空间控制技术发展与展望

袁利; 姜甜甜; 魏春岭; 杨孟飞

doi:10.16383/j.aas.c220792

空间控制技术发展与展望

doi: 10.16383/j.aas.c220792

袁利^{1, 2, 3,},
姜甜甜^{1, 3,},
魏春岭^{1, 3,},
杨孟飞^{2, 3,}

1.
北京控制工程研究所北京 100094
2.
中国空间技术研究院北京 100094
3.
空间智能控制技术全国重点实验室北京 100094

基金项目: 国家自然科学基金(U21B6001)资助

详细信息

作者简介:
袁利：北京控制工程研究所研究员. 主要研究方向为航天器自主控制和鲁棒容错控制. E-mail: yuanli@spacechina.com

姜甜甜：北京控制工程研究所高级工程师. 主要研究方向为航天器控制和非线性控制. 本文通信作者. E-mail: jiangtt@amss.ac.cn

魏春岭：北京控制工程研究所研究员. 主要研究方向为估计理论, 控制理论和航天器自主导航. E-mail: clwei502@163.com

杨孟飞：中国空间技术研究院研究员. 主要研究方向为空间飞行器系统总体, 控制系统, 控制计算机和可信软件. E-mail: yangmf@bice.org.cn

计量
- 文章访问数: 4691
- HTML全文浏览量: 514
- PDF下载量: 628
- 被引次数: 0
出版历程
- 收稿日期: 2022-10-09
- 录用日期: 2022-12-09
- 网络出版日期: 2023-02-01
- 刊出日期: 2023-03-20

Advances and Perspectives of Space Control Technology

YUAN Li^{1, 2, 3
,},
JIANG Tian-Tian^{1, 3
,},
WEI Chun-Ling^{1, 3
,},
YANG Meng-Fei^{2, 3
,}

1.
Beijing Institute of Control Engineering, Beijing 100094
2.
China Academy of Space Technology, Beijing 100094
3.
National Key Laboratory of Space Intelligent Control, Beijing 100094

Funds: Supported by National Natural Science Foundation of China (U21B6001)

More Information

Author Bio:
YUAN Li　Professor at Beijing Institute of Control Engineering. His research interest covers spacecraft autonomous control and robust fault-tolerant control

JIANG Tian-Tian　Senior engineer at Beijing Institute of Control Engineering. Her research interest covers spacecraft control and nonlinear control. Corresponding author of this paper

WEI Chun-Ling　Professor at Beijing Institute of Control Engineering. His research interest covers estimation theory, control theory, and spacecraft autonomous navigation

YANG Meng-Fei　Professor at China Academy of Space Technology. His research interest covers spacecraft system, control system, control computer, and trustworthy software

摘要

摘要: 控制是航天器在空间环境下自主完成复杂任务的关键技术. 首先梳理了中国空间控制技术过去50多年来的发展成果, 总结划分为航天器姿态控制、姿态轨道控制、“感知−决策−执行” (Perception-decision-action, PDA)自主控制三个方面, 并在综述了各方面主要进展的基础上, 围绕超大结构航天器姿态轨道控制、轨道空间博弈控制、网络化航天器集群控制、地外探测智能无人系统控制、跨域航天器自主控制、在轨建造与维护(On-orbit servicing, assembly, and manufacturing, OSAM)控制6个技术方向, 提出面临的挑战和需要重点关注的基础性问题, 为空间控制技术未来的发展提供借鉴和参考.
- 空间控制技术 /
- 姿态控制 /
- 姿态轨道控制 /
- “感知−决策−执行”自主控制 /
- 超大结构航天器 /
- 轨道空间博弈 /
- 网络化航天器集群 /
- 地外探测 /
- 跨域航天器 /
- 在轨建造与维护
Abstract: Control has a key role in enabling spacecraft to perform complex tasks in space environment autonomously. After a brief review of the development of space control technology in China over the past 50 years, we focus on the main progress of the three aspects from the spacecraft attitude control to the attitude-orbit control, and then to the “perception-decision-action” (PDA) autonomous control. Based on which, and an analysis of the challenges brought by more complex space missions in the future, some fundamental control issues worthy of follow-up focus are involved, especially in the fields of extra-large spacecraft, orbital games, networked spacecraft swarms, extraterrestrial operations, cross-domain spacecraft and on-orbit servicing, assembly, and manufacturing (OSAM).

HTML全文

图 1 空间控制技术三个方面包含关系韦恩图

Fig. 1 Venn diagram illustrating the relationship between the three aspects of space control technology

下载: 全尺寸图片幻灯片

参考文献(164)

[1]	中国空间技术研究院. 中国航天器. 北京: 电子工业出版社, 2008. China Academy of Space Technology. Chinese Spacecraft. Beijing: Publishing House of Electronics Industry, 2008.
[2]	Iwata T. Precision on-board orbit model for attitude control of the advanced land observing satellite (ALOS). Journal of Aerospace Engineering Sciences and Applications, 2012, 4(3): 62-74
[3]	ALOS-2 — Satellite overview [Online], available: https://spaceflight101.com/spacecraft/alos-2/, November 20, 2022
[4]	WorldView-4 [Online], available: https://www.eoportal.org/satellite-missions/worldview-4#worldview-4-formerly-geoeye-2, January 28, 2023
[5]	屠善澄, 吕振铎, 邹广瑞, 邢光谦, 刘良栋. 中国同步试验通信卫星STW-1的控制. 宇航学报, 1986, 7(4): 1-13 Tu Shan-Cheng, Lü Zhen-Duo, Zou Guang-Rui, Xing Guang-Qian, Liu Liang-Dong. Control of the Chinese geostationary experimental communication satellite STW-1. Journal of Astronautics, 1986, 7(4): 1-13
[6]	吕振铎. 地球同步通信广播卫星的两种姿态控制方式. 中国空间科学技术, 1990(1): 28-35 Lü Zhen-Duo. Two different attitude control methods for geostationary communication broadcasting satellite. Chinese Space Science and Technology, 1990(1): 28-35
[7]	吕振铎, 李铁寿, 刘良栋. 实用通信广播卫星控制软件的改进. 宇航学报, 1990(1): 1-6 Lü Zhen-Duo, Li Tie-Shou, Liu Liang-Dong. Improvements in attitude and orbit control software for Chinese STW-2 satellite. Journal of Astronautics, 1990(1): 1-6
[8]	齐春子, 于嘉茹. FY-2C星控制分系统设计. 上海航天, 2005, 22(S1): 36-41 (查阅所有网上资料, 未找到对应的卷号信息, 请联系作者确认) Qi Chun-Zi, Yu Jia-Ru. Control subsystem design of FY-2C meteorological satellite. Aerospace Shanghai, 2005, 22(S1): 36-41
[9]	徐福祥. 第二颗风云一号试验气象卫星的技术改进. 世界导弹与航天, 1991(1): 5-7 Xu Fu-Xiang. The technological improvements of FY-l(B). Missiles & Spacecraft, 1991(1): 5-7
[10]	Xiong Y Z, Wu Y P, Cheng H Y, Liu D. The online estimation of relative alignments for multiple heads star tracker based on the invariability of inter-star angle principle. In: Proceedings of SPIE 10141, Selected Papers of the Chinese Society for Optical Engineering Conferences. Changchun, China: SPIE, 2016. 60−66
[11]	李骥, 张洪华, 赵宇, 梁俊, 张晓文, 关轶峰, 等. 嫦娥三号着陆器的陀螺在轨标定. 中国科学: 技术科学, 2014, 44(6): 582-588 doi: 10.1360/092014-54 Li Ji, Zhang Hong-Hua, Zhao Yu, Liang Jun, Zhang Xiao-Wen, Guan Yi-Feng, et al. In-flight calibration of the gyros of the Chang’E-3 lunar lander. Scientia Sinica Technologica, 2014, 44(6): 582-588 doi: 10.1360/092014-54
[12]	韩京清. 自抗扰控制技术 — 估计补偿不确定因素的控制技术. 北京: 国防工业出版社, 2008. Han Jing-Qing. Active Disturbance Rejection Control Technique — The Technique for Estimating and Compensating the Uncertainties. Beijing: National Defense Industry Press, 2008.
[13]	Han J Q. From PID to active disturbance rejection control. IEEE Transactions on Industrial Electronics, 2009, 56(3): 900-906 doi: 10.1109/TIE.2008.2011621
[14]	Guo L, Cao S Y. Anti-disturbance control theory for systems with multiple disturbances: A survey. ISA Transactions, 2014, 53(4): 846-849 doi: 10.1016/j.isatra.2013.10.005
[15]	Chen W H, Yang J, Guo L, Li S H. Disturbance-observer-based control and related methods - An overview. IEEE Transactions on Industrial Electronics, 2016, 63(2): 1083-1095 doi: 10.1109/TIE.2015.2478397
[16]	斯祝华, 刘一武. 帆板驱动影响下的卫星姿态高精度高稳定度控制. 宇航学报, 2010, 31(12): 2697-2703 Si Zhu-Hua, Liu Yi-Wu. High accuracy and high stability attitude control of a satellite with a rotating solar array. Journal of Astronautics, 2010, 31(12): 2697-2703
[17]	Chak Y C, Varatharajoo R, Razoumny Y. Disturbance observer-based fuzzy control for flexible spacecraft combined attitude & sun tracking system. Acta Astronautica, 2017, 133: 302-310 doi: 10.1016/j.actaastro.2016.12.028
[18]	Zou A M, de Ruiter A H J, Dev Kumar K. Disturbance observer-based attitude control for spacecraft with input MRS. IEEE Transactions on Aerospace and Electronic Systems, 2019, 55(1): 384-396 doi: 10.1109/TAES.2018.2852369
[19]	Liu Y W, Si Z H, Tang L, Chen S L. Angular momentum management strategy of the FengYun-4 meteorological satellite. Acta Astronautica, 2018, 151: 22-31 doi: 10.1016/j.actaastro.2018.05.031
[20]	Tang L, Chen S L, Wang K, Liu Y W. Fengyun-4 attitude control system design and its in-flight performance. Journal of Spacecraft and Rockets, 2019, 56(1): 200-210 doi: 10.2514/1.A34226
[21]	李明群, 雷拥军, 牟小刚. 具有载荷扰动抑制的卫星姿态控制方法及验证. 中国空间科学技术, 2019, 39(1): 73-77, 86 Li Ming-Qun, Lei Yong-Jun, Mu Xiao-Gang. Satellite attitude control method and physical test with load disturbance suppression. Chinese Space Science and Technology, 2019, 39(1): 73-77, 86
[22]	Lei Y J, Lu D N, Mu X G, Li L J, Chen C. Modelling and mitigation of dual-axis antenna-induced disturbances on spacecraft. In: Proceedings of the Chinese Control Conference (CCC). Guangzhou, China: IEEE, 2019. 3202−3207
[23]	陆栋宁, 雷拥军, 陈超. 具有运动约束的姿态机动路径规划方法研究. 见: 惯性技术与智能导航学术研讨会论文集. 昆明, 中国: 中国惯性技术学会, 2019. 237−244 Lu Dong-Ning, Lei Yong-Jun, Chen Chao. Research on attitude maneuvering path planning method with motion constraints. In: Proceedings of the Symposium on Inertial Technology and Intelligent Navigation. Kunming, China: China Inertial Technology Society, 2019. 237−244
[24]	陆栋宁, 郭超勇, 王淑一, 陈超. 星载运动附件扰动抑制方法研究. 中国空间科学技术, 2020, 40(5): 26-33 Lu Dong-Ning, Guo Chao-Yong, Wang Shu-Yi, Chen Chao. A disturbance mitigation method for moving appendages on spacecraft. Chinese Space Science and Technology, 2020, 40(5): 26-33
[25]	郭超勇, 陆栋宁, 陈超, 张猛, 于国庆. 高分七号卫星太阳翼驱动主动控制方案. 航天器工程, 2020, 29(3): 151-156 Guo Chao-Yong, Lu Dong-Ning, Chen Chao, Zhang Meng, Yu Guo-Qing. Drive and active control scheme of solar array for GF-7 satellite. Spacecraft Engineering, 2020, 29(3): 151-156
[26]	Pinilla-Alonso N, Stansberry J A, Holler B J. Surface properties of large TNOs: Expanding the study to longer wavelengths with the James Webb Space Telescope. The Trans-Neptunian Solar System. Amsterdam: Elsevier, 2020. 395−412
[27]	关新, 郑钢铁. 空间相机隔振与姿态控制一体化设计. 宇航学报, 2013, 34(2): 214-221 Guan Xin, Zheng Gang-Tie. Integrated design of space telescope vibration isolation and attitude control. Journal of Astronautics, 2013, 34(2): 214-221
[28]	刘潇翔, 胡军. 包含密集模态的空间结构的模糊主动振动控制. 空间控制技术与应用, 2010, 36(4): 18-24 Liu Xiao-Xiang, Hu Jun. Fuzzy vibration control of space structures with close modes. Aerospace Control and Application, 2010, 36(4): 18-24
[29]	李东旭. 大型挠性空间桁架结构动力学分析与模糊振动控制. 北京: 科学出版社, 2008. Li Dong-Xu. Large Flexible Space Truss Structures: Dynamic Analyses and Vibration Fuzzy Control. Beijing: Science Press, 2008.
[30]	杨鸿杰, 刘磊, 李新国. 超静空间科学卫星分离式主动隔振技术. 中国空间科学技术, 2021, 41(4): 102-110 Yang Hong-Jie, Liu Lei, Li Xin-Guo. Separated active vibration isolation technology for ultra-quiet scientific satellites. Chinese Space Science and Technology, 2021, 41(4): 102-110
[31]	郝仁剑, 汤亮, 关新. 基于观测器的超静卫星平台关节－任务空间鲁棒控制方法. 空间控制技术与应用, 2019, 45(3): 8-16 Hao Ren-Jian, Tang Liang, Guan Xin. Observer-based robust control for the Hexapod platform on the ultra-quiet spacecraft in the joint-task space. Aerospace Control and Application, 2019, 45(3): 8-16
[32]	王有懿, 汤亮, 何英姿. 超静平台动力学建模与解耦控制. 空间控制技术与应用, 2016, 42(4): 6-11 Wang You-Yi, Tang Liang, He Ying-Zi. Dynamic modeling and decoupled control of ultra quiet platform. Aerospace Control and Application, 2016, 42(4): 6-11
[33]	Kong Y F, Huang H. Vibration isolation and dual-stage actuation pointing system for space precision payloads. Acta Astronautica, 2018, 143: 183-192 doi: 10.1016/j.actaastro.2017.11.038
[34]	廖波, 梁健, 刘胜, 刘磊. 双超敏捷卫星载荷舱扰动补偿研究. 空间电子技术, 2019, 16(3): 48-54 Liao Bo, Liang Jian, Liu Sheng, Liu Lei. Disturbance compensation research of disturbance-free payload agility satellite with disturbances in payload module. Space Electronic Technology, 2019, 16(3): 48-54
[35]	许域菲, 赵艳彬. 基于音圈式Stewart平台的零刚度卫星复合姿态控制研究. 上海航天, 2017, 34(2): 52-60 Xu Yu-Fei, Zhao Yan-Bin. Complex attitude control study of a zero stiffness satellite based on voice coil Stewart platform. Aerospace Shanghai, 2017, 34(2): 52-60
[36]	Tang L, Guo Z X, Guan X, Wang Y Y, Zhang K B. Integrated control method for spacecraft considering the flexibility of the spacecraft bus. Acta Astronautica, 2020, 167: 73-84 doi: 10.1016/j.actaastro.2019.08.030
[37]	Tang L, Guo Z X. Integrated control and magnetic suspension for fast attitude maneuvering and stabilization. IEEE Transactions on Aerospace and Electronic Systems, 2019, 55(6): 3273-3283 doi: 10.1109/TAES.2019.2907343
[38]	Wie B, Bailey D, Heiberg C. Rapid multitarget acquisition and pointing control of agile spacecraft. Journal of Guidance, Control, and Dynamics, 2002, 25(1): 96-104 doi: 10.2514/2.4854
[39]	袁利, 王淑一, 雷拥军. 航天器姿态敏捷稳健控制方法与应用. 北京: 科学出版社, 2021. Yuan Li, Wang Shu-Yi, Lei Yong-Jun. Agile and Robustifying Attitude Control of Spacecraft: Methods and Applications. Beijing: Science Press, 2021.
[40]	Kojima H. Singularity analysis and steering control laws for adaptive-skew pyramid-type control moment gyros. Acta Astronautica, 2013, 85: 120-137 doi: 10.1016/j.actaastro.2012.12.019
[41]	孙羽佳, 袁利, 雷拥军. 基于指令力矩螺旋式搜索的SGCMG奇异规避方法. 空间控制技术与应用, 2016, 42(6): 26-30 Sun Yu-Jia, Yuan Li, Lei Yong-Jun. SGCMG singularity avoidance method based on command torque vector helix search. Aerospace Control and Application, 2016, 42(6): 26-30
[42]	雷拥军, 姚宁, 刘洁, 赵江涛, 朱琦, 何海锋, 等. 一种基于指令力矩矢量调节的控制力矩陀螺奇异规避方法, 中国 105388902A, 2016-03 Lei Yong-Jun, Yao Ning, Liu Jie, Zhao Jiang-Tao, Zhu Qi, He Hai-Feng, et al. A Command Torque Vector Regulation Based SGCMG Singularity Avoidance Method, CN 105388902A, March 2016
[43]	雷拥军, 袁利, 王淑一, 田科丰. SGCMG系统的力矩指令调节及动态分配操纵方法. 宇航学报, 2019, 40(7): 794-802 doi: 10.3873/j.issn.1000-1328.2019.07.008 Lei Yong-Jun, Yuan Li, Wang Shu-Yi, Tian Ke-Feng. A steering method with torque command adjustment and dynamic distribution for single-gimbal control moment gyro systems. Journal of Astronautics, 2019, 40(7): 794-802 doi: 10.3873/j.issn.1000-1328.2019.07.008
[44]	Creamer G, Delahunt P, Gates S, Levenson M. Attitude determination and control of Clementine during lunar mapping. Journal of Guidance, Control, and Dynamics, 1996, 19(3): 505-511 doi: 10.2514/3.21650
[45]	周端, 申晓宁, 郭毓, 陈庆伟, 胡维礼. 基于多目标优化的挠性航天器姿态机动路径规划. 南京理工大学学报, 2012, 36(5): 846-853 Zhou Duan, Shen Xiao-Ning, Guo Yu, Chen Qing-Wei, Hu Wei-Li. Profile planning for attitude maneuver of flexible spacecrafts based on multi-objective optimization. Journal of Nanjing University of Science and Technology, 2012, 36(5): 846-853
[46]	Zhang Y, Zhang J R. Combined control of fast attitude maneuver and stabilization for large complex spacecraft. Acta Mechanica Sinica, 2013, 29(6): 875-882 doi: 10.1007/s10409-013-0080-8
[47]	Wie B, Lu J B. Feedback control logic for spacecraft eigenaxis rotations under slew rate and control constraints. Journal of Guidance, Control, and Dynamics, 1995, 18(6): 1372-1379 doi: 10.2514/3.21555
[48]	Su W C, Drakunov S V, Ozguner U, Young K D. Sliding mode with chattering reduction in sampled data systems. In: Proceedings of the 32nd IEEE Conference on Decision and Control. San Antonio, USA: IEEE, 1993. 2452−2457
[49]	雷拥军, 陆栋宁, 关新. 一种对地姿态重定向的机动轨迹规划及控制方法. 航天控制, 2020, 38(1): 9-16 Lei Yong-Jun, Lu Dong-Ning, Guan Xin. A maneuver attitude trajectory planning and control method for earth remote-sensing satellite reorientations. Aerospace Control, 2020, 38(1): 9-16
[50]	Lee J F L, Yeichner J A, Matulenko R, Chang D S. Space station attitude control system. In: Proceedings of the 43rd International Astronautical Congress. Washington, USA: 1992.
[51]	中国宇航学会. 2018–2019 航天科学技术学科发展报告. 北京: 中国科学技术出版社, 2020. Chinese Society of Astronautics. Report on Advances in Space Science and Technology. Beijing: China Science and Technology Press, 2020.
[52]	Zhang J, He Y Z, Zhang J J. Attitude control and momentum management of inertially oriented space station. IFAC Proceedings Volumes, 2013, 46: 1-6
[53]	程迎坤, 孙承启, 张锦江. 空间站力矩平衡姿态和动量平衡姿态的研究. 航天控制, 2008, 26(2): 3-8 Cheng Ying-Kun, Sun Cheng-Qi, Zhang Jin-Jiang. Study on torque equilibrium attitude and momentum equilibrium attitude of the space station. Aerospace Control, 2008, 26(2): 3-8
[54]	刘将辉, 李海阳, 张亚坤. 空间站平均力矩平衡姿态的气动力矩影响. 国防科技大学学报, 2018, 40(5): 20-26 doi: 10.11887/j.cn.201805004 Liu Jiang-Hui, Li Hai-Yang, Zhang Ya-Kun. Influence of air torque on average torque equilibrium attitude of space station. Journal of National University of Defense Technology, 2018, 40(5): 20-26 doi: 10.11887/j.cn.201805004
[55]	张军, 张志方, 刘成瑞, 张锦江, 冯帅, 林瀚峥, 等. 中国空间站GNC系统设计与在轨验证. 中国科学: 技术科学, 2022, 52(9): 1355-1374 doi: 10.1360/SST-2021-0517 Zhang Jun, Zhang Zhi-Fang, Liu Cheng-Rui, Zhang Jin-Jiang, Feng Shuai, Lin Han-Zheng, et al. Design and on-orbit verification of the guidance, navigation and control system of the China space station. Scientia Sinica Technologica, 2022, 52(9): 1355-1374 doi: 10.1360/SST-2021-0517
[56]	Flores-Abad A, Wei Z, Ma O, Pham K. Optimal control of space robots for capturing a tumbling object with uncertainties. Journal of Guidance, Control, and Dynamics, 2014, 37(6): 2014-2017 doi: 10.2514/1.G000003
[57]	Huang P F, Wang M, Meng Z J, Zhang F, Liu Z X. Attitude takeover control for post-capture of target spacecraft using space robot. Aerospace Science and Technology, 2016, 51: 171-180 doi: 10.1016/j.ast.2016.02.006
[58]	Huang P F, Wang M, Meng Z J, Zhang F, Liu Z X, Chang H T. Reconfigurable spacecraft attitude takeover control in post-capture of target by space manipulators. Journal of the Franklin Institute, 2016, 353(9): 1985-2008 doi: 10.1016/j.jfranklin.2016.03.011
[59]	马广富, 高寒, 吕跃勇, 宋婷, 袁建平. 组合体航天器有限时间超螺旋反步姿态控制. 宇航学报, 2017, 38(11): 1168-1176 doi: 10.3873/j.issn.1000-1328.2017.11.005 Ma Guang-Fu, Gao Han, Lv Yue-Yong, Song Ting, Yuan Jian-Ping. Super-twisting observer based finite-time backstepping attitude control for a combined spacecraft. Journal of Astronautics, 2017, 38(11): 1168-1176 doi: 10.3873/j.issn.1000-1328.2017.11.005
[60]	Han D, Huang P F, Liu X Y, Yang Y. Combined spacecraft stabilization control after multiple impacts during the capture of a tumbling target by a space robot. Acta Astronautica, 2020, 176: 24-32 doi: 10.1016/j.actaastro.2020.05.035
[61]	Huang X W, Biggs J D, Duan G R. Post-capture attitude control with prescribed performance. Aerospace Science and Technology, 2020, 96: Article No. 105572
[62]	杨保华. 航天器制导、导航与控制. 北京: 中国科学技术出版社, 2011. Yang Bao-Hua. Guidance, Navigation and Control of Spacecraft. Beijing: China Science and Technology Press, 2011.
[63]	Crouch P. Spacecraft attitude control and stabilization: Applications of geometric control theory to rigid body models. IEEE Transactions on Automatic Control, 1984, 29(4): 321-331 doi: 10.1109/TAC.1984.1103519
[64]	Byrnes C I, Isidori A. On the attitude stabilization of rigid spacecraft. Automatica, 1991, 27(1): 87-95 doi: 10.1016/0005-1098(91)90008-P
[65]	郭朝礼, 张笃周, 王淑一. 欠驱动航天器滑模速率阻尼控制. 空间控制技术与应用, 2013, 39(4): 12-17 doi: 10.3969/j.issn.1674-1579.2013.04.003 Guo Chao-Li, Zhang Du-Zhou, Wang Shu-Yi. Sliding mode control for rate damping of underactuated spacecraft. Aerospace Control and Application, 2013, 39(4): 12-17 doi: 10.3969/j.issn.1674-1579.2013.04.003
[66]	张洪华, 王芳, 胡锦昌, 王泽国. 欠驱动挠性航天器的全姿态控制. 宇航学报, 2015, 36(4): 419-429 Zhang Hong-Hua, Wang Fang, Hu Jin-Chang, Wang Ze-Guo. All-attitude control for underactuated flexible spacecraft. Journal of Astronautics, 2015, 36(4): 419-429
[67]	Kim S, Kim Y. Spin-axis stabilization of a rigid spacecraft using two reaction wheels. Journal of Guidance, Control, and Dynamics, 2001, 24(5): 1046-1049 doi: 10.2514/2.4818
[68]	Lei Y J, Yuan L, Zhu Q, Wang Z G, Liu J. A steering method with multiobjective optimizing for nonredundant single-gimbal control moment gyro systems. IEEE Transactions on Industrial Electronics, 2022, 69(4): 4177-4184 doi: 10.1109/TIE.2021.3073357
[69]	雷拥军, 袁利, 刘其睿, 刘洁. 2-SGCMGs与磁力矩器的对地姿态混合控制方法. 中国空间科学技术, 2021, 41(1): 75-83 Lei Yong-Jun, Yuan-Li, Liu Qi-Rui, Liu Jie. An attitude hybrid control method for earth-orienting satellite systems with 2-SGCMGs and magnet torquers. Chinese Space Science and Technology, 2021, 41(1): 75-83
[70]	胡军, 李毛毛. 航天器进入制导方法综述. 航空学报, 2021, 42(11): Article No. 525048 Hu Jun, Li Mao-Mao. Review of spacecraft entry guidance method. Acta Aeronautica et Astronautica Sinica, 2021, 42(11): Article No. 525048
[71]	吴宏鑫, 胡军. 特征建模理论、方法和应用. 北京: 国防工业出版社, 2019. Wu Hong-Xin, Hu Jun. Theory, Methods and Applications of Characteristic Modeling. Beijing: National Defense Industry Press, 2019.
[72]	吴宏鑫, 胡军, 解永春. 基于特征模型的智能自适应控制. 合肥: 中国科学技术出版社, 2009. Wu Hong-Xin, Hu Jun, Xie Yong-Chun. Characteristic Model-based Intelligent Adaptive Control. Hefei: China Science and Technology Press, 2009.
[73]	吴宏鑫. 全系数自适应控制理论及其应用. 北京: 国防工业出版社, 1990. Wu Hong-Xin. Theory and Applications of All Coefficient Adaptive Control. Beijing: National Defense Industry Press, 1990.
[74]	胡军. 载人飞船全系数自适应再入升力控制. 宇航学报, 1998, 19(1): 8-12 Hu Jun. All coefficients adaptive reentry lifting control of manned spacecraft. Journal of Astronautics, 1998, 19(1): 8-12
[75]	解永春, 吴宏鑫. 黄金分割在自适应鲁棒控制器设计中的应用. 自动化学报, 1992, 18(2): 177-185 Xie Yong-Chun, Wu Hong-Xin. The application of the golden section in adaptive robust controller design. Acta Automatica Sinica, 1992, 18(2): 177-185
[76]	解永春, 胡军. 基于特征模型的智能自适应控制方法在交会对接中的应用. 系统科学与数学, 2013, 33(9): 1017-1023 Xie Yong-Chun, Hu Jun. The application of the intelligent adaptive control method based on characteristic model in rendezvous and docking. Journal of Systems Science and Mathematical Sciences, 2013, 33(9): 1017-1023
[77]	杨孟飞, 张高, 张伍, 彭兢, 王勇, 王晓磊, 等. 探月三期月地高速再入返回飞行器技术设计与实现. 中国科学: 技术科学, 2015, 45(2): 111-123 doi: 10.1360/N092014-00484 Yang Meng-Fei, Zhang Gao, Zhang Wu, Peng Jing, Wang Yong, Wang Xiao-Lei, et al. Technique design and realization of the circumlunar return and reentry spacecraft of 3rd phase of Chinese Lunar exploration program. Scientia Sinica Technologica, 2015, 45(2): 111-123 doi: 10.1360/N092014-00484
[78]	叶培建, 杨孟飞, 彭兢, 李齐, 董彦芝, 张钊, 等. 中国深空探测进入/再入返回技术的发展现状和展望. 中国科学: 技术科学, 2015, 45(3): 229-238 doi: 10.1360/N092015-00049 Ye Pei-Jian, Yang Meng-Fei, Peng Jing, Li Qi, Dong Yan-Zhi, Zhang Zhao, et al. Review and prospect of atmospheric entry and earth reentry technology of China deep space exploration. Scientia Sinica Technologica, 2015, 45(3): 229-238 doi: 10.1360/N092015-00049
[79]	张柏楠, 杨庆, 杨雷, 马晓兵, 黄震. 我国新一代载人飞船及其研制进展. 科学通报, 2021, 66(32): 4065-4073 doi: 10.1360/TB-2021-0228 Zhang Bai-Nan, Yang Qing, Yang Lei, Ma Xiao-Bing, Huang Zhen. Progress on China’s new-generation manned spaceships. Chinese Science Bulletin, 2021, 66(32): 4065-4073 doi: 10.1360/TB-2021-0228
[80]	Li M M, Hu J, Huang H. A segmented and weighted adaptive predictor-corrector guidance method for the ascent phase of hypersonic vehicle. Aerospace Science and Technology, 2020, 106: Article No. 106231 doi: 10.1016/j.ast.2020.106231
[81]	Lu P. Predictor-corrector entry guidance for low-lifting vehicles. Journal of Guidance, Control, and Dynamics, 2008, 31(4): 1067-1075 doi: 10.2514/1.32055
[82]	Brunner C W, Lu P. Skip entry trajectory planning and guidance. Journal of Guidance, Control, and Dynamics, 2008, 31(5): 1210-1219 doi: 10.2514/1.35055
[83]	水尊师, 周军, 葛致磊. 基于高斯伪谱方法的再入飞行器预测校正制导方法研究. 宇航学报, 2011, 32(6): 1249-1255 doi: 10.3873/j.issn.1000-1328.2011.06.007 Shui Zun-Shi, Zhou Jun, Ge Zhi-Lei. On-line predictor-corrector reentry guidance law based on Gauss pseudospectral method. Journal of Astronautics, 2011, 32(6): 1249-1255 doi: 10.3873/j.issn.1000-1328.2011.06.007
[84]	张洪波, 曾亮. 一种跳跃式返回再入的预测-校正制导方法. 飞行器测控学报, 2014, 33(1): 82-87 Zhang Hong-Bo, Zeng Liang. A predictor-corrector guidance method for skip reentry missions. Journal of Spacecraft TT&C Technology, 2014, 33(1): 82-87
[85]	Zhang Z, Hu J. Prediction-based guidance algorithm for high-lift reentry vehicles. Science China Information Sciences, 2011, 54(3): 498-510 doi: 10.1007/s11432-011-4187-x
[86]	胡军, 吴宏鑫, 杨鸣, 张钊, 董文强, 杨俊春. 一种基于一阶特征模型的全系数自适应控制方法, 中国 104570734B, 2015-04 Hu Jun, Wu Hong-Xin, Yang Ming, Zhang Zhao, Dong Wen-Qiang, Yang Jun-Chun. All-coefficient Adaptive Control Method Based on One-order Characteristic Model, CN 104570734B, April 2015
[87]	胡军. 自适应预测制导: 一种统一的制导方法. 空间控制技术与应用, 2019, 45(4): 53-63 doi: 10.3969/j.issn.1674-1579.2019.04.007 Hu Jun. Adaptive predictive guidance: A unified guidance method. Aerospace Control and Application, 2019, 45(4): 53-63 doi: 10.3969/j.issn.1674-1579.2019.04.007
[88]	解永春, 陈长青, 刘涛, 王敏. 航天器交会对接制导导航控制原理和方法. 北京: 国防工业出版社, 2018. Xie Yong-Chun, Chen Chang-Qing, Liu Tao, Wang Min. Theory and Methods of Guidance, Navigation and Control for Spacecraft Rendezvous and Docking. Beijing: National Defense Industry Press, 2018.
[89]	解永春, 胡勇. 空间交会策略回顾及自主快速交会方案研究. 空间控制技术与应用, 2014, 40(4): 1-8 doi: 10.3969/j.issn.1674-1579.2014.04.001 Xie Yong-Chun, Hu Yong. Reviews of space rendezvous strategy and short rendezvous profile design for autonomous spacecraft. Aerospace Control and Application, 2014, 40(4): 1-8 doi: 10.3969/j.issn.1674-1579.2014.04.001
[90]	胡军, 解永春, 张昊, 于丹, 胡海霞, 张维瑾. 神舟八号飞船交会对接制导、导航与控制系统及其飞行结果评价. 空间控制技术与应用, 2011, 37(6): 1-5, 13 doi: 10.3969/j.issn.1674-1579.2011.06.001 Hu Jun, Xie Yong-Chun, Zhang Hao, Yu Dan, Hu Hai-Xia, Zhang Wei-Jin. Shenzhou-8 spacecraft guidance navigation and control system and flight result evaluation for rendezvous and docking. Aerospace Control and Application, 2011, 37(6): 1-5, 13 doi: 10.3969/j.issn.1674-1579.2011.06.001
[91]	杨震, 罗亚中, 张进. 近地快速交会调相策略设计与任务分析. 国防科技大学学报, 2015, 37(3): 61-67 doi: 10.11887/j.cn.201503011 Yang Zhen, Luo Ya-Zhong, Zhang Jin. Analysis and design of phasing strategy for near-earth short rendezvous mission. Journal of National University of Defense Technology, 2015, 37(3): 61-67 doi: 10.11887/j.cn.201503011
[92]	李萌, 龚胜平, 彭坤, 马晓兵. 直接优化算法在快速交会组合变轨策略中的应用. 载人航天, 2017, 23(2): 156-162 doi: 10.3969/j.issn.1674-5825.2017.02.003 Li Meng, Gong Sheng-Ping, Peng Kun, Ma Xiao-Bing. Application of direct optimization algorithmin synthetic orbit maneuver strategy of short rendezvous. Manned Spaceflight, 2017, 23(2): 156-162 doi: 10.3969/j.issn.1674-5825.2017.02.003
[93]	张强, 陈长青, 刘宗玉, 郝慧, 奚坤, 苏晏, 等. 天舟二号货运飞船全相位自主快速交会对接技术和在轨验证. 空间控制技术与应用, 2021, 47(5): 33-39 doi: 10.3969/j.issn.1674-1579.2021.05.005 Zhang Qiang, Chen Chang-Qing, Liu Zong-Yu, Hao Hui, Xi Kun, Su Yan, et al. All-phase autonomous quick rendezvous and docking technology and in-orbit verification of Tianzhou-2 cargo spacecraft. Aerospace Control and Application, 2021, 47(5): 33-39 doi: 10.3969/j.issn.1674-1579.2021.05.005
[94]	张昊, 解永春, 吴宏鑫. 交会对接光学成像敏感器光点布局求解有效性研究. 航天控制, 2008, 26(3): 44-48, 58 Zhang Hao, Xie Yong-Chun, Wu Hong-Xin. Research on the target pattern solution validity of optical imaging sensor used in RVD. Aerospace Control, 2008, 26(3): 44-48, 58
[95]	张昊, 石磊, 涂俊峰, 管乐鑫, 解永春. 基于交会对接CCD光学成像敏感器的双目测量算法. 空间控制技术与应用, 2011, 37(6): 66-71 doi: 10.3969/j.issn.1674-1579.2011.06.011 Zhang Hao, Shi Lei, Tu Jun-Feng, Guan Yue-Xin, Xie Yong-Chun. A CCD optical sensor based new binocular vision measurement algorithm for rendezvous and docking. Aerospace Control and Application, 2011, 37(6): 66-71 doi: 10.3969/j.issn.1674-1579.2011.06.011
[96]	王世新, 华宝成, 袁琦, 张良, 李明政, 赵春晖. 交会对接光学成像敏感器中合作目标的分析与设计. 空间控制技术与应用, 2020, 46(6): 56-62 Wang Shi-Xin, Hua Bao-Cheng, Yuan Qi, Zhang Liang, Li Ming-Zheng, Zhao Chun-Hui. Analysis and design of cooperative targets for camera-type rendezvous and docking sensor. Aerospace Control and Application, 2020, 46(6): 56-62
[97]	顾营迎, 王立, 华宝成, 刘达, 吴云, 徐云飞. 一种面向空间非合作目标位姿测量应用的三维点云滤波算法. 应用光学, 2019, 40(2): 210-216 Gu Ying-Ying, Wang Li, Hua Bao-Cheng, Liu Da, Wu Yun, Xu Yun-Fei. 3D point cloud filtering method for pose measurement application of space non-cooperative targets. Journal of Applied Optics, 2019, 40(2): 210-216
[98]	刘涛, 解永春. UKF稳定性研究及其在相对导航中的应用. 宇航学报, 2010, 31(3): 739-747 doi: 10.3873/j.issn.1000-1328.2010.03.019 Liu Tao, Xie Yong-Chun. Stability analysis of UKF and its application in relative navigation. Journal of Astronautics, 2010, 31(3): 739-747 doi: 10.3873/j.issn.1000-1328.2010.03.019
[99]	刘涛, 解永春. 一种自适应确定性采样滤波方法. 信息与控制, 2010, 39(6): 673-680 Liu Tao, Xie Yong-Chun. Adaptive deterministic sampling filter algorithm. Information and Control, 2010, 39(6): 673-680
[100]	刘涛, 解永春, 胡海霞. 粒子滤波及其在航天器交会对接相对导航中的应用. 空间控制技术与应用, 2011, 37(6): 19-27 doi: 10.3969/j.issn.1674-1579.2011.06.004 Liu Tao, Xie Yong-Chun, Hu Hai-Xia. Application of particle filtering in relative navigation filter design for spacecraft. Aerospace Control and Application, 2011, 37(6): 19-27 doi: 10.3969/j.issn.1674-1579.2011.06.004
[101]	Sharma S, D’Amico S. Neural network-based pose estimation for noncooperative spacecraft rendezvous. IEEE Transactions on Aerospace and Electronic Systems, 2020, 56(6): 4638-4658 doi: 10.1109/TAES.2020.2999148
[102]	Valada A, Mohan R, Burgard W. Self-supervised model adaptation for multimodal semantic segmentation. International Journal of Computer Vision, 2020, 128(5): 1239-1285 doi: 10.1007/s11263-019-01188-y
[103]	王颖, 解永春. 基于视线制导的空间交会停靠控制方法. 空间控制技术与应用, 2012, 38(2): 1-4, 23 doi: 10.3969/j.issn.1674-1579.2012.02.001 Wang Ying, Xie Yong-Chun. Rendezvous and berthing control method based on line of sight guidance. Aerospace Control and Application, 2012, 38(2): 1-4, 23 doi: 10.3969/j.issn.1674-1579.2012.02.001
[104]	陈志华, 解永春. 刚体卫星相平面控制闭环系统稳定性分析. 空间控制技术与应用, 2018, 44(1): 1-14, 29 doi: 10.3969/j.issn.1674-1579.2018.01.001 Chen Zhi-Hua, Xie Yong-Chun. Stability analysis of the closed-loop system of a phase-plane controlled rigid satellite. Aerospace Control and Application, 2018, 44(1): 1-14, 29 doi: 10.3969/j.issn.1674-1579.2018.01.001
[105]	胡勇, 徐李佳, 解永春. 针对失控翻滚目标航天器的交会对接控制. 字航学报, 2015, 36(1): 47-57 Hu Yong, Xu Li-Jia, Xie Yong-Chun. Control for rendezvous and docking with a tumbling target spacecraft. Journal of Astronautics, 2015, 36(1): 47-57
[106]	刘涛, 解永春, 王晓磊, 胡锦昌. 火星轨道交会自主导航与制导方法. 宇航学报, 2019, 40(4): 406-414 doi: 10.3873/j.issn.1000-1328.2019.04.005 Liu Tao, Xie Yong-Chun, Wang Xiao-Lei, Hu Jin-Chang. An autonomous rendezvous navigation and guidance method in mars orbit. Journal of Astronautics, 2019, 40(4): 406-414 doi: 10.3873/j.issn.1000-1328.2019.04.005
[107]	Zhao Z M, Liu Y W, Xie B, Zhai F, Yao F, Li L. Flight result and achievement of SJ-9 technology demonstration satellite. In: Proceedings of the 64th International Astronautical Congress. Beijing, China: 2013.
[108]	苟兴宇, 李克行, 张斌, 刘捷, 谭田, 董筠, 等. 实践九号编队飞行轨控中的姿轨耦合与推力损失研究. 空间控制技术与应用, 2013, 39(6): 1-5, 11 Gou Xing-Yu, Li Ke-Hang, Zhang Bin, Liu Jie, Tan Tian, Dong Jun, et al. On attitude and orbit coupling and thrust loss of SJ-9 formation flying orbit control. Aerospace Control and Application, 2013, 39(6): 1-5, 11
[109]	李克行, 苟兴宇, 张斌, 何英姿, 魏春岭, 白旭辉, 等. 一种星上相对运动状态获取方法, 中国 104765373A, 2015-07 Li Ke-Hang, Gou Xing-Yu, Zhang Bin, He Ying-Zi, Wei Chun-Ling, Bai Xu-Hui, et al. A Method for Obtaining Satellite Relative Motion State, CN 104765373A, July 2015
[110]	苟兴宇, 韩冬, 李克行, 张斌, 董筠, 赵键, 等. 一种航天器编队维持或绕飞撤离的控制方法, 中国 104317303A, 2015-01 Gou Xing-Yu, Han Dong, Li Ke-Hang, Zhang Bin, Dong Jun, Zhao Jian, et al. A Control Method for Spacecraft Formation Maintenance or Orbiting Evacuation, CN 104317303A, January 2015
[111]	陈统, 徐世杰, 李克行. 利用大气阻力的横向编队维持控制. 中国空间科学技术, 2008, 28(6): 8-13 doi: 10.3321/j.issn:1000-758X.2008.06.002 Chen Tong, Xu Shi-Jie, Li Ke-Hang. Control strategy using atmospheric drag for along-track formation maintenance. Chinese Space Science and Technology, 2008, 28(6): 8-13 doi: 10.3321/j.issn:1000-758X.2008.06.002
[112]	宋明轩, 邵晓巍, 刘付成, 王继河, 张德新. 基于差分气动力的J2项摄动下卫星编队构形重构研究. 航天控制, 2014, 32(4): 42-48, 61 doi: 10.3969/j.issn.1006-3242.2014.04.008 Song Ming-Xuan, Shao Xiao-Wei, Liu Fu-Cheng, Wang Ji-He, Zhang De-Xin. Research on satellite formation reconfiguration by using differential aerodynamic forces under J2 perturbation. Aerospace Control, 2014, 32(4): 42-48, 61 doi: 10.3969/j.issn.1006-3242.2014.04.008
[113]	范凡. 基于大气阻力微纳卫星编队轨道与姿态控制研究 [硕士论文], 国防科学技术大学, 中国, 2014 Fan Fan. The Micro Satellite Formation and Attitude Control Based on the Atmospheric Drag [Master thesis], University of Defense Technology, China, 2014
[114]	张亚博, 师鹏, 张皓, 赵育善. 电磁航天器编队悬停鲁棒协同控制方法. 北京航空航天大学学报, 2019, 45(2): 388-397 Zhang Ya-Bo, Shi Peng, Zhang Hao, Zhao Yu-Shan. A robust coordinated control method for hovering of electromagnetic spacecraft formation. Journal of Beijing University of Aeronautics and Astronautics, 2019, 45(2): 388-397
[115]	高策. 磁通钉扎作用的星间相对运动动力学与控制研究 [硕士论文], 国防科技大学, 中国, 2017 Gao Ce. Research on Dynamics and Control of Flux-pinned Spacecraft Relative Motion [Master thesis], University of Defense Technology, China, 2017
[116]	Scharf D P, Hadaegh F Y, Ploen S R. A survey of spacecraft formation flying guidance and control. Part II: Control. In: Proceedings of the American Control Conference. Boston, USA: IEEE, 2004. 2976−2985
[117]	Mesbahi M, Hadaegh F Y. Formation flying control of multiple spacecraft via graphs, matrix inequalities, and switching. Journal of Guidance, Control, and Dynamics, 2001, 24(2): 369-377 doi: 10.2514/2.4721
[118]	Ren W. Formation keeping and attitude alignment for multiple spacecraft through local interactions. Journal of Guidance, Control, and Dynamics, 2007, 30(2): 633-638 doi: 10.2514/1.25629
[119]	Ran D C, Chen X Q, Misra A K, Xiao B. Relative position coordinated control for spacecraft formation flying with communication delays. Acta Astronautica, 2017, 137: 302-311 doi: 10.1016/j.actaastro.2017.04.011
[120]	Lasserre E, Dufour F, Bernussou J, Brousse P, Lefebvre L. A linear programming solution to the homogeneous satellite constellation station keeping. In: Proceedings of the 48th International Astronautical Congress. Turin, Italy: 1997.
[121]	钱山, 李恒年, 张力军, 张智斌. 全球导航星座构型维持“死区”分析. 见: 第五届中国卫星导航学术年会论文集-S3 精密定轨与精密定位. 南京, 中国: 中国卫星导航学术年会组委会, 2014. Qian Shan, Li Heng-Nian, Zhang Li-Jun, Zhang Zhi-Bin. The station keeping dead-band budgets and analysis for GNSS constellation. In: Proceedings of the 5th China Satellite Navigation Conference-S3 Precise Orbit Determination and Positioning. Nanjing, China: Organizing Committee of China Satellite Navigation Academic Annual Meeting, 2014.
[122]	杨晓龙, 刘忠汉. 基于覆盖性能的Walker-\delta星座构型保持. 空间控制技术与应用, 2012, 38(2): 53-57 doi: 10.3969/j.issn.1674-1579.2012.02.011 Yang Xiao-Long, Liu Zhong-Han. Walker-\delta constellation configuration maintenance based on coverage performance. Aerospace Control and Application, 2012, 38(2): 53-57 doi: 10.3969/j.issn.1674-1579.2012.02.011
[123]	胡松杰, 申敬松, 郇佩. 基于参考轨道的Walker星座相对相位保持策略. 空间控制技术与应用, 2010, 36(5): 45-49 doi: 10.3969/j.issn.1674-1579.2010.05.009 Hu Song-Jie, Shen Jing-Song, Huan Pei. A relative phase-keeping strategy of Walker constellation based on reference orbit. Aerospace Control and Application, 2010, 36(5): 45-49 doi: 10.3969/j.issn.1674-1579.2010.05.009
[124]	姜宇, 李恒年, 宝音贺西. Walker星座摄动分析与保持控制策略. 空间控制技术与应用, 2013, 39(2): 36-41 doi: 10.3969/j.issn.1674-1579.2013.02.007 Jiang Yu, Li Heng-Nian, Baoyin He-Xi. On perturbation and orbital maintenance control strategy for Walker constellation. Aerospace Control and Application, 2013, 39(2): 36-41 doi: 10.3969/j.issn.1674-1579.2013.02.007
[125]	李恒年, 李济生, 焦文海. 全球星摄动运动及摄动补偿运控策略研究. 宇航学报, 2010, 31(7): 1756-1761 doi: 10.3873/j.issn.1000-1328.2010.07.009 Li Heng-Nian, Li Ji-Sheng, Jiao Wen-Hai. Analyzing perturbation motion and studying configuration maintenance strategy for Compass-M navigation constellation. Journal of Astronautics, 2010, 31(7): 1756-1761 doi: 10.3873/j.issn.1000-1328.2010.07.009
[126]	孙泽洲, 陈百超, 贾阳, 袁宝峰, 刘国强, 马静雅, 等. 天问一号火星巡视探测技术. 中国科学: 技术科学, 2022, 52(2): 214-225 doi: 10.1360/SST-2021-0487 Sun Ze-Zhou, Chen Bai-Chao, Jia Yang, Yuan Bao-Feng, Liu Guo-Qiang, Ma Jing-Ya, et al. The Tianwen-1 roving exploration technology for the Martian surface. Scientia Sinica Technologica, 2022, 52(2): 214-225 doi: 10.1360/SST-2021-0487
[127]	袁利, 黄煌. 空间飞行器智能自主控制技术现状与发展思考. 空间控制技术与应用, 2019, 45(4): 7-18 doi: 10.3969/j.issn.1674-1579.2019.04.002 Yuan Li, Huang Huang. Current trends of spacecraft intelligent autonomous control. Aerospace Control and Application, 2019, 45(4): 7-18 doi: 10.3969/j.issn.1674-1579.2019.04.002
[128]	袁利. 面向不确定环境的航天器智能自主控制技术. 宇航学报, 2021, 42(7): 839-849 doi: 10.3873/j.issn.1000-1328.2021.07.004 Yuan Li. Spacecraft intelligent autonomous control technology toward uncertain environment. Journal of Astronautics, 2021, 42(7): 839-849 doi: 10.3873/j.issn.1000-1328.2021.07.004
[129]	袁利, 姜甜甜. 航天器威胁规避智能自主控制技术研究综述. 自动化学报, DOI: 10.16383/j.aas.c211027 Yuan Li, Jiang Tian-Tian. Review on intelligent autonomous control for spacecraft confronting orbital threats. Acta Automatica Sinica, DOI: 10.16383/j.aas.c211027
[130]	李茂登, 黄翔宇, 郭敏文, 徐超, 魏春岭, 张晓文, 等. 一种递归多子样大动态惯性导航方法, 中国 111351483A, 2020-06 Li Mao-Deng, Huang Xiang-Yu, Guo Min-Wen, Xu Chao, Wei Chun-Ling, Zhang Xiao-Wen, et al. A Recursive Multi-sample Large Dynamic Inertial Navigation Method, CN 111351483A, June 2020
[131]	张洪华, 李骥, 轶峰, 黄翔宇. 嫦娥三号着陆器动力下降的自主导航. 控制理论与应用, 2014, 31(12): 1686-1694 关 doi: 10.7641/CTA.2014.40795 Zhang Hong-Hua, Li Ji, Guan Yi-Feng, Huang Xiang-Yu. Autonomous navigation for powered descent phase of Chang’E-3 lunar lander. Control Theory & Applications, 2014, 31(12), 1686-1694 doi: 10.7641/CTA.2014.40795
[132]	吴伟仁, 李骥, 黄翔宇, 张洪华, 王大轶, 张哲. 惯导/测距/测速相结合的安全软着陆自主导航方法. 宇航学报, 2015, 36(8): 893-899 Wu Wei-Ren, Li Ji, Huang Xiang-Yu, Zhang Hong-Hua, Wang Da-Yi, Zhang Zhe. INS/Rangefinder/Velocimetry based autonomous navigation method for safe landing. Journal of Astronautics, 2015, 36(8): 893-899
[133]	李茂登, 黄翔宇, 徐超, 郭敏文, 胡锦昌, 赵宇, 等. 天问一号火星探测器EDL过程自主导航技术. 宇航学报, 2022, 43(1): 11-20 doi: 10.3873/j.issn.1000-1328.2022.01.002 Li Mao-Deng, Huang Xiang-Yu, Xu Chao, Guo Min-Wen, Hu Jin-Chang, Zhao Yu, et al. Autonomous navigation technology of Tianwen-1 Mars probe during EDL process. Journal of Astronautics, 2022, 43(1): 11-20 doi: 10.3873/j.issn.1000-1328.2022.01.002
[134]	Li M D, Huang X Y, Wang D Y, Xu C, Guo M W, Hu J C, et al. Radar-updated inertial landing navigation with online initialization. IEEE Transactions on Aerospace and Electronic Systems, 2020, 56(5): 3360-3374 doi: 10.1109/TAES.2020.2987405
[135]	Li M D, Huang X Y, Xu C, Guo M W, Hu J C, Hao C, et al. Velocimeter-aided attitude estimation for Mars autonomous landing: Observability analysis and filter algorithms. IEEE Transactions on Aerospace and Electronic Systems, 2022, 58(1): 451-463 doi: 10.1109/TAES.2021.3103254
[136]	张洪华, 梁俊, 黄翔宇, 赵宇, 王立, 关轶峰, 等. 嫦娥三号自主避障软着陆控制技术. 中国科学: 技术科学, 2014, 44(6): 559-568 doi: 10.1360/092014-51 Zhang Hong-Hua, Liang Jun, Huang Xiang-Yu, Zhao Yu, Wang Li, Guan Yi-Feng, et al. Autonomous hazard avoidance control for Chang’E-3 soft landing. Scientia Sinica Technologica, 2014, 44(6): 559-568 doi: 10.1360/092014-51
[137]	张洪华, 关轶峰, 程铭, 李骥, 于萍, 张晓文, 等. 嫦娥四号着陆器制导导航与控制系统. 中国科学: 技术科学, 2019, 49(12): 1418-1428 Zhang Hong-Hua, Guan Yi-Feng, Cheng Ming, Li Ji, Yu Ping, Zhang Xiao-Wen, et al. Guidance navigation and control for Chang’E-4 lander. Scientia Sinica Technologica, 2019, 49(12): 1418-1428
[138]	Hu J C, Huang X Y, Li M D, Guo M W, Xu C, Zhao Y, et al. Entry vehicle control system design for the Tianwen-1 mission. Astrodynamics, 2022, 6(1): 27-37 doi: 10.1007/s42064-021-0124-y
[139]	张洪华, 关轶峰, 黄翔宇, 李骥, 赵宇, 于萍, 等. 嫦娥三号着陆器动力下降的制导导航与控制. 中国科学: 技术科学, 2014, 44(4): 377-384 doi: 10.1360/092014-43 Zhang Hong-Hua, Guan Yi-Feng, Huang Xiang-Yu, Li Ji, Zhao Yu, Yu Ping, et al. Guidance navigation and control for Chang’E-3 powered descent. Scientia Sinica Technologica, 2014, 44(4): 377-384 doi: 10.1360/092014-43
[140]	李骥, 张洪华, 张晓文, 关轶峰. 载人月球软着陆GNC技术研究. 载人航天, 2020, 26(6): 733-740, 750 doi: 10.3969/j.issn.1674-5825.2020.06.009 Li Ji, Zhang Hong-Hua, Zhang Xiao-Wen, Guan Yi-Feng. Research on GNC technology for crewed lunar soft landing. Manned Spaceflight, 2020, 26(6): 733-740, 750 doi: 10.3969/j.issn.1674-5825.2020.06.009
[141]	Zhang H H, Li J, Wang Z G, Guan Y F. Guidance navigation and control for Chang’E-5 powered descent. Space: Science & Technology, 2021, 2021: Article No. 9823609
[142]	Huang X Y, Li M D, Wang X L, Hu J C, Zhao Y, Guo M W, et al. The Tianwen-1 guidance, navigation, and control for Mars entry, descent, and landing. Space: Science & Technology, 2021, 2021: Article No. 9846185
[143]	Li J, Wang D Y. Autonomous positioning and orientating for Lunar launch. In: Proceedings of the 62nd International Astronautical Congress. Cape Town, South Africa: 2011. 5195−5202
[144]	张洪华, 李骥, 于萍, 关轶峰, 王磊, 王志文, 等. 嫦娥五号月面起飞上升制导导航与控制技术. 中国科学: 技术科学, 2021, 51(8): 921-937 doi: 10.1360/SST-2021-0102 Zhang Hong-Hua, Li Ji, Yu Ping, Guan Yi-Feng, Wang Lei, Wang Zhi-Wen, et al. Guidance navigation and control technology for the lunar ascent vehicle of the Chang’E-5 mission. Scientia Sinica Technologica, 2021, 51(8): 921-937 doi: 10.1360/SST-2021-0102
[145]	李骥, 张洪华, 关轶峰, 张晓文. 主发动机故障下的月面上升应急制导策略. 见: 深空探测技术专业委员会第十六届学术年会. 青岛, 中国: 2019. Li Ji, Zhang Hong-Hua, Guan Yi-Feng, Zhang Xiao-Wen. Emergency guidance strategy for lunar surface ascent under main engine failure. In: Proceedings of the 16th Committee of Deep Space Exploration Technology Annual Academic Conference. Qingdao, China: 2019.
[146]	杨孟飞, 贾阳, 陈建新. 月球巡视探测器系统研究. 空间控制技术与应用, 2008, 34(3): 3-6, 36 doi: 10.3969/j.issn.1674-1579.2008.03.001 Yang Meng-Fei, Jia Yang, Chen Jian-Xin. Research on system design of lunar rover. Aerospace Control and Application, 2008, 34(3): 3-6, 36 doi: 10.3969/j.issn.1674-1579.2008.03.001
[147]	邢琰, 魏春岭, 汤亮, 姜甜甜, 胡勇, 黄煌, 等. 地外巡视探测无人系统自主感知与操控技术发展综述. 空间控制技术与应用, 2021, 47(6): 1-8 doi: 10.3969/j.issn.1674-1579.2021.06.001 Xing Yan, Wei Chun-Ling, Tang Liang, Jiang Tian-Tian, Hu Yong, Huang Huang, et al. Development of autonomous sensing and control technology for extraterrestrial mobile exploration unmanned systems. Aerospace Control and Application, 2021, 47(6): 1-8 doi: 10.3969/j.issn.1674-1579.2021.06.001
[148]	陈建新, 邢琰, 李志平, 毛晓艳, 滕宝毅, 刘祥, 等. 祝融号火星车自主环境感知与避障技术. 中国科学: 技术科学, 2022, 52(8): 1186-1197 doi: 10.1360/SST-2022-0045 Chen Jian-Xin, Xing Yan, Li Zhi-Ping, Mao Xiao-Yan, Teng Bao-Yi, Liu Xiang, et al. Autonomous environment perception and obstacle avoidance technologies of Zhurong Mars rover. Scientia Sinica Technologica, 2022, 52(8): 1186-1197 doi: 10.1360/SST-2022-0045
[149]	陈建新, 邢琰, 滕宝毅, 毛晓艳, 刘祥, 贾永, 等. 嫦娥三号巡视器GNC及地面试验技术. 中国科学: 技术科学, 2014, 44(5): 461-469 doi: 10.1360/092014-48 Chen Jian-Xin, Xing Yan, Teng Bao-Yi, Mao Xiao-Yan, Liu Xiang, Jia Yong, et al. Guidance, navigation and control technologies of Chang’E-3 Lunar rover. Scientia Sinica Technologica, 2014, 44(5): 461-469 doi: 10.1360/092014-48
[150]	Ding L, Gao H B, Deng Z Q, Nagatani K, Yoshida K. Experimental study and analysis on driving wheels’ performance for planetary exploration rovers moving in deformable soil. Journal of Terramechanics, 2011, 48(1): 27-45 doi: 10.1016/j.jterra.2010.08.001
[151]	李楠, 高海波, 吕凤天, 丁亮, 刘振, 于海涛, 等. 车辙图像频域分析及星球车车轮滑转率估计方法. 宇航学报, 2016, 37(11): 1356-1364 doi: 10.3873/j.issn.1000-1328.2016.11.010 Li Nan, Gao Hai-Bo, Lv Feng-Tian, Ding Liang, Liu Zhen, Yu Hai-Tao, et al. Wheel trace imprint image frequency domain analysis and rover wheel slip ratio estimation. Journal of Astronautics, 2016, 37(11): 1356-1364 doi: 10.3873/j.issn.1000-1328.2016.11.010
[152]	Gonzalez R, Chandler S, Apostolopoulos D. Characterization of machine learning algorithms for slippage estimation in planetary exploration rovers. Journal of Terramechanics, 2019, 82: 23-34 doi: 10.1016/j.jterra.2018.12.001
[153]	Cunningham C, Nesnas I A, Whittaker W L. Improving slip prediction on Mars using thermal inertia measurements. Autonomous Robots, 2019, 43(2): 503-521 doi: 10.1007/s10514-018-9796-4
[154]	邢琰, 刘祥, 滕宝毅, 毛晓艳. 月球表面巡视探测自主局部避障规划. 控制理论与应用, 2019, 36(12): 2042-2046 Xing Yan, Liu Xiang, Teng Bao-Yi, Mao Xiao-Yan. Autonomous local obstacle avoidance path planning of Lunar surface exploration rovers. Control Theory & Applications, 2019, 36(12): 2042-2046
[155]	邢琰, 滕宝毅, 刘祥, 毛晓艳. 月球表面巡视探测GNC技术. 空间科学学报, 2016, 36(2): 196-201 doi: 10.11728/cjss2016.02.196 Xing Yan, Teng Bao-Yi, Liu Xiang, Mao Xiao-Yan. Guidance, navigation and control technology for Lunar surface exploration. Chinese Journal of Space Science, 2016, 36(2): 196-201 doi: 10.11728/cjss2016.02.196
[156]	董士伟, 侯欣宾, 王薪. 空间太阳能电站微波能量反向波束控制技术. 中国空间科学技术, 2022, 42(5): 91-102 doi: 10.16708/j.cnki.1000-758X.2022.0070 Dong Shi-Wei, Hou Xin-Bin, Wang Xin. Retro-directive microwave power beam steering technology for space solar power station. Chinese Space Science and Technology, 2022, 42(5): 91-102 doi: 10.16708/j.cnki.1000-758X.2022.0070
[157]	侯欣宾, 王立, 张兴华, 周璐. 多旋转关节空间太阳能电站概念方案设计. 宇航学报, 2015, 36(11): 1332-1338 doi: 10.3873/j.issn.1000-1328.2015.11.016 Hou Xin-Bin, Wang Li, Zhang Xing-Hua, Zhou Lu. Concept design on multi-rotary joints SPS. Journal of Astronautics, 2015, 36(11): 1332-1338 doi: 10.3873/j.issn.1000-1328.2015.11.016
[158]	Roulette J. OneWeb, SpaceX satellites dodged a potential collision in orbit [Online], available: https://www.theverge.com/2021/4/9/22374262/onewebspacex-satellites-dodged-potential-collision-orbit-spaceforce, August 17, 2022
[159]	European Space Policy Institute. Towards a European Approach to Space Traffic Management, ESPI Report 71, European Space Policy Institute, Austria, 2020
[160]	Araguz C, Bou-Balust E, Alarcón E. Applying autonomy to distributed satellite systems: Trends, challenges, and future prospects. Systems Engineering, 2018, 21(5): 401-416 doi: 10.1002/sys.21428
[161]	Vassev E, Sterritt R, Rouff C, Hinchey M. Swarm technology at NASA: Building resilient systems. IT Professional, 2012, 14(2): 36-42 doi: 10.1109/MITP.2012.18
[162]	Sterritt R, Rouff C A, Hinchey M G, Rash J L, Truszkowski W. Next generation system and software architectures: Challenges from future NASA exploration missions. Science of Computer Programming, 2006, 61(1): 48-57 doi: 10.1016/j.scico.2005.11.005
[163]	Agle D C. NASA will inspire world when it returns Mars samples to Earth in 2033 [Online], available: https://www.nasa.gov/press-release/nasa-will-inspire-world-when-it-returns-mars-samples-to-earth-in-2033, October 8, 2022
[164]	李林峰, 解永春. 空间机器人操作: 一种多任务学习视角. 中国空间科学技术, 2022, 42(3): 10-24 Li Lin-Feng, Xie Yong-Chun. Space robotic manipulation: A multi-task learning perspective. Chinese Space Science and Technology, 2022, 42(3): 10-24