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arXiv · 2601.03143

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

Yuta Takahashi·Hiraku Sakamoto·Shin-ichiro Sakai
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Abstract

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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Yuta Takahashi, Hiraku Sakamoto, Shin-ichiro Sakai. 2026-01-06. Time-Varying Kinematics Control for Magnetically-Actuated Satellite Swarm without Additional Actuator. https://arxiv.org/abs/2601.03143

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