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
下载
收藏
页码：803 / 812
页数：10
相关论文
共 50 条
  • [21] Exponential and Resilient Control for Attitude Tracking Maneuvering of Spacecraft With Actuator Uncertainties
    Cao, Lu
    Xiao, Bing
    IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2019, 24 (06) : 2531 - 2540
  • [22] Coordinated attitude control of spacecraft based on distributed intelligent actuators
    Li W.
    Wu Y.
    Zhu Y.
    Xu X.
    Chen Z.
    Hua B.
    Yu D.
    Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University, 2022, 43 (05): : 639 - 648
  • [23] A time suboptimal method for real-time spacecraft attitude agile maneuvering with angular velocity constraint
    Wu, Yun-Hua
    Hu, Ya-Bo
    Hua, Bing
    Chen, Zhi-Ming
    Ge, Lin-Lin
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2019, 233 (02) : 561 - 572
  • [24] HYBRID CONTROL FOR RAPID SPACECRAFT ATTITUDE MANEUVERS
    Hou, Zhili
    Wang, Xueqian
    Li, Zhiheng
    Liang, Bin
    Huang, Simeng
    FOURTH IAA CONFERENCE ON DYNAMICS AND CONTROL OF SPACE SYSTEMS 2018, PTS I-III, 2018, 165 : 1049 - 1066
  • [25] Agile Spacecraft Attitude Control: an Incremental Nonlinear Dynamic Inversion Approach
    Acquatella, Paul B.
    Chu, Qi Ping
    IFAC PAPERSONLINE, 2020, 53 (02): : 5709 - 5716
  • [26] Large angle attitude control of spacecraft based on on-off actuators
    Zhou, Di, 1792, Chinese Institute of Electronics (36):
  • [27] Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators
    N. E. Zubov
    E. A. Mikrin
    M. Sh. Misrikhanov
    V. N. Ryabchenko
    Journal of Computer and Systems Sciences International, 2015, 54 : 621 - 628
  • [28] Spacecraft attitude control with simultaneous unloading of the angular momentum of inertial actuators
    Zubov, N. E.
    Mikrin, E. A.
    Misrikhanov, M. Sh.
    Ryabchenko, V. N.
    JOURNAL OF COMPUTER AND SYSTEMS SCIENCES INTERNATIONAL, 2015, 54 (04) : 621 - 628
  • [29] Review:A Survey of Single Gimbal Control Moment Gyroscope for Agile Spacecraft Attitude Control
    Yunhua Wu
    Feng Han
    Bing Hua
    Zhiming Chen
    Dafu Xu
    Linlin Ge
    Journal of Harbin Institute of Technology(New series), 2018, 25 (06) : 22 - 45
  • [30] Adaptive control for flexible spacecraft attitude maneuvering based on variable speed control moment gyroscopes
    Lin Z.
    Lu G.
    Lyu W.
    Wu B.
    Li H.
    Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology, 56 (04): : 1 - 11
12345