基于事件触发的航天器变周期控制方法研究

Abstract

Abstract: Abstract：Future spacecraft will have much autonomous work. And the utilization of embedded system continues growing with data increasing. In this paper, a nonlinear event triggered control approach is applied for the spacecraft attitude control. By this approach, the utilization of bus bandwidth decreases greatly and a good control performance is achieved. Moreover, the design procedure and stability proof of this algorithm are given via perturbation theorem. Finally, a numerical example is provided to illustrate the efficiency and feasibility of the proposed approach.

Key words: Keywords：cyberphysical system, eventtriggered control, attitude control, bus bandwidth

CLC Number:

SUN Shuai, WANG Lei, WANG Zhi-Wen- . Aperiodic Spacecraft Control Method：An Event Triggered Approach[J]., 2018, 44(2): 31-35.

References

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Aperiodic Spacecraft Control Method：An Event Triggered Approach

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