Time-Varying Kinematics Control for Magnetically-Actuated Satellite Swarm without Additional Actuator
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arXiv
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| Hauptverfasser: | , , |
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| Format: | Preprint |
| Veröffentlicht: |
2026
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| _version_ | 1866909982710038528 |
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| author | Takahashi, Yuta Sakamoto, Hiraku Sakai, Shin-ichiro |
| author_facet | Takahashi, Yuta Sakamoto, Hiraku Sakai, Shin-ichiro |
| contents | 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. |
| format | Preprint |
| id |
arxiv_https___arxiv_org_abs_2601_03143 |
| institution | arXiv |
| publishDate | 2026 |
| record_format | arxiv |
| spellingShingle | Time-Varying Kinematics Control for Magnetically-Actuated Satellite Swarm without Additional Actuator Takahashi, Yuta Sakamoto, Hiraku Sakai, Shin-ichiro Systems and Control 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. |
| title | Time-Varying Kinematics Control for Magnetically-Actuated Satellite Swarm without Additional Actuator |
| topic | Systems and Control |
| url | https://arxiv.org/abs/2601.03143 |