Attitude Agile Maneuvering Control for Spacecraft Equipped with Hybrid Actuators

被引：27
|
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
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2018年 / 41卷 / 03期
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
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