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Control of Three-axis Stabilized Flexible Spacecraft Using Variable Structure Strategies Subject to Input Nonlinearities - MaRDI portal

Control of Three-axis Stabilized Flexible Spacecraft Using Variable Structure Strategies Subject to Input Nonlinearities (Q5188395)

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scientific article; zbMATH DE number 5679919
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Control of Three-axis Stabilized Flexible Spacecraft Using Variable Structure Strategies Subject to Input Nonlinearities
scientific article; zbMATH DE number 5679919

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    Control of Three-axis Stabilized Flexible Spacecraft Using Variable Structure Strategies Subject to Input Nonlinearities (English)
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    10 March 2010
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    flexible spacecraft
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    variable structure output feedback control
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    vibration suppression
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    input nonlinearities
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