Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation

LIU Gaoqi, ZHANG Kai, LI Bin

系统科学与复杂性(英文) ›› 2022, Vol. 35 ›› Issue (2) : 688-702.

PDF(310 KB)
中国科学院数学与系统科学研究院期刊网
JSSC
PDF(310 KB)
系统科学与复杂性(英文) ›› 2022, Vol. 35 ›› Issue (2) : 688-702. DOI: 10.1007/s11424-022-1515-8

Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation

    LIU Gaoqi, ZHANG Kai, LI Bin
作者信息 +

Fully-Actuated System Approach Based Optimal Attitude Tracking Control of Rigid Spacecraft with Actuator Saturation

    LIU Gaoqi, ZHANG Kai, LI Bin
Author information +
文章历史 +

本文亮点

{{article.keyPoints_cn}}

HeighLight

{{article.keyPoints_en}}

摘要

{{article.zhaiyao_cn}}

Abstract

{{article.zhaiyao_en}}

关键词

Key words

本文二维码

引用本文

EndNote

Ris (Procite)

Bibtex

导出引用
{{article.zuoZheCn_L}}. {{article.title_cn}}. {{journal.qiKanMingCheng_CN}}, 2022, 35(2): 688-702 https://doi.org/10.1007/s11424-022-1515-8
{{article.zuoZheEn_L}}. {{article.title_en}}. {{journal.qiKanMingCheng_EN}}, 2022, 35(2): 688-702 https://doi.org/10.1007/s11424-022-1515-8
中图分类号：

参考文献

原文顺序 | 文献年度倒序 | 文中引用次数倒序

参考文献

{{article.reference}}

基金

版权

{{article.copyrightStatement_cn}}
{{article.copyrightLicense_cn}}
PDF(310 KB)

Accesses

Citation

Detail
段落导航
相关文章

/

〈 〉