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Spacecraft synchronization in the presence of attitude constrained zones

机译:存在姿态约束区域的航天器同步

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In this paper, we consider the problem of achieving identical orientation for a group of spacecraft in presence of attitude forbidden zones. The attitude forbidden zones can be identically defined over the group of spacecraft or can be defined independently. In order to find a feasible consensuslike algorithm, we utilize the quadratic convex parameterization for the attitude forbidden zones with unit quaternions. Subsequently, we embed this parameterization into a convex auxiliary system-whose output is shared among the spacecraft through a communication network. The auxiliary system's output play the role of an indicator function for the spacecraft dynamics such that it does not violate the attitude forbidden zones while attempting to reach consensus. In order to evaluate the effectiveness of the algorithm, we present two sets of simulations where synchronization of six spacecraft with identical and independent attitude forbidden zones with random initial attitudes are considered.
机译:在本文中,我们考虑在存在姿态禁止区域的情况下使一组航天器获得相同方向的问题。禁止姿态区可以在航天器组上相同定义,也可以独立定义。为了找到一种可行的类似共识的算法,我们将二次凸参数化用于单位四元数的姿态禁区。随后,我们将此参数化嵌入凸辅助系统中,该辅助系统的输出通过通信网络在航天器之间共享。辅助系统的输出起到航天器动力学指示功能的作用,以便在尝试达成共识时不会违反姿态禁区。为了评估该算法的有效性,我们提出了两组模拟,其中考虑了具有相同初始姿态和随机姿态的六个航天器与初始姿态随机的同步。

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  • 来源
    《American Control Conference;ACC 》|2012年|p.6071- 6076|共6页
  • 会议地点 Montreal(CA)
  • 作者

    Lee, Unsik;

  • 作者单位

    Department of Aeronautics and Astronautics University of Washington Seattle WA 98195-2400;

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