IEEE Trans Neural Netw Learn Syst. 2012 Jul;23(7):1155-62. doi: 10.1109/TNNLS.2012.2196710.
This brief considers the attitude coordination control problem for spacecraft formation flying when only a subset of the group members has access to the common reference attitude. A quaternion-based distributed attitude coordination control scheme is proposed with consideration of the input saturation and with the aid of the sliding-mode observer, separation principle theorem, Chebyshev neural networks, smooth projection algorithm, and robust control technique. Using graph theory and a Lyapunov-based approach, it is shown that the distributed controller can guarantee the attitude of all spacecraft to converge to a common time-varying reference attitude when the reference attitude is available only to a portion of the group of spacecraft. Numerical simulations are presented to demonstrate the performance of the proposed distributed controller.
本简要考虑了仅一部分群体成员可以访问公共参考姿态时的航天器编队飞行的姿态协调控制问题。提出了一种基于四元数的分布式姿态协调控制方案,考虑了输入饱和,并借助滑模观测器、分离原理定理、Chebyshev 神经网络、平滑投影算法和鲁棒控制技术。利用图论和基于 Lyapunov 的方法,证明了当参考姿态仅可用于部分航天器组时,分布式控制器可以保证所有航天器的姿态收敛到公共时变参考姿态。数值模拟结果验证了所提出的分布式控制器的性能。