Active nutation control of an asymmetric spacecraft using an axial reaction wheel
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- 作者：Hamed Shahmohamadi Ousaloo hamed.oosaloo@gmail.com" class="auth_mail" title="E-mail the corresponding author
- 关键词：Active nutation control ; Reaction wheel ; Arbitrary spin recovery ; Detumbling ; Asymmetric spacecraft ; Lyapunov control
- 刊名：Advances in Space Research
- 出版年：2016
- 出版时间：1 December 2016
- 年：2016
- 卷：58
- 期：11
- 页码：2287-2303
- 全文大小：5423 K
文摘
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An active nutation control scheme for a spin satellite is proposed.
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This control provides logical recovery of desired spin from any initial state.
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The controller uses a single reaction wheel mounted along the desired spin axis.
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This attitude recovery technique does not require accurate estimates of inertias.
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Simulations confirm that stability is not affected by various inertia ratios.