裸电动系索系统平衡位置的分析与控制

IF 3.1 2区 物理与天体物理 Q1 ENGINEERING, AEROSPACE Acta Astronautica Pub Date : 2024-11-13 DOI:10.1016/j.actaastro.2024.11.006
Mingze Xie , Hongshi Lu , Changqing Wang , Aijun Li , Yuriy Zabolotnov
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引用次数: 0

摘要

本文研究了裸电动力系绳(BEDT)在离轨过程中平衡位置的计算和稳定控制的实现。提出了一种利用积分变量代换法计算BEDT系统平衡位置的新方法。该方法提供了平衡位置的解析表达式,从而解决了数值曲线拟合方法的局限性,便于进一步的动态分析和控制器设计。为了解决地磁场强度和电子密度变化对系统姿态的影响,设计了一种基于规定性能的滑模控制器,通过调节系统缆绳长度使系统稳定在平衡位置附近。这种调整同时调节了系绳上的角动量和电流。与传统的电流切换方法相比,该策略有效地减轻了不期望的瞬态响应和额外的系统干扰,并精确地稳定了BEDT系统在平衡位置附近的稳定性。数值模拟结果表明,解析平衡计算与非线性模型吻合较好,误差小于5%。此外,系绳长度调整策略成功地将系统稳定在平衡位置附近,实现了小于0.2度的角偏差,与目前的切换控制方法相比,提高了脱轨效率。
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Analysis and control of the equilibrium position in bare electrodynamic tether systems
This study focuses on the calculation of the equilibrium position of the bare electrodynamic tether (BEDT) and the implementation of stable control during the de-orbiting process. A novel method for calculating the equilibrium position of the BEDT system is proposed, utilizing integral variable substitution. This approach provides an analytical expression for the equilibrium position, thereby addressing the limitations of numerical curve-fitting methods and facilitating further dynamic analysis and controller design. To address the influence of variations in geomagnetic field strength and electron density on the tether attitude during deorbiting, a sliding mode controller based on prescribed performance is designed to stabilize the BEDT around its equilibrium position by adjusting the tether length. This adjustment simultaneously regulates angular momentum and current on the tether. In contrast to conventional current switching methods, the proposed strategy effectively mitigates undesired transient responses and additional system disturbances, and accurately stabilizing the BEDT system around the equilibrium position. Numerical simulations show that the analytical equilibrium calculations closely match the nonlinear model, with an error margin of less than 5%. Additionally, the tether length adjustment strategy successfully stabilizes the system around the equilibrium position, achieving an angular deviation of less than 0.2 degrees and enhanced deorbit efficiency compared to the current switching control method.
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来源期刊
Acta Astronautica
Acta Astronautica 工程技术-工程:宇航
CiteScore
7.20
自引率
22.90%
发文量
599
审稿时长
53 days
期刊介绍: Acta Astronautica is sponsored by the International Academy of Astronautics. Content is based on original contributions in all fields of basic, engineering, life and social space sciences and of space technology related to: The peaceful scientific exploration of space, Its exploitation for human welfare and progress, Conception, design, development and operation of space-borne and Earth-based systems, In addition to regular issues, the journal publishes selected proceedings of the annual International Astronautical Congress (IAC), transactions of the IAA and special issues on topics of current interest, such as microgravity, space station technology, geostationary orbits, and space economics. Other subject areas include satellite technology, space transportation and communications, space energy, power and propulsion, astrodynamics, extraterrestrial intelligence and Earth observations.
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