... 地磁力矩 geomagnetic torque 姿态动力学 attitude dynamics 挠性航天器动力学 flexible spacecraft dynamics ...
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The two algorithms do not use information of relative attitude dynamics between spacecrafts.
两种算法都不需要编队卫星间的姿态动力学联系。
参考来源 - 基于GPS的航天器姿态、相对姿态确定研究·2,447,543篇论文数据，部分数据来源于NoteExpress
本项目研究了可重组航天器的姿态动力学与控制问题。
The present project deals with attitude dynamics and control of reconfigurable spacecrafts.
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。
The model of spacecraft attitude dynamics and the attitude control technology are generalized.
建立卫星姿态动力学数学模型，并分析星体所受的外部扰动力矩。
Mathematic model of satellite attitude dynamic is set up, and external disturbance torque is analyzed.
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