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Event-triggered coordinated attitude method for chip satellite cluster

机译:芯片卫星簇的事件触发协调姿态方法

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摘要

Event-triggered coordinated attitude control problem for chip satellite cluster was investigated in this paper. Considering the constraints of computation, measurement and communication on chip satellites, adaptive attitude tracking controller based on event-triggered strategy was proposed for chip satellite cluster with leader-follower architecture. Triggering function with state tracking error was designed to adjust update period of controller, event was triggered and controller was updated once triggering function value satisfied the condition, while controller in non-triggering time used state information of triggering time. As the state of cluster system gradually tended to be stable, triggering frequency was reduced, which effectively reduced update frequency of controller and reduced resource on board. Cluster system was proved to be globally asymptotical convergence by Lyapunov stability theory. Simulation results showed that the proposed event-triggered adaptive attitude tracking controller could reduce control execution frequency, meet the constraints of resource and ability of chip satellites, as well as ensure control performance of cluster system. The influence of control gain coefficients and triggering parameters on control performance of cluster system were further analyzed, and criterion for parameters design was provided.
机译:本文研究了芯片卫星集群的事件触发的协调姿态控制问题。考虑到芯片卫星的计算,测量和通信,基于事件触发策略的自适应姿态跟踪控制器被提出了具有引导跟随器架构的芯片卫星集群。使用状态跟踪错误触发功能旨在调整控制器的更新周期,触发事件并更新了控制器一旦触发功能值满足条件,而控制器在非触发时间使用触发时间的状态信息。由于集群系统逐渐趋于稳定,因此减少了触发频率,从而有效减少了控制器的更新频率和船上的减少资源。被证明集群系统由Lyapunov稳定性理论成为全球渐近趋同。仿真结果表明,建议的事件触发的自适应姿态跟踪控制器可以减少控制执行频率,符合芯片卫星的资源和能力的约束,以及确保集群系统的控制性能。进一步分析了对照增益系数的影响和触发参数对集群系统的控制性能的影响,提供了参数设计的标准。

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