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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Veröffentlicht in:	Communications in nonlinear science & numerical simulation Jg. 17; H. 2; S. 1065 - 1084
Hauptverfasser:	Navabi, M., Nasiri, N., Dehghan, Mehdi
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Elsevier B.V 01.02.2012
Schlagworte:	Approximation Dynamic tests Gravitation Gravity gradient moment Linear and nonlinear modeling Mathematical analysis Mathematical models Nonlinear dynamics Nonlinearity Numerical simulation Spacecraft Spacecraft attitude dynamics Numerical simulation Gravity gradient moment Spacecraft attitude dynamics Linear and nonlinear modeling
ISSN:	1007-5704, 1878-7274
Online-Zugang:	Volltext
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