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。
The error between satellite attitude dynamics and its linearized model can affect the attitude control precision.
卫星姿态动力学系统与其线性化模型之间的误差会影响姿态控制的精度。
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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