The model of spacecraft attitude dynamics and the attitude control technology are generalized.

对航天器姿态动力学模型和姿态控制技术进行了概括和总结。

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A mathematical model derived from spacecraft attitude dynamics is treated as an example to demonstrate its application.

以一个呈现混沌姿态运动的航天器动力学模型为例说明了该控制律的应用。

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