Finite-time velocity-free relative position coordinated control of spacecraft formation with dynamic event triggered transmission

Jiao Wu; Shi Qiu; Ming Liu; Huayi Li; Yuan Liu; Jiao Wu; Shi Qiu; Ming Liu; Huayi Li; Yuan Liu

doi:10.3934/mbe.2022324

Mathematical Biosciences and Engineering

2022, Volume 19, Issue 7: 6883-6906. doi: 10.3934/mbe.2022324

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Finite-time velocity-free relative position coordinated control of spacecraft formation with dynamic event triggered transmission

Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150001, China

Academic Editor:Hamid Reza Karimi

Received: 28 February 2022 Revised: 11 April 2022 Accepted: 14 April 2022 Published: 07 May 2022

This paper investigates the finite-time relative position coordinated control problem of distributed spacecraft formation without velocity information over limited communication bandwidth. In this design, a dynamic event triggered transmission scheme among spacecraft is designed to reduce communication burden, and a finite-time extended state observer is proposed to estimate the velocity information and the effects of non-linearity and disturbance of each spacecraft. A fast terminal sliding mode control law is developed to achieve finite-time coordination of the overall spacecraft formation. Finally, a numerical simulation is presented to demonstrate the effectiveness of the proposed control strategy.
- spacecraft formation,
- relative position coordinated control,
- finite-time control,
- dynamic event trigger,
- extended state observer
Citation: Jiao Wu, Shi Qiu, Ming Liu, Huayi Li, Yuan Liu. Finite-time velocity-free relative position coordinated control of spacecraft formation with dynamic event triggered transmission[J]. Mathematical Biosciences and Engineering, 2022, 19(7): 6883-6906. doi: 10.3934/mbe.2022324

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Abstract

This paper investigates the finite-time relative position coordinated control problem of distributed spacecraft formation without velocity information over limited communication bandwidth. In this design, a dynamic event triggered transmission scheme among spacecraft is designed to reduce communication burden, and a finite-time extended state observer is proposed to estimate the velocity information and the effects of non-linearity and disturbance of each spacecraft. A fast terminal sliding mode control law is developed to achieve finite-time coordination of the overall spacecraft formation. Finally, a numerical simulation is presented to demonstrate the effectiveness of the proposed control strategy.

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