Attitude Agile Maneuvering Control for Spacecraft Equipped with Hybrid Actuators

被引:28
作者
Wu, Yun-Hua [1 ]
Han, Feng [1 ,3 ]
Zhang, Shi-Jie [2 ]
Hua, Bing [1 ]
Chen, Zhi-Ming [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Sch Astronaut, Microsatellite Res Ctr, Nanjing 210016, Jiangsu, Peoples R China
[2] Harbin Inst Technol, Sch Astronaut, Res Ctr Satellite Technol, Harbin 150001, Heilongjiang, Peoples R China
[3] Harbin Inst Technol, Res Ctr Satellite Technol, Harbin 150001, Heilongjiang, Peoples R China
基金
中国国家自然科学基金;
关键词
CONTROL MOMENT GYROS; SINGULARITY ANALYSIS; SYSTEMS; LOGIC; LAWS;
D O I
10.2514/1.G002982
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
[No abstract available]
引用
收藏
页码:803 / 812
页数:10
相关论文
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