Modeling and Analysis of Relative Hovering Control for Spacecraft-Reference-Cited by-同舟云学术

Modeling and Analysis of Relative Hovering Control for Spacecraft

Published:2014-07 Issue:4 Volume:37 Page:1091-1102
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Dang Zhaohui¹,Wang Zhaokui²,Zhang Yulin³

Affiliation:

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

2. School of Aerospace, Tsinghua University, 100084 Beijing, People’s Republic of China

3. College of Aerospace Science and Engineering, and School of Aerospace, National University of Defense Technology, 410073 Changsha, 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.G000004

Reference19 articles.

1. Research on hovering control scheme to non-circular orbit

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