Finite-Time Attitude Stabilization Adaptive Control for Spacecraft with Actuator Dynamics

For the attitude stabilization of spacecraft with actuator dynamics, this paper proposed a finite-time control law. Firstly, the dynamic property of the actuator is analyzed by an example. Then, a basic control law is derived to achieve the finite-time stability using the double fast terminal slidin...

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Detalles Bibliográficos
Autores principales: Wang, Chunbao, Ye, Dong, Mu, Zhongcheng, Sun, Zhaowei, Wu, Shufan
Formato: Online Artículo Texto
Lenguaje:English
Publicado: MDPI 2019
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6960679/
https://www.ncbi.nlm.nih.gov/pubmed/31888307
http://dx.doi.org/10.3390/s19245568

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC6960679/
https://www.ncbi.nlm.nih.gov/pubmed/31888307
http://dx.doi.org/10.3390/s19245568

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