Adaptive model-free prescribed performance control for spacecraft proximity operations with safety concerns

IF 8.1 1区 物理与天体物理 Q2 ASTRONOMY & ASTROPHYSICS
Qi Li, Shuo Song, Chong Sun, Zhiqi Niu, Yungang Yang, Sheng Luo
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引用次数: 0

Abstract

In this paper, the issue of robust safety control for spacecraft proximity operations is investigated in the presence of model uncertainties and external disturbances. Initially, a line-of-sight-based relative dynamics model is established to describe the translational motion between the chaser spacecraft and the target spacecraft, based on this, a novel two-stage safety constraint including keep-out zone (Stage I) and field-of-view (FOV) corridor (Stage II) is introduced. Then, an adaptive model-based control scheme is proposed by exploiting the prescribed performance control approach. In addition, a neural networks-based model-free controller that relies only on the input/output measurement data is designed, which is more effective in the unknown and complex proximity process. It is shown that the derived controller can provide an online safety proximity trajectory for the chaser spacecraft while guaranteeing a prescribed convergence performance. Finally, simulations are given to verify the superiorities of the proposed method.

具有安全考虑的航天器近距离操作自适应无模型规定性能控制
本文研究了存在模型不确定性和外部干扰的航天器接近操作的鲁棒安全控制问题。首先,建立了一种基于视距的相对动力学模型来描述追星航天器与目标航天器之间的平移运动,在此基础上,引入了一种新的两级安全约束,即保持区(阶段1)和视场走廊(阶段2)。然后,利用规定的性能控制方法,提出了一种基于自适应模型的控制方案。此外,设计了一种基于神经网络的无模型控制器,该控制器仅依赖于输入/输出测量数据,在未知和复杂的接近过程中更有效。仿真结果表明,该控制器能够在保证收敛性能的前提下,为跟踪飞行器提供在线安全接近轨迹。最后通过仿真验证了该方法的优越性。
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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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