Relative Position and Attitude Coupling Control of Sun-Earth L2 Point Formation Flying by QLTV Polynomial Eigenstructure Assignment-Reference-Cited by-同舟云学术

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Relative Position and Attitude Coupling Control of Sun-Earth L2 Point Formation Flying by QLTV Polynomial Eigenstructure Assignment

Published:2010-06-26 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
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Author:

Wang Feng¹,Tsourdos Antonios¹,Zbikowski Rafal¹,White Brian¹,Ankersen Finn²,Stanley Adrian³

Affiliation:

1. Cranfield University

2. European Space Research and Technology Center

3. EADS Astrium Ltd

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-7716

Reference31 articles.

1. 1http://www.esa.int/esaSC/120382_index_0_m.html(cited20,August,2008).

2. 2http://www.esa.int/esaSC/120369_index_0_m.html(cited20,August,2008).

3. 3http://www.terrestrial-planet-finder.com/(cited20,August,2008).

4. 4http://hires.gsfc.nasa.gov/si/(cited20,August,2008).

5. 5http://maxim.gsfc.nasa.gov/(cited20,August,2008).

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