Analysis and Control of Space Systems Dynamics via Floquet Theory, Normal Forms and Center Manifold Reduction

Analysis and Control of Space Systems Dynamics via Floquet Theory, Normal Forms and Center Manifold Reduction

abstract: It remains unquestionable that space-based technology is an indispensable component of modern daily lives. Success or failure of space missions is largely contingent upon the complex system analysis and design methodologies exerted in converting the initial idea into an elaborate function...

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Bibliographic Details
Other Authors: WASWA, PETER (Author)
Format: Doctoral Thesis
Language:English
Published: 2019
Subjects:
Aerospace engineering
Mechanics
Systems science
Center Manifold Reduction
Lyapunov-Floquet
Nonlinear Dynamics
Normal Forms
Spacecraft Dynamics
Toutatis
Online Access:http://hdl.handle.net/2286/R.I.55623

Internet

http://hdl.handle.net/2286/R.I.55623

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