Nonlinear Attitude Control of Spacecraft with a Large Captured Object-Reference-Cited by-同舟云学术

Nonlinear Attitude Control of Spacecraft with a Large Captured Object

Published:2016-04 Issue:4 Volume:39 Page:754-769
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Bandyopadhyay Saptarshi¹,Chung Soon-Jo¹,Hadaegh Fred Y.²

Affiliation:

1. University of Illinois at Urbana–Champaign, Urbana, Illinois 61801

2. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California 91109

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.G001341

Reference35 articles.

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2. The European Union funded NEOShield project: A global approach to near-Earth object impact threat mitigation

3. BrophyJ.CulickF.FriedmanL. “Asteroid Retrieval Feasibility Study,” Keck Inst. for Space Studies TR, California Inst. of Technology, Pasadena, CA, April 2012.

4. Space debris removal system using a small satellite

5. Inverse optimal adaptive control for attitude tracking of spacecraft

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