【摘要】 考虑刚性主体上带有挠性梁的航天器,在建立挠性系统动力学模型的基础上,基于"喷气-飞轮"执行机构工作模式,设计了简单易行的滑模变结构控制策略进行大角度机动控制.通过最优控制理论设计弹性稳态器,抑制由于刚体运动而激发的弹性振动.实现了旋转机动的同时,有效抑制了弹性振动.更多还原

【Abstract】 This paper is concerned with large angle slew maneuvering of flexible spacecraft, consisting of a rigid central body and a flexible beam. The dynamic model is derived by the assumption mode method. The variable structure control(VSC) method is applied to drive slew maneuvering using jet and fly wheel as actuators. To suppress the simultaneous elastic vibration in movement, an elastic stabilizer is designed by using the LQR control method. Numerical simulation results are presented to show the effectiveness of the proposed control strategy.更多还原