Spacecraft attitude control via a combined state-dependent Riccati equation and adaptive neuro-fuzzy approach

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Spacecraft attitude control via a combined state-dependent Riccati equation and adaptive neuro-fuzzy approach

A hybrid nonlinear controller for spacecraft attitude and rate tracking is presented though a combination of two control techniques. Based on the augmentation of spacecraft dynamics and kinematics, a pseudo-linear formulation is derived and used for the development of the basic controller. The bas...

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Bibliographic Details
Main Authors:	Abdelrahman, Mohammad, Park, Sang-Young
Format:	Article
Language:	English
Published:	Elsevier Masson SAS 2011
Subjects:	TL787 Astronautics
Online Access:	http://irep.iium.edu.my/8584/ http://irep.iium.edu.my/8584/4/AST_Revised_2_.pdf

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