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

LUO Weiwei, ZHOU Bin

Journal of Systems Science and Mathematical Sciences ›› 2025

PDF(888 KB)
PDF(888 KB)
Journal of Systems Science and Mathematical Sciences ›› 2025 DOI: 10.12341/jssms250322

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

  • LUO Weiwei1, ZHOU Bin2,3
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 https://doi.org/10.12341/jssms250322

References

References

{{article.reference}}

Funding

RIGHTS & PERMISSIONS

{{article.copyrightStatement_en}}
{{article.copyrightLicense_en}}
PDF(888 KB)

Accesses

Citation

Detail

Sections
Recommended

/