Near-Time-Optimal RepointingManeuver of a Spacecraft with One DOF for Final Attitude

Geng Yuanzhuo; Guo Yanning; Li Chuanjiang; Bai Xiaoli

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Near-Time-Optimal RepointingManeuver of a Spacecraft with One DOF for Final Attitude

机译：具有最终自由度的一个自由度的航天器的近时最佳重新定位操纵

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来源
《Journal of guidance, control, and dynamics 》 |2019年第7期| 1587-1594| 共8页
作者
Geng Yuanzhuo; Guo Yanning; Li Chuanjiang; Bai Xiaoli;
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Harbin Inst Technol, Dept Control Sci & Engn, West Dazhi St 92,Box 327,Room 606, Harbin 150001, Heilongjiang, Peoples R China;

Harbin Inst Technol, Dept Control Sci & Engn, West Dazhi St 92,Box 327,Room 421, Harbin 150001, Heilongjiang, Peoples R China;

Harbin Inst Technol, Dept Control Sci & Engn, West Dazhi St 92,Box 327,Room 325, Harbin 150001, Heilongjiang, Peoples R China;

Rutgers State Univ, Mech & Aerosp Engn, 98 Brett Rd EN B-222, Piscataway, NJ 08854 USA;

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1. Suboptimal Repointing Maneuver of a staring-mode spacecraft with one DOF for final attitude [J] . Li Chuanjiang, Geng Yuanzhuo, Guo Yanning, Acta astronautica . 2020 ,第Octa期

机译：凝视模式宇宙飞船的次优与一体的态度换取最终态度
2. Six-DOF Spacecraft Optimal Trajectory Planning and Real-Time Attitude Control: A Deep Neural Network-Based Approach [J] . Chai Runqi, Tsourdos Antonios, Savvaris Al, Neural Networks and Learning Systems, IEEE Transactions on . 2020 ,第11期

机译：六自由度航天器最优轨迹规划与实时态度控制：基于深度神经网络的方法
3. Spacecraft attitude maneuver control using two parallel mounted 3-DOF spherical actuators [J] . Li Guidan, Li Haike, Li Bin 中国航空学报（英文版） . 2017 ,第001期

机译：使用两个并联安装的3-DOF球形执行器进行航天器姿态操纵控制
4. Attitude determination of large non-cooperative spacecrafts in final approach [C] . The 11th International Conference on Control Automation Robotics and Vision . 2010

机译：大型非合作航天器在最终进近中的姿态确定
5. Spacecraft Attitude Control Program: A spacecraft attitude determination and control simulation program. [D] . Rajagopalan, Murlidhar. 1996

机译：航天器姿态控制程序：航天器姿态确定和控制模拟程序。
6. Questionable research practices in student final theses – Prevalence, attitudes, and the role of the supervisor’s perceived attitudes [O] . Anand Krishna, Sebastian M. Peter 2012

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7. Six-DOF Spacecraft Optimal Trajectory Planning and Real-Time Attitude Control: A Deep Neural Network-Based Approach [O] . Runqi Chai, Antonios Tsourdos, Al Savvaris, 2020

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8. ATTITUDE CONTROL OF THREE-AXES STABILISED SPACECRAFT WITH FLEXIBLE APPENDAGES RIDER NO. 1 - FINAL REPORT Volume II [R] . R.S. Harris, M.J. Hammond, D.C. Todman 1977

机译：具有灵活附件的三轴稳定航天器的姿态控制1 - 最终报告第二卷

Near-Time-Optimal RepointingManeuver of a Spacecraft with One DOF for Final Attitude

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