The characteristic model is derived based on the dynamics model of the spacecraft with flexible appendix.

根据带柔性附件的航天器的动力学模型推导并建立其特征模型。

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This paper is concerned with the dynamics and control for planar, large Angle rapid slew maneuvering of a flexible multi body spacecraft, consisting of a rigid central body and a flexible beam.

研究一类构形为中心刚性带挠性梁的航天器平面快速大角度机动的动力学与控制问题。

youdao

This paper is concerned with the dynamics and control for planar, large Angle rapid slew maneuvering of a flexible multi body spacecraft, consisting of a rigid central body and a flexible beam.

研究一类构形为中心刚性带挠性梁的航天器平面快速大角度机动的动力学与控制问题。

youdao