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Momentum exchange feedback control: A new approach to the control of flexible spacecraft and space-tethered systems.

机译:动量交换反馈控制:一种控制灵活的航天器和系留系统的新方法。

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This dissertation studies the control methods for the maneuver and vibration control of flexible space structures and the control of space tethered systems. An innovative control concept and technique, so-called momentum exchange feedback control, is introduced to provide a general methodological framework for the control design of the various systems. This new control method is first developed for the two-dimensional maneuver and vibration control of a flexible system. An energy Lyapunov function is used to establish the global stability of the closed-loop system and obtain the stability ranges of the control gains. Both the analytical and numerical results are investigated to show the theoretical and practical merits of the new approach. The implementation of this control technique to the three-dimensional maneuver and vibration control of a flexible spacecraft, the control of an articulated flexible arm, and the retrieval problem of a space tethered system are sequentially investigated. Also, various control techniques such as independent modal control and piezoelectric film actuator control for vibration suppression are discussed. The results of this research demonstrate that the flexible vibrations can be significantly suppressed with the momentum exchange feedback control design for the spacecraft attitude controller. Also, the independent modal control, as well as the piezoelectric film actuator control, can provide further micro-vibration control and fine-tune the system performance. Micro-vibration control at the final stage of a maneuver operation or at a stationkeeping mode is crucial for precision pointing or shape control of advanced spacecraft. As to the control of the tethered antenna/reflector system, the control design based on the concept of the momentum exchange feedback control is shown to be effective for suppression of the tether swing motions during the otherwise unstable retrieval procedure.
机译:本文研究了柔性空间结构的操纵和振动控制方法以及空间系留系统的控制方法。介绍了一种创新的控制概念和技术,即所谓的动量交换反馈控制,旨在为各种系统的控制设计提供通用的方法框架。这种新的控制方法首先是为柔性系统的二维操纵和振动控制而开发的。能量李雅普诺夫函数用于建立闭环系统的整体稳定性,并获得控制增益的稳定性范围。分析和数值结果都进行了研究,以显示该新方法的理论和实践价值。依次研究了该控制技术在挠性航天器的三维操纵和振动控制,铰接挠性臂的控制以及空间系留系统的回收问题上的实现。另外,还讨论了各种控制技术,例如用于抑制振动的独立模态控制和压电薄膜致动器控制。研究结果表明,航天器姿态控制器的动量交换反馈控制设计可以显着抑制柔性振动。同样,独立的模态控制以及压电薄膜致动器控制可以提供进一步的微振动控制,并微调系统性能。机动操作的最后阶段或驻站模式下的微振动控制对于先进航天器的精确指向或形状控制至关重要。关于系留天线/反射器系统的控制,基于动量交换反馈控制概念的控制设计显示出在抑制原本不稳定的检索程序期间可有效抑制系链摆动的控制设计。

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