Angular-Momentum Management of Spacecraft Electromagnetic Docking Considering the Earth’s Magnetic Field-Reference-Cited by-同舟云学术

Angular-Momentum Management of Spacecraft Electromagnetic Docking Considering the Earth’s Magnetic Field

Published:2013-05 Issue:3 Volume:36 Page:860-869
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Zhang Yuan-wen¹,Yang Le-ping¹,Zhu Yan-wei¹,Huang Huan¹,Cai Wei-wei¹

Affiliation:

1. College of Aerospace Science and Engineering, National University of Defense Technology, 410073 Hunan, People’s Republic of China

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

http://arc.aiaa.org/doi/pdf/10.2514/1.57723

Reference19 articles.

1. Pose Estimation for In-Orbit Self-Assembly of Intelligent Self-Powered Modules

2. BloomJ. “On Orbit Autonomous Servicing Satellite (OASIS) Systems Requirements Document,” Dept. of Aeronautics and Astronautics, Univ. of Washington, Seattle, WA, 2000, pp. 1–101.

3. BloomJ.SandhuJ.PaulseneM. “On Orbit Autonomous Servicing Satellite (OASIS) Project Preliminary Design Review,” Dept. of Aeronautics and Astronautics, Univ. of Washington, Seattle, WA, 2000, pp. 1–224.

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