Self-Triggered 6-DOF Formation Control for Multispacecraft Systems With Restricted Communication and Computation Resources

The 6-DOF event-based formation control issue for multispacecraft systems considering unknown disturbances is investigated. First, a 6-DOF coupling dynamics is given, and a 6-DOF dynamic event-driven formation controller is designed to achieve stability and avoid continuous data transmission. The formation spacecraft updates its controller and transmits its states at the trigger instants. Further, a self-triggered function using triggering states to calculate the next triggering moment is designed to save computing resources. It should be noted that the logarithmic function does not need to be used in the computation of the next trigger moment, significantly improving resource conservation's effectiveness. Furthermore, the developed 6-DOF event-driven controllers make the system bounded stable and Zeno-free. Finally, simulations present that the self-triggered mechanism avoids the continuous computation of the trigger function while reducing the communication resource-saving efficiency by only 7% compared with the dynamic trigger mechanism.

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Publication Details

Journal
IEEE Transactions on Aerospace and Electronic Systems
Published
2024-11-25
DOI
https://doi.org/10.1109/taes.2024.3501233
Primary Topic
Space Satellite Systems and Control
Type
article
Field-Weighted Citation Impact
0.00
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article

Self-Triggered 6-DOF Formation Control for Multispacecraft Systems With Restricted Communication and Computation Resources

Xiong Xie, Tao Sheng
IEEE Transactions on Aerospace and Electronic Systems
Space Satellite Systems and Control
article

Self-Triggered 6-DOF Formation Control for Multispacecraft Systems With Restricted Communication and Computation Resources

Xiong Xie, Tao Sheng
article en

Abstract

The 6-DOF event-based formation control issue for multispacecraft systems considering unknown disturbances is investigated. First, a 6-DOF coupling dynamics is given, and a 6-DOF dynamic event-driven formation controller is designed to achieve stability and avoid continuous data transmission. The formation spacecraft updates its controller and transmits its states at the trigger instants. Further, a self-triggered function using triggering states to calculate the next triggering moment is designed to save computing resources. It should be noted that the logarithmic function does not need to be used in the computation of the next trigger moment, significantly improving resource conservation's effectiveness. Furthermore, the developed 6-DOF event-driven controllers make the system bounded stable and Zeno-free. Finally, simulations present that the self-triggered mechanism avoids the continuous computation of the trigger function while reducing the communication resource-saving efficiency by only 7% compared with the dynamic trigger mechanism.

IEEE Transactions on Aerospace and Electronic SystemsVol. 61(2)
National University of Defense Technology (CN)
Openalex Percentile: Top 67%
Space Satellite Systems and Control
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Self-Triggered 6-DOF Formation Control for Multispacecraft Systems With Restricted Communication and Computation Resources — Xiong Xie, Tao Sheng · IEEE Transactions on Aerospace and Electronic Systems (2024) | TGRS Research Map | TGRS