Model independent near eigenaxis rotation for spacecraft maneuver under slew rate and control constraints

被引：0
|
作者：
Cao, Xi-Bin [1 ]
Wang, Feng [1 ]
Zhang, Shi-Jie [1 ]
机构：
[1] Research Center of Satellite Technology, Harbin Institute of Technology, Harbin 150001, China
来源：
Harbin Gongye Daxue Xuebao/Journal of Harbin Institute of Technology | 2006年 / 38卷 / 09期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1413 / 1418
相关论文
共 50 条
  • [31] Adaptive attitude maneuver control for liquid-filled spacecraft with angular velocity and torque constraints
    Zhang, Wei
    Guo, Yanning
    Ran, Guangtao
    Wu, Yongbao
    Lam, Hak-keung
    NONLINEAR DYNAMICS, 2025, 113 (07) : 6941 - 6957
  • [32] Model Predictive Control of a Flexible Spacecraft with Constraints on Torques
    Koc, Ahmet Burak
    Olca, Mert
    Dogruer, Can Ulas
    2023 10TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN AIR AND SPACE TECHNOLOGIES, RAST, 2023,
  • [33] Artificial potential function based spacecraft proximity maneuver 6-DOF control under multiple pyramid-type constraints
    Wang, Liangyue
    Guo, Yanning
    Ma, Guangfu
    Zhang, Haibo
    ISA TRANSACTIONS, 2022, 126 : 316 - 325
  • [34] Saturated Attitude Control for Rigid Spacecraft Under Attitude Constraints
    Hu, Qinglei
    Liu, Yueyang
    Dong, Hongyang
    Zhang, Youmin
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2020, 43 (04) : 790 - 805
  • [35] Characteristic Model-Based Large Angle Maneuver Attitude Control for Spacecraft
    Sun Yujia
    Yuan Li
    Lei Yongjun
    PROCEEDINGS OF THE 36TH CHINESE CONTROL CONFERENCE (CCC 2017), 2017, : 3379 - 3384
  • [36] Inverse Dynamics based Model Predictive Control for Spacecraft Rapid Attitude Maneuver
    Song, Chao
    Islas, Genaro
    Schilling, Klaus
    IFAC PAPERSONLINE, 2019, 52 (12): : 111 - 116
  • [37] Energy optimal spacecraft attitude control subject to convergence rate constraints
    Horri, Nadjim M.
    Palmer, Philip L.
    Roberts, Mark
    CONTROL ENGINEERING PRACTICE, 2011, 19 (11) : 1297 - 1314
  • [38] Sliding Mode Attitude Control of Spacecraft Considering Angular Rate Constraints
    Kim, Min-young
    Jang, Seok-ho
    Leeghim, Henzeh
    JOURNAL OF THE KOREAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2021, 49 (02) : 129 - 138
  • [39] Robust attitude control design for spacecraft under assigned velocity and control constraints
    Hu, Qinglei
    Li, Bo
    Zhang, Youmin
    ISA TRANSACTIONS, 2013, 52 (04) : 480 - 493
  • [40] CLOSED-FORM OPTIMAL MANEUVER CONTROL SOLUTIONS FOR UNDER-ACTUATED SPACECRAFT
    Kim, Donghoon
    Turner, James D.
    SPACEFLIGHT MECHANICS 2013, PTS I-IV, 2013, 148 : 2553 - 2566
12345