用于系留卫星系统稳定回收的基于神经动态的自适应混合控制策略

IF 2.7 1区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS Astrodynamics Pub Date : 2024-02-02 DOI:10.1007/s42064-023-0178-0
Zhixiong Ji, Gefei Shi
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引用次数: 0

摘要

本研究提出了一种基于自适应神经动力学的新型混合控制策略,用于双体系留卫星系统的子卫星稳定回收。通过分析给出了回收速度,确保了无振动稳定状态。为减轻潜在的振动运动,通过自适应神经动力学(AND)算法生成一般控制输入信号,并通过调整子卫星上的回收速度和推进器来执行。为了解决回收速度受限的问题并提高控制性能,推进器控制器是根据一种基于高阶振动状态的新型高级状态模糊控制法则进行控制的,而其余控制输入则分配给速度控制器。该控制策略的 Lyapunov 稳定性得到了分析论证。数值模拟验证了所提出的控制策略,表明两个控制器的控制输入分配合理,控制性能良好。
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Adaptive neural dynamic-based hybrid control strategy for stable retrieval of tethered satellite systems

This study proposes a novel adaptive neural dynamic-based hybrid control strategy for stable subsatellite retrieval of two-body tethered satellite systems. The retrieval speed is given analytically, ensuring a libration-free steady state. To mitigate the potential libration motion, a general control input signal is generated by an adaptive neural-dynamic (AND) algorithm and executed by adjusting the retrieval speed and thruster on the subsatellite. To address the limited retrieval speed and improve the control performance, the thruster controller is manipulated according to a novel advanced state fuzzy control law based on higher-order libration states, whereas the remaining control input is allocated to the speed controller. The Lyapunov stability of the control strategy is demonstrated analytically. Numerical simulations validate the proposed control strategy, demonstrating well-allocated control inputs for both controllers and good control performance.

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来源期刊
Astrodynamics
Astrodynamics Engineering-Aerospace Engineering
CiteScore
6.90
自引率
34.40%
发文量
32
期刊介绍: Astrodynamics is a peer-reviewed international journal that is co-published by Tsinghua University Press and Springer. The high-quality peer-reviewed articles of original research, comprehensive review, mission accomplishments, and technical comments in all fields of astrodynamics will be given priorities for publication. In addition, related research in astronomy and astrophysics that takes advantages of the analytical and computational methods of astrodynamics is also welcome. Astrodynamics would like to invite all of the astrodynamics specialists to submit their research articles to this new journal. Currently, the scope of the journal includes, but is not limited to:Fundamental orbital dynamicsSpacecraft trajectory optimization and space mission designOrbit determination and prediction, autonomous orbital navigationSpacecraft attitude determination, control, and dynamicsGuidance and control of spacecraft and space robotsSpacecraft constellation design and formation flyingModelling, analysis, and optimization of innovative space systemsNovel concepts for space engineering and interdisciplinary applicationsThe effort of the Editorial Board will be ensuring the journal to publish novel researches that advance the field, and will provide authors with a productive, fair, and timely review experience. It is our sincere hope that all researchers in the field of astrodynamics will eagerly access this journal, Astrodynamics, as either authors or readers, making it an illustrious journal that will shape our future space explorations and discoveries.
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