Modeling and numerical simulation of linear and nonlinear spacecraft attitude dynamics and gravity gradient moments: A comparative study

► Spacecraft attitude dynamics and gravity gradient moments are modeled in two forms of linear and using Euler angles. ► By using numerical simulation a comparative study is presented such that it is useful for practical application. ► We show that designer should be careful about using the linear o...

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Bibliographic Details
Published in:Communications in nonlinear science & numerical simulation Vol. 17; no. 2; pp. 1065 - 1084
Main Authors: Navabi, M., Nasiri, N., Dehghan, Mehdi
Format: Journal Article
Language:English
Published: Elsevier B.V 01.02.2012
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ISSN:1007-5704, 1878-7274
Online Access:Get full text
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