[1] | 曹登庆, 白坤朝, 丁虎 等. 大型柔性航天器动力学与振动控制研究进展. 力学学报, 2019,51(1):1-13 | [1] | ( Cao Dengqing, Bai kunchao, Ding Hu, et al. Advances in dynamics and vibration control of large-scale flexible spacecraft. Chinese Journal of Theoretical and Applied Mechanics, 2019,51(1):1-13 (in Chinese)) | [2] | 柳森, 党雷宁, 赵君尧 等. 小行星撞击地球的超高速问题. 力学学报, 2018,50(6):1311-1327 | [2] | ( Liu Sen, Dang Leining, Zhao Junyao, et al. Hypervelocity issues of earth impact by asteroids. Chinese Journal of Theoretical and Applied Mechanics, 2018,50(6):1311-1327 (in Chinese)) | [3] | 王恩美, 邬树楠, 吴志刚. 在轨组装空间结构面向主动控制的动力学建模. 力学学报, 2020,52(3):805-816 | [3] | ( Wang Enmei, Wu Shunan, Wu Zhigang. Active-control-oriented dynamic modelling for on-orbit assembly space structure. Chinese Journal of Theoretical and Applied Mechanics, 2020,52(3):805-816 (in Chinese)) | [4] | Hughes SP, Mailhe LM, Guzman JJ. A comparison of trajectory optimization methods for the impulsive minimum propellant rendezvous problem. Advances in the Astronautical Sciences, 2003,13:85-104 | [5] | 郗小宁, 王威, 高玉东 等. 近地航天器轨道基础. 长沙: 国防科技大学出版社, 2003,105 | [5] | ( Xi Xiaoning, Wang Wei, Gao Yudong, et al. Fundamentals of Near-Earth Spacecraft Orbit. Changsha: National University of Defense Technology Press, 2003,105(in Chinese)) | [6] | 李皓皓, 张进, 罗亚中. 基于机动目标滤波估计的航天器主动规避策略. 力学学报, 2020,52(6) | [6] | ( Li Haohao, Zhang Jin, Luo Yazhong. Spacecraft evasion strategy using active maneuvers based on maneuvering target acceleration estimation. Chinese Journal of Theoretical and Applied Mechanics, 2020,52(6) (in Chinese)) | [7] | 范红旗, 王胜, 付强. 目标机动检测算法综述. 系统工程与电子技术, 2009,31(5):1064-1070 | [7] | ( Fan Honqi, Wang Sheng, Fu Qiang. Survey of algorithms of target maneuver detection. Systems Engineering and Electronics, 2009,31(5):1064-1070 (in Chinese)) | [8] | 汪雄良, 周海银, 朱炬波. 三状态样条滤波与平滑. 数学理论与应用, 2002(1):109-112 | [8] | ( Wang Xiongliang, Zhou Haiyin, Zhu Jubo. Three-state spline filter and smooth method. Mathematical Theory and Applications, 2002(1):109-112 (in Chinese)) | [9] | 徐国亮, 邓雅娟. 机动目标建模及机动检测算法. 情报指挥控制系统与仿真技术, 2005,27(4):81-83 | [9] | ( Xu Guoliang, Deng Yajuan. Mathematical models for maneuvering target tracking and maneuver detection algorithms. Information Command Control System & Simulation Technology, 2005,27(4):81-83 (in Chinese)) | [10] | 李元凯, 敬忠良, 胡士强. 基于瞬态相对模型的轨道机动目标运动参数估计. 控制与决策, 2009,24(7):1059-1064 | [10] | ( Li Yuankai, Jing Zhongliang, Hu Shiqiang. Transient relativemodel based kinematical parameter estimation for orbital maneuvering target. Control and Decision, 2009,24(7):1059-1064 (in Chinese)) | [11] | 梁彦刚, 王伟林. 在轨服务航天器任务指派问题. 国防科技大学学报, 2013,35(5):26-30 | [11] | ( Liang Yangang, Wang Weilin. Research on mission assignment of on-orbit servicing spacecraft. Journal of National University of Defense Technology, 2013,35(5):26-30 (in Chinese)) | [12] | Curtis HD. Orbital Mechanics for Engineering Students. Burlington: Elsevier Ltd, 2010 | [13] | 武凌斯. 有翼导弹引论. 北京: 国防工业出版社, 1979 | [13] | ( Wu Lingsi. Introduction to Winged Missiles. Beijing: National Defense Industry Press, 1979 (in Chinese)) | [14] | Beckner FL. Regions Accessible to A Ballistic Weapon. Austin, TX: University of Texas at Austin | [15] | Battin RH. An introduction to the mathematics and methods of astrodynamics. rev. Reston, VA: AIAA, 1999 | [16] | Vinh NX, Lu P, Howe RM, et al. Optimal interception with time constraint. Journal of Optimization Theory and Applications, 1990,66(3):361-390 | [17] | Vinh NX, Gilbert EG, Howe RM, et al. Reachable domain for interception at hyperbolic speeds. Acta Astronautica, 1995,35(1):1-8 | [18] | 陈茂良, 周军, 常燕. 空间拦截攻击区和威胁区仿真研究. 航天控制, 2009,27(1):41-44 | [18] | ( Chen Maoliang, Zhou Jun, Chang Yan. Simulation study of attacking area and threatening area for space interception. Aerospace Control, 2009,27(1):41-44 (in Chinese)) | [19] | 常燕, 周军. 空间飞行器追踪区设计. 宇航学报, 2006,27(6):1228-1231 | [19] | ( Chang Yan, Zhou Jun. Tracing area design for spacecraft. Journal of Astronautics, 2006,27(6):1228-1231 (in Chinese)) | [20] | 徐加瑞, 陈勇. 轨道机动的追踪区与机遇区仿真分析. 系统仿真技术及其应用学术会议论文集. 北京: 中国系统仿真学会, 2009 | [20] | ( Xu Jiarui, Chen yong. Simulation analysis of tracking area and opportune area of the orbital maneuvering. System Simulation Technology & Application. Beijing: Chinese Society for System Simulation, 2009 (in Chinese)) | [21] | 雪丹, 李俊峰. 平面脉冲作用下卫星轨道的可达范围研究. 宇航学报, 2009,30(1):88-92 | [21] | ( Xue Dan, Li Junfeng. Study on reachable domain for satellite trajectory with coplanar impulse applied. Journal of Astronautics, 2009,30(1):88-92 (in Chinese)) | [22] | 雪丹, 李俊峰. 确定卫星可达范围的优化方法. 清华大学学报: 自然科学版, 2009(11):1852-1855 | [22] | ( Xue Dan, Li Junfeng. Optimization of the reachable domain of a satellite. Journal of Tsinghua University: Science & Technology, 2009(11):1852-1855 (in Chinese)) | [23] | 雪丹, 李俊峰, 蒋方华. 卫星在轨道平面内的可达范围研究. 力学学报, 2010,42(2):337-342 | [23] | ( Xue Dan, Li Junfeng, Jiang Fanghua. Reachable domain of a satellite with a coplanar impulse applied. Chinese Journal of Theoretical and Applied Mechanics, 2010,42(2):337-342 (in Chinese)) | [24] | Xue D, Li J, Baoyin H, et al. Reachable domain for spacecraft with a single impulse. Journal of Guidance, Control, and Dynamics, 2010,33(3):934-942 | [25] | 温昶煊. 面向空间态势感知的可达范围理论和应用研究. [博士论文]. 北京: 北京航空航天大学, 2015 | [25] | ( Wen Changxuan. Space situational awareness oriented research on theory and application of reachable domain. [PhD Thesis]. Beijing: Beijing University of Aeronautics and Astronautics, 2015 (in Chinese)) | [26] | Wen C, Zhao Y, Shi P. Precise determination of reachable domain for spacecraft with single impulse. Journal of Guidance,Control, and Dynamics, 2014,37(6):1767-1779 | [27] | Wen C, Zhao Y, Shi P, Hao Z, Orbital accessibility problem for spacecraft with a single impulse. Journal of Guidance,Control, and Dynamics, 2014,37(4):1260-1271 | [28] | Wen C, Peng C, Gao Y, Reachable domain for spacecraft with ellipsoidal Delta-V distribution. Astrodynamics, 2018,2(3):265-288 | [29] | Chen Q, Qiao D, Shang HB, et al. A new method for solving reachable domain of spacecraft with a single impulse. Acta Astronautica, 2018,145:153-164 | [30] | 张洪波. 航天器轨道力学理论与方法. 北京: 国防工业出版社, 2015 | [30] | ( Zhang Hongbo. Theories and Methods of Spacecraft Orbital Mechanics. Beijing: National Defense Industry Press, 2015 (in Chinese)) |
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