制造误差,因此LCD的反射是一种复杂现象,必须理解以实现所需的性能。”第二句话的原因。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2018年第6期|1509-1518|共10页
  • 作者单位

    Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Chuo Ku, 3-1-1 Yoshinodai, Sagamihara, Kanagawa 2525210, Japan;

    Univ Tokyo, Dept Aeronaut & Astronaut, Bunkyo Ku, 7-3-1 Hongo, Tokyo 1138654, Japan;

  • 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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