arXiv 2601.031432026-01-06eess.SYcs.SY

磁性卫星群时变运动学控制无需额外执行器

Time-Varying Kinematics Control for Magnetically-Actuated Satellite Swarm without Additional Actuator

Yuta Takahashi, Hiraku Sakamoto, Shin-ichiro Sakai

备注：: This manuscript is a revised author's preprint based on a paper originally presented at the Workshop on JAXA, "Astrodynamics and Flight Mechanics,'' Sagamihara, Japan, C-6, 2020, and has not been peer-reviewed

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AI总结：

本文提出了一种无需额外执行器的磁性卫星群时变运动学控制方法，基于角动量守恒实现非完整约束下的系统可控性。

摘要：

电磁编队飞行是一种利用电磁力和力矩控制多个卫星而不使用传统燃料推进的技术。本文基于整个系统角动量守恒讨论系统的可控性，这构成了非完整约束。本文为多个卫星设计了一个新的控制器，无需额外的姿态执行器。

英文摘要：

Electromagnetic Formation Flight is a technology that uses electromagnetic forces and torques to control multiple satellites without conventional fuel-based propulsion. In this paper, the controllability of the system is discussed based on the conservation of the entire system's angular momentum, which constitutes a nonholonomic constraint. This paper designs a new controller for multiple satellites without an additional attitude actuator.

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