Control of nonlinear spacecraft attitude motion via state augmentation, Lyapunov-Floquet transformation and normal forms-Reference-Cited by-同舟云学术

Control of nonlinear spacecraft attitude motion via state augmentation, Lyapunov-Floquet transformation and normal forms

Published:2019-08 Issue:3 Volume:64 Page:668-686
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Waswa Peter M.B.,Redkar Sangram

Funder

Interplanetary Initiative of Arizona State University

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference38 articles.

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3. Librations on an Eccentric Orbit: NASA Technical Translation F-8504;Beletskii,1963

4. Beletskii, V.V., 1966. Motion of an Artificial Satellite About its Center of Mass: NASA Technical Translation F-429. Springfield, Va. USA, U.S. Dept. Commerce.

5. Nonlinear resonance affecting gravity-gradient stability;Breakwell,1965

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