A low-thrust finite state machine based controller for N-satellites formations in distributed synthetic aperture radar applications

Author:

Vela ClaudioORCID,Opromolla RobertoORCID,Fasano Giancarmine

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference39 articles.

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4. Minimum-fuel control strategy for spacecraft formation reconfiguration via finite-time maneuvers;Di Mauro;J. Guid. Control Dynam.,2019

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Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Performance Evaluation of Different Finite State Machines Implementations;2024 13th International Conference on Modern Circuits and Systems Technologies (MOCAST);2024-06-26

2. Distributed safe trajectory optimization for large-scale spacecraft formation reconfiguration;Acta Astronautica;2024-01

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