Kinematics Control of Electromagnetic Formation Flight Using Angular-Momentum Conservation Constraint-Reference-Cited by-同舟云学术

Kinematics Control of Electromagnetic Formation Flight Using Angular-Momentum Conservation Constraint

Published:2022-02 Issue:2 Volume:45 Page:280-295
ISSN:1533-3884
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Takahashi Yuta¹,Sakamoto Hiraku¹,Sakai Shin-ichiro²

Affiliation:

1. Tokyo Institute of Technology, Meguro-ku, Tokyo 152-8550, Japan

2. Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 252-5210, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.G005873

Reference29 articles.

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3. Ultralight Structures for Space Solar Power Satellites

4. Electromagnetic Formation Flight Testbed Using Superconducting Coils

5. SakaguchiA. “Micro-Electromagnetic Formation Flight of Satellite Systems,” Ph.D. Thesis, Massachusetts Inst. of Technology, Cambridge, MA, 2007, https://dspace.mit.edu/handle/1721.1/39708.

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