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Sensitivity of a physically realizable heliogyro root pitch control system to inherent damping models

机译:物理可实现的旋光根间距控制系统对固有阻尼模型的敏感性

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The heliogyro solar sail employs high aspect ratio blades that are rigidized by spinning about the central spacecraft, eliminating the need for structural booms typically used to tension traditional square sails. The easily scalable heliogyro gains its maneuverability by actuating the blades at their root with sinusoidal pitch profiles. The blade vibration caused by maneuvering must be attenuated using active control since there is little inherent damping in the blade material. Due to the small root pitch control torques required, on the order of 2 μNm, compared to the large friction torques associated with a root pitch actuator, it has only recently been shown that a single blade heliogyro impedance controller can add damping to the lowest frequency torsional modes of the blade in the presence of modeled actuator friction torques. However, the need to measure blade twist away from the actuator at the root creates a non-collocated control system. Some inherent damping at the blade's higher frequency modes is therefore needed to stably add damping to the larger-magnitude low-frequency modes, hence control design is sensitive to the accuracy of the blade damping model. Recently, damping characterization tests performed on a small-scale heliogyro blade in a high-vacuum chamber invalidated the assumption of a linear viscous torsional blade damping model that was previously used in blade control designs. This paper describes the formulation of three modal damping models based on the new experimental data and their integration into the single blade heliogyro model. A comparison of the robustness and performance envelopes for the baseline proximal blade twist feedback controller using these damping models shows the ability to meet the required settling time of less than 720 s necessary for a heliogyro technology demonstration mission. This comparison of physically realizable root pitch control systems for a heliogyro blade is critical to increasing the sailcraft to Technology Readiness Level three.
机译:Heliogyro Solar Sail采用高纵横比刀片,通过旋转围绕中央航天器刚化,消除了通常用于张力传统方帆的结构臂的需要。通过用正弦俯仰型材在根系根部致动刀片,易于可伸缩的光义罗来获得其机动性。由于叶片材料中的固有阻尼几乎没有固有的阻尼,因此必须衰减由操纵引起的叶片振动。由于所需的小桨距控制扭矩,大约2微米的顺序相比,与与根间距执行器相关的大摩擦扭矩相比,它仅显示了单个刀片直升机阻抗控制器可以向最低频率添加阻尼模型执行器摩擦扭矩存在下刀片的扭转模式。然而,需要测量从根部的致动器扭转刀片的需要产生非并发控制系统。因此,需要在刀片的较高频率模式下稳定地增加较大幅度低频模式的一些固有阻尼,因此控制设计对刀片阻尼模型的精度敏感。最近,在高真空室中对小型光叶片进行的阻尼表征测试使预先用于刀片控制设计的线性粘性扭转刀片阻尼模型的假设无效。本文介绍了基于新实验数据的三种模态阻尼模型的配方及其集成到单刀片旋光模型中。使用这些阻尼模型的基线近端叶片扭转反馈控制器的鲁棒性和性能信封的比较显示了符合Heliogyro Technology示范使命所需的所需沉降时间的能力。这种用于旋光叶片的物理可实现的根间距控制系统的这种比较对于增加帆船到技术准备水平三级至关重要。

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