2.845

2023影响因子

(CJCR)

  • 中文核心
  • EI
  • 中国科技核心
  • Scopus
  • CSCD
  • 英国科学文摘

留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

空间控制技术发展与展望

袁利 姜甜甜 魏春岭 杨孟飞

袁利, 姜甜甜, 魏春岭, 杨孟飞. 空间控制技术发展与展望. 自动化学报, 2023, 49(3): 476−493 doi: 10.16383/j.aas.c220792
引用本文: 袁利, 姜甜甜, 魏春岭, 杨孟飞. 空间控制技术发展与展望. 自动化学报, 2023, 49(3): 476−493 doi: 10.16383/j.aas.c220792
Yuan Li, Jiang Tian-Tian, Wei Chun-Ling, Yang Meng-Fei. Advances and perspectives of space control technology. Acta Automatica Sinica, 2023, 49(3): 476−493 doi: 10.16383/j.aas.c220792
Citation: Yuan Li, Jiang Tian-Tian, Wei Chun-Ling, Yang Meng-Fei. Advances and perspectives of space control technology. Acta Automatica Sinica, 2023, 49(3): 476−493 doi: 10.16383/j.aas.c220792

空间控制技术发展与展望

doi: 10.16383/j.aas.c220792
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

Advances and Perspectives of Space Control Technology

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: 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.
  • 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

  • [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
  • 加载中
图(1)
计量
  • 文章访问数:  5010
  • HTML全文浏览量:  670
  • PDF下载量:  710
  • 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

目录

    /

    返回文章
    返回