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Optimal attitude control for rigid spacecraft using successive approximation approach - MaRDI portal

Optimal attitude control for rigid spacecraft using successive approximation approach (Q2844345)

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scientific article; zbMATH DE number 6202486
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English
Optimal attitude control for rigid spacecraft using successive approximation approach
scientific article; zbMATH DE number 6202486

    Statements

    28 August 2013
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    optimal control
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    successive approximation approach
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    spacecraft control system
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    sliding mode control
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    Optimal attitude control for rigid spacecraft using successive approximation approach (English)
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    Identifiers

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