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Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (10): 329412-329412.doi: 10.7527/S1000-6893.2023.29412

• Electronics and Electrical Engineering and Control • Previous Articles     Next Articles

Event-triggered-based orbit maintenance control for spacecraft subsatellite point control

Kai NING, Baolin WU()   

  1. School of Astronautics,Harbin Institute of Technology,Harbin 150000,China
  • Received:2023-08-05 Revised:2023-08-29 Accepted:2023-10-31 Online:2024-05-25 Published:2023-11-01
  • Contact: Baolin WU E-mail:wubaolin@hit.edu.cn
  • Supported by:
    National Natural Science Foundation of China(62188101)

Abstract:

A fuzzy adaptive control method based on event-triggered mechanism is proposed for high precision autonomous orbit maintenance of ultra-low orbit spacecraft with limited communication and atmosphere drag perturbation. Firstly, a spacecraft orbit dynamics model is established based on the relative average orbital elements. The fuzzy adaptive control method is used to estimate the nonlinear function caused by atmosphere drag. Then, an event-triggered mechanism placed on the controller cellular satellite is proposed to reduce the communication burden and computation. Meanwhile, constant control thrust over a certain period of time can be ensured which can extend the lifetime of electric thrust cellular satellite. An event-triggered-based fuzzy adaptive autonomous orbit maintenance controller is designed for maintaining subsatellite point trajectory. Finally, the effectiveness of the proposed control algorithm is verified through simulation results.

Key words: ultra-low orbit spacecraft, atmosphere drag, autonomous orbit maintenance, event-triggered mechanism, fuzzy adaptive control

CLC Number: