2022
DOI: 10.1016/j.actaastro.2022.07.035
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Adaptive dynamic event-triggered deployment control for space triangle tethered formation system with external disturbance

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Cited by 12 publications
(5 citation statements)
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“…12 Therefore, DET mechanism-based distributed coordination control for SFF systems with limited communications has been a focus, of which recent progresses have been reported. [13][14][15][16][17] For the SFF systems without the velocity measurement unit, extended state observer (ESO)-based adaptive sliding mode control (SMC) strategy with the DET mechanism is considered, and a finite-time ESO is used to observe external disturbances while a fast terminal SMC law is developed for finite-time orbit coordination. 13 A DET mechanism-based adaptive SMC law is designed to achieve configuration maintenance and reconfiguration for drag-free spacecraft inner-formation.…”
Section: Introductionmentioning
confidence: 99%
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“…12 Therefore, DET mechanism-based distributed coordination control for SFF systems with limited communications has been a focus, of which recent progresses have been reported. [13][14][15][16][17] For the SFF systems without the velocity measurement unit, extended state observer (ESO)-based adaptive sliding mode control (SMC) strategy with the DET mechanism is considered, and a finite-time ESO is used to observe external disturbances while a fast terminal SMC law is developed for finite-time orbit coordination. 13 A DET mechanism-based adaptive SMC law is designed to achieve configuration maintenance and reconfiguration for drag-free spacecraft inner-formation.…”
Section: Introductionmentioning
confidence: 99%
“…14 Based on adaptive integral sliding mode strategy, the DET mechanism-based finite-time formation configuration issue for space tethered system with limited communications is investigated, and an adaptive neural network estimator is applied to approximate system coupling nonlinearities. 15 A DET mechanism-based adaptive appointed-time formation tracking control approach is proposed for multiple spacecraft formation with collision avoidance. 16 The issue of DET mechanism-based adaptive optimal tracking control for SFF systems with event-trigger input is studied, and a single-critic adaptive neural network is developed to approximate the optimal cost function.…”
Section: Introductionmentioning
confidence: 99%
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