Robust Saturated Finite-Time Attitude Control for Spacecraft Using Integral Sliding Mode

Guo Yong; Huang Bing; Song Shen-min; Li Ai-jun; Wang Chang-qing

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Robust Saturated Finite-Time Attitude Control for Spacecraft Using Integral Sliding Mode

机译：使用积分滑模的航天器鲁棒饱和有限时间姿态控制

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《Journal of guidance, control, and dynamics 》 |2019年第2期| 440-446| 共7页
作者
Guo Yong; Huang Bing; Song Shen-min; Li Ai-jun; Wang Chang-qing;
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Northwestern Polytech Univ, Xian 710129, Shaanxi, Peoples R China|Sch Automat, 127 Youyi West Rd, Beilin, Shaanxi, Peoples R China;

Northwestern Polytech Univ, Xian 710129, Shaanxi, Peoples R China|Sch Automat, 127 Youyi West Rd, Beilin, Shaanxi, Peoples R China;

Harbin Inst Technol, Ctr Control Theory & Guidance Technol, Harbin 150001, Heilongjiang, Peoples R China;

Northwestern Polytech Univ, Xian 710129, Shaanxi, Peoples R China|Sch Automat, 127 Youyi West Rd, Beilin, Shaanxi, Peoples R China;

Northwestern Polytech Univ, Xian 710129, Shaanxi, Peoples R China|Sch Automat, 127 Youyi West Rd, Beilin, Shaanxi, Peoples R China;

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1. Robust spacecraft attitude tracking control with integral terminal sliding mode surface considering input saturation [J] . Chen Haitao, Song Shenmin, Li Xuehui Transactions of the Institute of Measurement and Control . 2019 ,第2期

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2. Robust stabilization of spacecraft attitude motion under magnetic control through time-varying integral sliding mode [J] . Sofyali Ahmet, Jafarov Elbrous M. International Journal of Robust and Nonlinear Control . 2019 ,第11期

机译：通过时变整个滑动模式在磁控控制下的稳健稳定在磁控下的稳定
3. Finite-time cooperative attitude control of multiple spacecraft using terminal sliding mode control technique [J] . Haibo Du, Shihua Li International Journal of Modelling, Identification and Control . 2012 ,第4期

机译：利用终端滑模控制技术的多航天器有限时间协同姿态控制
4. A finite-time convergent continuous time sliding mode controller for spacecraft attitude control [C] . Tiwari Pyare Mohan, Janardhanan S, Nabi Mashuq un Proceedings of the 2010 11th International Workshop on Variable Structure Systems . 2010

机译：用于航天器姿态控制的有限时间收敛连续时间滑模控制器
5. Robust autopilot design for lunar spacecraft powered descent using high order sliding mode control. [D] . Orr, Jeb S. 2009

机译：采用高阶滑模控制的月球航天器动力下降的鲁棒自动驾驶仪设计。
6. Finite-Time Attitude Stabilization Adaptive Control for Spacecraft with Actuator Dynamics [O] . Chunbao Wang, Dong Ye, Zhongcheng Mu, 2019

机译：具有执行器动力学的航天器航天器的有限时间态度稳定控制
7. Robustness and Actuator Bandwidth of MRP-Based Sliding Mode Control for Spacecraft Attitude Control Problems [O] . Jung-Hoon Keum, Sung-Woong Ra 2009

机译：基于mRp的航天器姿态控制问题滑模控制的鲁棒性和执行器带宽
8. Nonlinear Decoupling Sliding Mode Control and Attitude Control of Spacecraft. [R] . Nartker, T. A., Singh, S. N., Iyer, A. 1989

机译：航天器非线性解耦滑模控制与姿态控制。

Robust Saturated Finite-Time Attitude Control for Spacecraft Using Integral Sliding Mode

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