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Bibliografická citace

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Chichester, U.K. : Wiley, 2013
1 online resource (xviii, 569 p.) : ill
Externí odkaz    Plný text PDF 
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ISBN 9781118403303 (electronic bk.)
ISBN 9781118342367 (hardback)
Obsahuje bibliografii a rejstřík
Provides the basics of spacecraft orbital dynamics plus attitude dynamics and control, using vectrix notationSpacecraft Dynamics and Control: An Introduction presents the fundamentals of classical control in the context of spacecraft attitude control. This approach is particularly beneficial for the training of students in both of the subjects of classical control as well as its application to spacecraft attitude control. By using a physical system (a spacecraft) that the reader can visualize (rather than arbitrary transfer functions), it is easier to grasp the motivation for why topics in control theory are important, as well as the theory behind them. The entire treatment of both orbital and attitude dynamics makes use of vectrix notation, which is a tool that allows the user to write down any vector equation of motion without consideration of a reference frame. This is particularly suited to the treatment of multiple reference frames..
001893341
full
(Au-PeEL)EBL7103613
(MiAaPQ)EBC7103613
(OCoLC)1347024463

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