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

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

Reference29 articles.

1. Science enabled by high precision inertial formation flying

2. LawsonP.DooleyJ. “Technology Plan for the Terrestrial Planet Finder Interferometer,” NASA Jet Propulsion Lab. TR 05-5, June 2005, http://hdl.handle.net/2014/37428.

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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