This paper is concerned with the dynamics and control for planar, large Angle rapid slew maneuvering of a flexible multi bodyspacecraft, 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。
2
By transformation, the differential equation group of couple motions of solar wings and the central rigidbody of the spacecraft is obtained.
通过变换，给出太阳帆板、航天器中心刚体耦合运动微分方程组。
3
The researches are based on the spacecraft that can be regarded as a central rigid-body with stored angular momentum and some ?exible appendages attached.