LPV Polynomial Eigenstructure Assignment for Formation Flying Control Around Sun-Earth L2 Point-Reference-Cited by-同舟云学术

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LPV Polynomial Eigenstructure Assignment for Formation Flying Control Around Sun-Earth L2 Point

Published:2009-06-14 Issue: Volume: Page:
ISSN:
Container-title:AIAA Guidance, Navigation, and Control Conference
language:
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Author:

Ke F¹,Tsourdos Antonios¹,White Brian¹

Affiliation:

1. Cranfield University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6288

Reference19 articles.

1. http://www.esa.int/esaSC/120382_index_0_m.html

2. http://www.esa.int/esaSC/120369_index_0_m.html

3. HamiltonN.H.,FoltaD.andCarpenterR.,Formationflyingsatellitecontrolaroundthel2sun-earthlibrationpoint.AIAA2002-4528

4. Jennifer A. Roberts. Satellite formation flying for an interferometry mission. PhD Thesis,2005, Cranfield University, Swindon.

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