Global Stabilization of the Axisymmetric Spacecraft Attitude Control System with Actuator Saturation

LUO Weiwei, ZHOU Bin

Journal of Systems Science and Mathematical Sciences ›› 2025, Vol. 45 ›› Issue (12) : 3728-3742.

PDF(400 KB)
PDF(400 KB)
Journal of Systems Science and Mathematical Sciences ›› 2025, Vol. 45 ›› Issue (12) : 3728-3742. DOI: 10.12341/jssms250322

Global Stabilization of the Axisymmetric Spacecraft Attitude Control System with Actuator Saturation

  • LUO Weiwei1,2, ZHOU Bin3,4
Author information +
History +

HeighLight

{{article.keyPoints_en}}

Abstract

{{article.zhaiyao_en}}

Key words

QR code of this article

Cite this article

Download Citations
{{article.zuoZheEn_L}}. {{article.title_en}}. Journal of Systems Science and Mathematical Sciences, 2025, 45(12): 3728-3742 https://doi.org/10.12341/jssms250322

References

References

{{article.reference}}

Funding

RIGHTS & PERMISSIONS

{{article.copyrightStatement_en}}
{{article.copyrightLicense_en}}
PDF(400 KB)

Accesses

Citation

Detail

Sections
Recommended

/