荆武兴

期刊论文

1. 高佳伟，胡玉东，荆武兴，高长生（2026）. 考虑碰撞角约束的拦截弹运动伪装末制导律. 《宇航学报》.
2. Yudong Hu, Zehang Qu, Fei Wang, Zichu Liu, Junbo Hu, Changsheng Gao, Wuxing Jing (2026). A Trajectory Prediction Method Based on Parametric Modeling of Trajectory Curve Evolution Patterns. Advances in Astronautics.DOI
3. Yong Hu, Zhehao Wang, Changsheng Gao, Wuxing Jing, Junbo Hu (2026). An Online Trajectory‐Planning Guidance Method for Reentry Vehicles With Bézier Curve–Based Shaping Approach. International Journal of Aerospace Engineering.DOI
4. Xinru Liang, Changsheng Gao, Wuxing Jing, Ruoming An (2025). A robust adaptive filtering algorithm for high-maneuvering hypersonic vehicles. Journal Of Systems Engineering And Electronics, Vol. 36, No. 5.DOI
5. 杜青峰，孟庆展，胡玉东，荆武兴，高长生（2025）. 变质心飞行器双速率前馈-反馈组合姿态控制. 《宇航学报》.
6. 安若铭，荆武兴，高长生，胡玉东，杜青峰（2025）. 飞行器轨迹规划及姿态演示实验设计. 《中国现代教育装备》.
7. 王凯，胡玉东，高长生，荆武兴（2025）. 基于多尺度模型的异构信息融合跟踪算法. 《电光与控制》.
8. Kun-Lin Cheng, Jiahui Li, Zekuan Liu, Wente Pan, Jiang Qin, Wuxing Jing (2025). A novel solar-powered closed-Brayton-cycle and thermoelectric generator integrated energy system with thermal storage for lunar base: Modeling and analysis. Energy.DOI
9. Jiahui Li, Kun-Lin Cheng, Fangyan Jiang, Qi Xiao, Zhenhai Zou, Jiang Qin, Wuxing Jing (2025). Novel nuclear power and chemical energy hybrid propulsion system with fuel precooling: Scheme comparison and performance evaluation. International journal of hydrogen energy.DOI
10. PENG SUI, Yudong Hu, Changsheng Gao, Wuxing Jing, Jie Sun (2025). Dynamic Analysis and Slider Vibration Control of a Moving-Mass High-Speed Cruise Vehicle. IEEE Transactions on Aerospace and Electronic Systems.DOI
11. Hongyan Zang, Yudong Hu, Changsheng Gao, Wuxing Jing (2025). Trajectory Prediction Algorithm of Missile Based on Physics-Augmented Deep Learning. IEEE Transactions on Aerospace and Electronic Systems.DOI
12. Zichu Liu, Yudong Hu, Changsheng Gao, Wuxing Jing, Qingzhan Meng (2025). Probabilistic trajectory prediction for reentry glider vehicles using koopman operators under uncertainty. Aerospace Science and Technology.DOI
13. Xinru Liang, Changsheng Gao, Wuxing Jing (2025). Trajectory prediction algorithm based on maneuver analysis for hypersonic glide vehicles in a deep neural network. Astrodynamics.DOI
14. Xinru Liang, Changsheng Gao, Wuxing Jing (2025). A student-t mixture filtering algorithm based on adaptive parametric model. Digital Signal Processing.DOI
15. Hongyan Zang, Lili Liu, Yudong Hu, Changsheng Gao, Wuxing Jing (2025). Trajectory tracking algorithm of ballistic missile in the ascent phase based on deep learning. Aerospace Science and Technology.DOI
16. Hongyan Zang, Changsheng Gao, Yudong Hu, Wuxing Jing (2025). Trajectory prediction algorithm of ballistic missile driven by data and knowledge. Defence Technology.DOI
17. Wenxue Chen, Yingjing Qian, Changsheng Gao, Wuxing Jing (2025). Line-of-Sight Triangle-Based Prescribed-Time Guidance Law for 3-Player with Second-Order Lag Dynamics. Space Science & Technology.DOI
18. Zichu Liu, Yudong Hu, Changsheng Gao, Wuxing Jing (2025). Data-Driven Online Modeling and Tracking of Hypersonic Glide Vehicles. IFAC-PapersOnLine.DOI
19. Peng Sui, Changsheng Gao, Wuxing Jing, Jie Sun (2025). Rigid-Flexible Coupling Dynamic Modeling and Characteristics Analysis of Thin-Film Spacecraft. IFAC-PapersOnLine.DOI
20. Hanyu Ni, Qingfeng Du, Changsheng Gao, Wuxing Jing, Sui Peng (2025). The Degree Of Controllability Analysis and Calculation of Large Moving-Mass vehicles. IFAC-PapersOnLine.DOI
21. Zhijie Zhang, Qingfeng Du, Hanyu Ni, Wuxing Jing, Changsheng Gao, Sui Peng (2025). Analysis of evader escape strategy for 3D nonlinear model. IFAC-PapersOnLine.DOI
22. Xudong Ji, Zhe Chen, Zichu Liu, Changsheng Gao, Wuxing Jing (2025). Hypersonic vehicle trajectory tracking based on moving horizon estimation. IFAC-PapersOnLine.DOI
23. Jiaming Ye, Yudong Hu, Wuxing Jing, Changsheng Gao (2025). Rapid Trajectory Planning for Launch Vehicle Based on Deep Neural Network and Particle Swarm Differential Evolution Optimization. IFAC-PapersOnLine.DOI
24. 陈文雪，胡玉东，高长生，荆武兴，安若铭（2024）. 拦截高超声速滑翔飞行器：制导进展与展望. 《宇航学报》.
25. 孙佳慧，胡玉东，高长生，荆武兴（2024）. 大质量比滚控式变质心飞行器动力学特性分析. 《宇航学报》.
26. 杜青峰，荆武兴，高长生，安若铭（2024）. 考虑滑块动态特性的变质心四旋翼无人机双回路控制. 《北京航空航天大学学报》.
27. 臧红岩，王凯，高长生，荆武兴，王越欣（2024）. 基于滚动时域估计的高超声速飞行器轨迹跟踪. 《现代防御技术》.
28. 安若铭，荆武兴，高长生，胡玉东（2024）. 飞行器虚拟实验平台开发及其在教学中的应用. 《科技创新与应用》.
29. Kun-Lin Cheng, Jiahui Li, Fangyan Jiang, Qi Xiao, Zhenhai Zou, Jiang Qin, Wuxing Jing (2024). Novel Nuclear Power and Fossil Fuel Hybrid Propulsion Systems for Long-Endurance Unmanned Aerial Vehicles: Configuration Comparison and Performance Optimization. Energy.DOI
30. Kun-Lin Cheng, Jianchi Yu, Chaolei Dang, Jiang Qin, Wuxing Jing (2024). Performance comparison between closed-Brayton-cycle power generation systems using supercritical carbon dioxide and helium–xenon mixture at ultra-high turbine inlet temperatures on hypersonic vehicles. Energy.DOI
31. Yi-Lin Wang, Kun-Lin Cheng, Jing Xu, Wuxing Jing, Hongyan Huang, Jiang Qin (2024). Thermodynamic and mass analysis of a novel two-phase liquid metal MHD enhanced energy conversion system for space nuclear power source. Energy.DOI
32. Yi-Lin Wang, Kun-Lin Cheng, Jing Xu, Wuxing Jing, Hongyan Huang, Jiang Qin (2024). Novel onboard High-Power electricity generation system of Closed-Brayton-Cycle enhanced by Multi-Stage LMMHD Generators: Coupling analysis with propulsion system. Applied Thermal Engineering.DOI
33. Zichu Liu, Yudong Hu, Changsheng Gao, Wuxing Jing, Xudong Ji (2024). Modeling and analysis of maneuver laws based on higher order multi-resolution dynamic mode decomposition for hypersonic glide vehicles. Defence Technology.DOI
34. Yudong Hu, Zichu Liu, Chunwang Jiang, Wuxing Jing, Changsheng Gao (2024). Maneuver mode parametric modeling based on trajectory curve evolution laws for hypersonic glide vehicles. Aerospace Science and Technology.DOI
35. Qingfeng Du, Yudong Hu, Wuxing Jing, Changsheng Gao (2024). Three-dimensional target evasion strategy without missile guidance information. Aerospace Science and Technology.DOI
36. Qingfeng Du, Yudong Hu, Wuxing Jing, Changsheng Gao (2024). Dynamics and Moving-Mass Parameter Design of Single Moving-Mass Roll and Trim Control Hypersonic Vehicle. IEEE Transactions on Aerospace and Electronic Systems.DOI
37. Xinru Liang, Changsheng Gao, Wuxing Jing, Ruoming An (2024). Iterated rational quadratic kernel - High-order unscented Kalman filtering algorithm for spacecraft tracking. Defence Technology.DOI
38. Wenxue Chen, Yudong Hu, Changsheng Gao, Wuxing Jing (2024). Luring cooperative capture guidance strategy for the pursuit—evasion game under incomplete target information. Astrodynamics.DOI
39. Yue Liu, Yongqiang Zhang, Xiangzhen Hou, Yanchao He, Xi Cai, Minghu Li, Yingjing Qian, Wuxing Jing (2024). Optimization of the Low Earth Orbit Constellation Deployment Strategy Considering the Launching Schedule Constraints. 《第43届中国控制会议论文集（4）》.DOI
40. Sui Peng, Yongjun Shen, Changsheng Gao, Wuxing Jing (2024). Mechanical mechanism and parameter optimization of a tuned inerter damper with delayed fractional-order PID. Nonlinear Dynamics.DOI
41. Wenxue Chen, Changsheng Gao, Wuxing Jing (2024). Three-Dimensional Distributed Cooperative Guidance via Motion Camouflage Theory Against Hypersonic Vehicles With Speed Advantages. IEEE Transactions on Aerospace and Electronic Systems.DOI
42. Jiahui Sun, Wuxing Jing, Jie Chen (2024). Robust Soft-Switching Multiple Model Predictive Control for Moving-Mass Reentry Vehicle. Journal of Guidance Control and Dynamics.DOI
43. Guanghui Cheng, Wuxing Jing, Changsheng Gao (2024). Calculate the ignition height of the vertical landing phase online for the reusable rocket. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
44. Kun Mao, Wuxing Jing, Fei Xue, Kai Chen, Yong Lu, Yingli Su, Meihong Zhang (2024). Applicability Research and Improvement of Modal Method in CFD/CSD Coupling Static Aeroelastic Analysis. Lecture notes in electrical engineering.DOI
45. 梁新茹，高长生，荆武兴（2023）. 高超声速飞行器自适应鲁棒跟踪滤波算法. 《宇航学报》.
46. 谭一廷，荆武兴，高长生，安若铭（2023）. 高超声速机动目标拦截多约束解析捕获区. 《航空学报》.
47. 陈文雪，高长生，荆武兴（2023）. 拦截机动目标的信赖域策略优化制导算法. 《航空学报》.
48. Kun-Lin Cheng, Jiahui Li, Jianchi Yu, Jiang Qin, Wuxing Jing (2023). Dynamic Characteristics Analysis for a Novel Double-Rotor He-Xe Closed-Brayton-Cycle Space Nuclear Power Generation System. Energies.DOI
49. Kun Mao, Wuxing Jing, Mei-Hong Zhang, Huining Zhang (2023). An Aerodynamic Correction Technique for the Unsteady Subsonic Wing–Body Interference Model. Aerospace.DOI
50. Kun-Lin Cheng, Jiahui Li, Jianchi Yu, Chuanjie Fu, Jiang Qin, Wuxing Jing (2023). Novel thermoelectric generator enhanced supercritical carbon dioxide closed-Brayton-cycle power generation systems: Performance comparison and configuration optimization. Energy.DOI
51. Yi-Lin Wang, Kun-Lin Cheng, Jing Xu, Wuxing Jing, Hongyan Huang, Jiang Qin (2023). A Rapid Performance Prediction Method for Two-Phase Liquid Metal MHD Generators Based on Quasi-One-Dimensional Model. Thermal Science and Engineering Progress.DOI
52. Kun-Lin Cheng, Wuxing Jing, Jiahui Li, Jiang Qin (2023). Performance Assessment of Closed-Brayton-Cycle and Thermoelectric Generator Combined Power Generation System Coupled with Hydrocarbon-Fueled Scramjet. Energies.DOI
53. Hongyan Zang, Changsheng Gao, Wuxing Jing (2023). Tracking Control of Combined Power Aerospace Vehicle in Climbing Phase. Lecture notes in mechanical engineering.DOI
54. Guanghui Cheng, Yudong Hu, Wuxing Jing, Chang Gao, Ruoming An (2023). Parameters Designing of the Sliding Mode Control for the Reusable Launch Vehicle Based on Deep Reinforcement Learning and Evolution Strategy. China Automation Congress (CAC).DOI
55. Guanghui Cheng, Yudong Hu, Wuxing Jing, Ruoming An, Changsheng Gao (2023). Trajectory Correction of the Rocket for Aerodynamic Load Shedding Based on Deep Neural Network and the Chaotic Evolution Strategy With Covariance Matrix Adaptation. IEEE Transactions on Aerospace and Electronic Systems.DOI
56. Wenxue Chen, Yudong Hu, Changsheng Gao, Wuxing Jing (2023). Three-dimensional trajectory tracking guidance against near-space maneuvering targets with multiple constraints under wind field. Control Engineering Practice.DOI
57. Xin-ru Liang, Yudong Hu, Changsheng Gao, Wuxing Jing (2023). A robust variational Bayesian Student-t CKF algorithm for hypersonic vehicle tracking. 《第42届中国控制会议论文集（6）》.DOI
58. Xiaoqi Qiu, Peng Lai, Changsheng Gao, Wuxing Jing (2023). Recorded recurrent deep reinforcement learning guidance laws for intercepting endoatmospheric maneuvering missiles. Defence Technology.DOI
59. Yidi Fan, Wuxing Jing, Franco Bernelli Zazzera (2023). Nonlinear Tracking Differentiator Based Prescribed Performance Control for Space Manipulator. International Journal of Control Automation and Systems.DOI
60. Kun Mao, Wuxing Jing, Pan Cheng, Xiaoyan Liu, Yuchen Sun, Meihong Zhang (2023). A Modification to the Enhanced Correction Factor Technique for the Subsonic Wing–Body Interference Model. Aerospace.DOI
61. 邱潇颀，高长生，荆武兴（2022）. 变质心固定翼无人机动力学分析与抗扰控制. 《北京航空航天大学学报》.
62. 程光辉，荆武兴，许元男，叶家铭（2022）. 基于粒子群优化算法的高空风弹道修正技术. 《导弹与航天运载技术(中英文)》.
63. 臧红岩，高长生，荆武兴（2022）. 机动发射弹道导弹集群诸元快速规划. 《宇航学报》.
64. 邱潇颀，高长生，荆武兴（2022）. 拦截大气层内机动目标的深度强化学习制导律. 《宇航学报》.
65. 王恒，荆武兴，杨源，郭建文，王岩（2022）. 基于自适应滑模变结构控制的临近空间拦截器末制导律设计. 《空天技术》.
66. Wenxue Chen, Changsheng Gao, Wuxing Jing (2022). Proximal policy optimization guidance algorithm for intercepting near-space maneuvering targets. Aerospace Science and Technology.DOI
67. Zhitao Liu, Jianqing Li, Huan Zhou, Changsheng Gao, Wuxing Jing (2022). Adaptive coupled attitude-servo control for moving mass flight vehicles with high-mass-ratio. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
68. Peng Cui, Changsheng Gao, Wuxing Jing, Ruoming An (2022). Fault-Tolerant Control of Hypersonic Vehicle Using Neural Network and Sliding Mode. International Journal of Aerospace Engineering.DOI
69. Yiting Tan, Wuxing Jing, Changsheng Gao, Ruoming An (2022). Adaptive improved super-twisting integral sliding mode guidance law against maneuvering target with terminal angle constraint. Aerospace Science and Technology.DOI
70. Xiaoqi Qiu, Changsheng Gao, Wuxing Jing (2022). Maneuvering penetration strategies of ballistic missiles based on deep reinforcement learning. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
71. Yudong Hu, Changsheng Gao, Wuxing Jing (2022). Joint State and Parameter Estimation for Hypersonic Glide Vehicles Based on Moving Horizon Estimation via Carleman Linearization. Aerospace.DOI
72. Jiahui Sun, Wuxing Jing, Changsheng Gao, Tong Wu (2022). Attitude dynamics and control of high-mass-ratio fixed-trim moving mass reentry vehicle. Aerospace Science and Technology.DOI
73. Yiting Tan, Wuxing Jing, Changsheng Gao (2022). Uncertain trajectory planning integrating polynomial chaos and convex programming. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
74. 高峰，荆武兴，高长生，李志刚，钟伟（2021）. 经济型月球探测器精确定点软着陆制导算法. 《宇航学报》.
75. 荆武兴，杨彪，高长生（2021）. 空基反助推段导弹制导技术综述. 《哈尔滨工业大学学报》.
76. 谭一廷，荆武兴，高长生（2021）. 考虑零控交班视窗角约束的拦截中制导设计. 《宇航学报》.
77. 安若铭，邢坤鹏，荆武兴（2021）. 卫星单轴姿态控制全物理仿真平台动态测试系统设计. 《中国现代教育装备》.DOI
78. 王克帆，邱潇颀，高长生，荆武兴（2021）. 临近空间太阳能无人机横航向变质心控制技术. 《空天防御》.
79. 钱首元，高长生，荆武兴（2021）. 单滑块与飞轮协同姿态控制卫星运动分析. 《上海航天(中英文)》.DOI
80. 高长生，王越欣，荆武兴，胡玉东（2021）. 一种高超声速飞行器在线反馈滤波算法. 《现代防御技术》.
81. Xiaoqi Qiu, Changsheng Gao, Kefan Wang, Wuxing Jing (2021). Attitude Control of a Moving Mass–Actuated UAV Based on Deep Reinforcement Learning. Journal of Aerospace Engineering.DOI
82. Feng Gao, Wei Zhong, Zhigang Li, Wuxing Jing, Changsheng Gao (2021). A Pose Synchronization Control Method for the Approach Phase of Lunar Lander. China Automation Congress (CAC).DOI
83. Yudong Hu, Changsheng Gao, Junlong Li, Wuxing Jing (2021). Maneuver mode analysis and parametric modeling for hypersonic glide vehicles. Aerospace Science and Technology.DOI
84. Biao Yang, Wuxing Jing, Changsheng Gao (2021). Online midcourse guidance method for boost phase interception via adaptive convex programming. Aerospace Science and Technology.DOI
85. Yidi Fan, Wuxing Jing, Changsheng Gao, Franco Bernelli Zazzera (2021). Immersion and Invariance-Based Adaptive Coordinate Control for Space Manipulator. IEEE International Conference on Control Science and Systems Engineering (ICCSSE).DOI
86. Guanghui Cheng, Wuxing Jing, Changsheng Gao (2021). Recovery trajectory planning for the reusable launch vehicle. Aerospace Science and Technology.DOI
87. Yudong Hu, Changsheng Gao, Junlong Li, Wuxing Jing, Zhen Li (2021). Novel trajectory prediction algorithms for hypersonic gliding vehicles based on maneuver mode on-line identification and intent inference. Measurement Science and Technology.DOI
88. Yudong Hu, Changsheng Gao, Junlong Li, Wuxing Jing, Wenxue Chen (2021). A novel adaptive lateral reentry guidance algorithm with complex distributed no-fly zones constraints. Chinese Journal of Aeronautics.DOI
89. Yidi Fan, Wuxing Jing (2021). Inertia-free appointed-time prescribed performance tracking control for space manipulator. Aerospace Science and Technology.DOI
90. Zhitao Liu, Changsheng Gao, Wuxing Jing (2021). Dynamic analysis and coupling control of underactuated flight vehicles with single moving mass. Aerospace Science and Technology.DOI
91. Zhitao Liu, Jianqing Li, Changsheng Gao, Wuxing Jing (2021). Bifurcation analysis for a novel flight vehicle with pitch-control single moving mass. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
92. Xiaoqi Qiu, Mingen Zhang, Wuxing Jing, Changsheng Gao (2021). Dynamics and Adaptive Sliding Mode Control of a Mass-Actuated Fixed-Wing UAV. International Journal of Aeronautical and Space Sciences.DOI
93. Yang Biao, Jing Wuxing, Gao Changsheng (2020). Three-dimensional cooperative guidance law for multiple missiles with impact angle constraint. Journal Of Systems Engineering And Electronics, Vol. 310, No. 60.DOI
94. Zheng Xu, Gao Yejun, Jing Wuxing, Wang Yongsheng (2020). Multidisciplinary integrated design of long-range ballistic missile using PSO algorithm. Journal Of Systems Engineering And Electronics, Vol. 31, No. 2.DOI
95. 杨彪，荆武兴，李涧青，高长生（2020）. 动能拦截器运动伪装末制导律设计. 《宇航学报》.
96. Erkang Chen, Wuxing Jing, Changsheng Gao (2020). Moving-horizon-estimator-integrated adaptive hierarchical sliding mode control for flexible hypersonic vehicles considering aeroservoelastic effect. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
97. Pengxin Wei, Wei Wei, Changsheng Gao, Wuxing Jing (2020). Dynamics and control authority of a flight vehicle equipped with a translating moving mass and rotating rail. Aerospace Science and Technology.DOI
98. 张召，王恒，荆武兴，高长生（2019）. 大气层外多拦截器协同跟踪与制导算法. 《宇航学报》.
99. 陈尔康，荆武兴，高长生（2019）. 弹性高速飞行器的状态/参数滚动时域估计. 《北京航空航天大学学报》.DOI
100. 范一迪，荆武兴，高长生，杜华军（2019）. 滚控式变质心飞行器动力学特性分析与控制. 《宇航学报》.
101. 张召，荆武兴，李君龙，高长生（2019）. 谱估计理论在弹道数据参数化建模中的应用. 《宇航学报》.
102. 陈尔康，荆武兴，高长生（2019）. 弹性高超声速滑翔飞行器的状态/参数联合估计. 《航空学报》.
103. 李臻，杨彪，荆武兴，高长生，常武权（2019）. 逃逸飞行器轨迹鲁棒性快速评估及制导. 《载人航天》.DOI
104. 陈尔康，高长生，荆武兴（2019）. 空间目标的轨迹和姿态数据生成. 《西北工业大学学报》.
105. Yue Liu, Ying-Jing Qian, Wuxing Jing (2019). Orbit Keeping Control Strategy Design for the Quasi-period Orbit with STK/Astrogator. Chinese Control Conference (CCC).DOI
106. Chunwang Jiang, Guofeng Zhou, Changsheng Gao, Biao Yang, Wuxing Jing (2019). Nonlinear reentry guidance law guaranteeing convergence before attainment of desired line-of-sight range. Aerospace Science and Technology.DOI
107. Pengxin Wei, Wuxing Jing, Changsheng Gao (2019). Dynamics and Control for Hypersonic Gliding Vehicles Equipped with a Moving Mass and RCS. Journal of Aerospace Engineering.DOI
108. Erkang Chen, Changsheng Gao, Wuxing Jing (2019). The Method of Trajectory and Attitude Data Generation for Space Target. Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University.DOI
109. Erkang Chen, Wuxing Jing, Changsheng Gao (2019). Sensor placement and moving horizon state/parameter estimation for flexible hypersonic vehicles. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
110. Wuxing Jing, Zheng Xu, Changsheng Gao (2019). Influence of Initial State Errors on Perturbation Guidance Accuracy. Defence Science Journal.DOI
111. Pengxin Wei, Changsheng Gao, Wuxing Jing (2019). Longitudinal Aerodynamic Coefficients Estimation and Identifiability Analysis for Hypersonic Glider Controlled by Moving Mass. International Journal of Aeronautical and Space Sciences.DOI
112. 陈尔康，廖欣，高长生，荆武兴（2018）. 考虑刚体运动与弹体变形耦合效应的旋转导弹动力学建模. 《兵工学报》.
113. 陈尔康，廖欣，高长生，荆武兴（2018）. 旋转导弹喷气阻尼效应建模与分析. 《哈尔滨工业大学学报》.
114. 荆武兴（2018）. 空间飞行器导航、制导与控制.
115. 柏涛，王在铎，王勇，檀朋硕，荆武兴（2018）. 基于气动力辨识的主动减载控制方法. 《兵器装备工程学报》.
116. 刘玥，付凯林，荆武兴，钱霙婧（2018）. 月地低能返回轨道最优控制策略研究. 《载人航天》.
117. Jianqing Li, Sai Chen, Chaoyong Li, Changsheng Gao, Wuxing Jing (2018). Adaptive control of underactuated flight vehicles with moving mass. Aerospace Science and Technology.DOI
118. Chunwang Jiang, G.F. Zhou, Biao Yang, Changsheng Gao, Wuxing Jing (2018). Novel guidance model and its application for optimal re-entry guidance. The Aeronautical Journal.DOI
119. Zhitao Liu, Changsheng Gao, Jianqing Li, Wuxing Jing (2018). Closed-Loop Bifurcation Analysis for a Novel Moving Mass Flight Vehicle. International Journal of Aeronautical and Space Sciences.DOI
120. Jianqing Li, Changsheng Gao, Chaoyong Li, Wuxing Jing (2018). A survey on moving mass control technology. Aerospace Science and Technology.DOI
121. Yue Liu, Ying-Jing Qian, Wuxing Jing (2018). Study on Low Energy Moon Return Orbit Construction and Low Thrust Propulsion Control Strategy. IEEE CSAA Guidance, Navigation and Control Conference (CGNCC).DOI
122. Erkang Chen, Wuxing Jing, Changsheng Gao, Zhao Zhang (2018). An Adaptive Control Approach for a Flexible Hypersonic Glide Vehicle. International Conference on Mechanical and Aerospace Engineering.DOI
123. Zhao Zhang, Changsheng Gao, Wuxing Jing, Erkang Chen (2018). Firing Data Design for the Midcourse Interceptor with Complex Flight Program. International Conference on Mechanical and Aerospace Engineering.DOI
124. Jianqing Li, Changsheng Gao, Tianming Feng, Wuxing Jing (2018). Novel Moving Mass Flight Vehicle and Its Equivalent Experiment. Journal of Dynamic Systems Measurement and Control.DOI
125. Zheng Xu, Wuxing Jing, Changsheng Gao (2018). Trajectory characteristic analysis influenced by initial state errors for long-range vehicles. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
126. Ying-Jing Qian, Xiaodong YANG, Wuxing Jing, Wei Zhang (2018). An improved numerical method for constructing Halo/Lissajous orbits in a full solar system model. Chinese Journal of Aeronautics.DOI
127. Changsheng Gao, Jianqing Li, Yidi Fan, Wuxing Jing (2018). Immersion and invariance-based control of novel moving-mass flight vehicles. Aerospace Science and Technology.DOI
128. Changsheng Gao, Chunwang Jiang, Wuxing Jing (2017). Optimization of projectile state and trajectory of reentry body considering attainment of carrying aircraft. Journal Of Systems Engineering And Electronics, Vol. 280, No. 10.DOI
129. 李涧青，高长生，荆武兴（2017）. 单滑块变质心飞行器动力学与控制问题. 《第十届全国多体动力学与控制暨第五届全国航天动力学与控制学术会议论文摘要集》.
130. 高长生，陈尔康，荆武兴（2017）. 高超声速飞行器机动规避轨迹优化. 《哈尔滨工业大学学报》.
131. 杨源，郭嘉，荆武兴，万自明，武立军（2017）. 基于固体火箭发动机的月球软着陆主减速段制导律设计. 《第18届中国系统仿真技术及其应用学术年会论文集（18th CCSSTA 2017）》.
132. 罗绪盛，荆武兴，高长生（2017）. 火星探测捕获的误差传播分析. 《系统工程与电子技术》.
133. 封天明，李涧青，高长生，荆武兴（2017）. 考虑地球敏感器误差的自主导航方法研究. 《上海航天(中英文)》.
134. 罗绪盛，麻娜，荆武兴，盛伟强（2017）. 采用有限推力的火星捕获制动策略. 《西北工业大学学报》.
135. 廖欣，陈尔康，高长生，荆武兴（2017）. 喷气阻尼效应作用下旋转导弹锥形运动分析. 《上海航天(中英文)》.
136. Changsheng Gao, Jing Li, Tianming Feng, Wuxing Jing (2017). Adaptive terminal guidance law with impact-angle constraint. The Aeronautical Journal.DOI
137. Jianqing Li, Changsheng Gao, Wuxing Jing, Yidi Fan (2017). Nonlinear vibration analysis of a novel moving mass flight vehicle. Nonlinear Dynamics.DOI
138. Zheng Xu, Na Ma, Changsheng Gao, Wuxing Jing (2017). Propagation mechanism analysis of navigation errors caused by initial state errors for long-range vehicles. Aerospace Science and Technology.DOI
139. 高长生，李涧青，荆武兴（2016）. 拦截机动目标的运动伪装制导律. 《宇航学报》.
140. 杨一岱，荆武兴，张召（2016）. 一种挠性航天器的对偶四元数姿轨耦合控制方法. 《宇航学报》.
141. 刘玥，钱霙婧，马林，王鹏，荆武兴（2016）. 月球低能返回轨道设计的混合自适应遗传算法. 《哈尔滨工业大学学报》.
142. 郑旭，高长生，荆武兴，常晓华（2016）. 发射初态误差对弹道特征参数的影响. 《固体火箭技术》.
143. 李瑞康，史秉政，张召，荆武兴（2016）. 基于粒子群算法的多拦截器分配优化策略. 《航天控制》.
144. 李涧青，高长生，荆武兴，杜华军（2016）. 俯控式单滑块变质心飞行器控制问题. 《中国科学:技术科学》.
145. 郑旭，高长生，陈尔康，荆武兴（2016）. 一种基于大气层外解析动力学模型的最优迭代制导方法. 《西北工业大学学报》.
146. 李瑞康，张学进，魏喜庆，张召，荆武兴（2016）. 多目标拦截任务分配建模与分析. 《上海航天(中英文)》.
147. Jianqing Li, Changsheng Gao, Wuxing Jing, Pengxin Wei (2016). Dynamic analysis and control of novel moving mass flight vehicle. Acta Astronautica.DOI
148. DU Hua-jun, Wuxing Jing, Changsheng Gao, Jianqing Li (2016). Attitude control of reentry vehicle with a pitch-control single moving mass. Scientia Sinica Technologica.DOI
149. Jianqing Li, Changsheng Gao, Tianming Feng, Wuxing Jing (2016). Error Correction of Infrared Earth Radiance for Autonomous Navigation. Journal of Navigation.DOI
150. Yi-dai Yang, Zheng Xu, Wuxing Jing (2016). Adaptive attitude control of liquid-filled spacecraft with flexible appendages. Chinese Control Conference (CCC).DOI
151. Zheng Xu, Yi-dai Yang, Changsheng Gao, Wuxing Jing (2016). On formation mechanism and influence characteristic of initial state error in disturbing gravity field. Chinese Control Conference (CCC).DOI
152. Erkang Chen, Changsheng Gao, Wuxing Jing (2016). Virtual displacement guidance for hypersonic glide vehicle. Chinese Control Conference (CCC).DOI
153. Changsheng Gao, Chunwang Jiang, Yan Zhang, Wuxing Jing (2016). Three-Dimensional Integrated Guidance and Control for Near Space Interceptor Based on Robust Adaptive Backstepping Approach. International Journal of Aerospace Engineering.DOI
154. Changsheng Gao, Jianqing Li, Wuxing Jing (2016). A Terminal Guidance Law Based on Motion Camouflage Strategy of Air-to-Ground Missiles. International Journal of Aerospace Engineering.DOI
155. 杨一岱，荆武兴，刘玥（2015）. 挠性航天器浮动质心动力学建模. 《哈尔滨工业大学学报》.
156. 李罗钢，荆武兴，高长生（2015）. 拦截临近空间飞行器零控脱靶量计算方法. 《弹道学报》.
157. Yue Liu, Wuxing Jing, Yingying Xiao (2015). Finite thrust transfer strategy designing for low energy moon return based on GPM/VSM. Machine Intelligence Research.DOI
158. Wuxing Jing, Zheng Xu, Pengxin Wei, Jia Guo (2015). An ascent iterative guidance algorithm for solid rocket concerned with multiconstraints.DOI
159. Jianqing Li, Changsheng Gao, Ying-Jing Qian, Wuxing Jing (2015). Stationkeeping strategy for quasi-periodic orbit around Earth-Moon L2 point.DOI
160. 李罗钢，荆武兴，高长生（2014）. 基于预警卫星系统的临近空间飞行器跟踪. 《航空学报》.
161. 荆武兴，刘玥（2014）. 椭圆三体问题下月球L2低能逃逸轨道设计. 《航空学报》.
162. 钱霙婧，荆武兴，刘玥，李涧青（2014）. 地月平动点拟周期轨道设计方法. 《系统工程与电子技术》.
163. 李涧青，高长生，郑建华，荆武兴（2014）. 基于金星借力的黄道面外日冕探测器轨道设计. 《上海航天(中英文)》.
164. Pengxin Wei, Changsheng Gao, Wuxing Jing (2014). Roll control problem for the long-range maneuverable warhead. Aircraft Engineering and Aerospace Technology.DOI
165. 高长生，荆武兴，魏鹏鑫（2013）. 远程机动弹头单滑块质量矩和喷气组合BTT控制问题研究. 《第七届全国动力学与控制青年学者研讨会论文摘要集》.
166. 韦文书，荆武兴，高长生（2013）. 捕获非合作目标后航天器的自主稳定技术研究. 《航空学报》.
167. 荆武兴，韦文书，高长生（2013）. 基于陀螺测量信息的航天器突变参数识别方法. 《系统工程与电子技术》.
168. 荆武兴，李罗钢，高长生（2013）. 反导拦截飞行方案及时间窗口快速搜索算法. 《系统工程与电子技术》.
169. 魏鹏鑫，荆武兴，高长生（2013）. 具有落角约束的弹道导弹再入末制导律设计. 《哈尔滨工业大学学报》.
170. 刘玥，荆武兴（2013）. 利用虚拟卫星法求解火星探测器近火点制动策略. 《哈尔滨工业大学学报》.
171. 钱霙婧，荆武兴，高长生，韦文书（2013）. 地月平动点拟周期轨道探测器自主导航方法研究. 《宇航学报》.
172. 魏鹏鑫，荆武兴，高长生（2013）. 攻防对抗机动过载关系分析. 《宇航学报》.
173. 高长生，张研，魏鹏鑫，荆武兴（2013）. 质量矩控制自旋弹弹体性能分析. 《飞行力学》.
174. Wuxing Jing, Ying-Jing Qian, Changsheng Gao, Jianqing Li (2013). Autonomous navigation to quasi-periodic orbits near translunar libration points. Chinese Journal of Aeronautics.DOI
175. Changsheng Gao, Wuxing Jing, Pengxin Wei (2013). Research on application of single moving mass in the reentry warhead maneuver. Aerospace Science and Technology.DOI
176. Changsheng Gao, Pengxin Wei, Wuxing Jing (2013). Dynamics modeling and control system design for the reentry warhead controlled by single moving mass. International Conference on Control and Automation.DOI
177. Wuxing Jing (2013). Research on the affect of inertial force on moving mass actuated spin missile. Flight Dynamics.
178. 高长生，郑建华，荆武兴（2012）. 借力飞行日冕探测器轨道设计. 《第六届全国动力学与控制青年学者学术研讨会》.
179. 韦文书，荆武兴，高长生（2012）. 机动发射的弹道导弹飞行诸元的快速计算. 《哈尔滨工业大学学报》.
180. 魏鹏鑫，高长生，荆武兴（2012）. 基于稳定性分析的变质心再入飞行器布局参数设计. 《导弹与航天运载技术(中英文)》.
181. 李茂登，荆武兴，黄翔宇（2012）. 考虑地球扁率修正的基于日地月方位信息的地球卫星自主导航. 《宇航学报》.
182. 李茂登，荆武兴，黄翔宇（2012）. 考虑月球扁率修正的月球卫星自主导航. 《宇航学报》.
183. 夏喜旺，荆武兴（2012）. 基于时间最优的大气层外拦截律设计. 《上海航天(中英文)》.
184. 高长生，姜春旺，魏鹏鑫，荆武兴（2012）. 一种新型质量矩飞行器总体布局方案研究. 《飞行力学》.
185. 魏鹏鑫，高长生，荆武兴（2012）. 质量矩控制飞行器的压心不确定性问题研究. 《航天控制》.
186. 魏鹏鑫，荆武兴，高长生（2012）. 轨道要素奇异问题的改进四元数方法. 《中国空间科学技术(中英文)》.
187. 夏喜旺，荆武兴，高长生，韦文书 (2012). Attitude control of spacecraft during propulsion of swing thruster. Journal of Harbin Institute of Technology(New series).
188. Ying-Jing Qian, Chaoyong Li, Wuxing Jing, Inseok Hwang, Wei Jian (2012). Sun–Earth–Moon autonomous orbit determination for quasi-periodic orbit about the translunar libration point and its observability analysis. Aerospace Science and Technology.DOI
189. Luogang Li, Wuxing Jing, Changsheng Gao (2012). Calculating flight program and launch time window for intercept missile. International Conference on Intelligent Control and Information Processing.DOI
190. Maodeng Li, Wuxing Jing, Xiangyu Huang (2012). Dual Cone-Scanning Horizon Sensor Orbit and Attitude Corrections for Earth Oblateness. Journal of Guidance Control and Dynamics.DOI
191. Wuxing Jing (2012). The Research on the Uncertainty of Pressure Center for Moving Mass Actuated Vehicle. Aerospace Control.
192. Wuxing Jing (2012). Exoatmospheric Interception Law Design Based on Minimum Time. Aerospace Shanghai.
193. Wuxing Jing (2012). Research on a new method of global layout for moving mass actuated vehicle. Flight Dynamics.
194. 高长生，荆武兴，魏鹏鑫（2011）. 质量矩控制导弹执行机构配置问题研究. 《The 5th 全国动力学与控制青年学者研讨会》.
195. 韦文书，荆武兴，谷立祥，高长生（2011）. 变质量飞行器变轨中摇摆发动机指向跟踪问题研究. 《宇航学报》.
196. 高长生，荆武兴，李君龙（2011）. 基于自适应反演法的质量矩导弹控制律设计. 《兵工学报》.
197. 魏鹏鑫，高长生，荆武兴（2011）. 基于自适应滑模的变质心再入飞行器控制律设计. 《上海航天(中英文)》.
198. 夏喜旺，荆武兴（2011）. 大气层外拦截器脉冲制导律. 《上海航天(中英文)》.
199. 荆武兴，李茂登，黄翔宇（2011）. 基于日地月方位信息的自主导航系统的脉冲仿真和方位确定. 《航天控制》.
200. 荆武兴，夏喜旺，高长生，韦文书（2011）. 大载荷摆动情况下飞行器姿态控制研究(英文). Chinese Journal of Aeronautics.
201. Wuxing Jing, Xiwang Xia, Changsheng Gao, Wenshu WEI (2011). Attitude Control for Spacecraft with Swinging Large-scale Payload. Chinese Journal of Aeronautics.DOI
202. 李罗刚，崔祜涛，马春飞，毛春晓，荆武兴（2010）. 月面返回最优轨道设计. 《哈尔滨工业大学学报》.
203. 高长生，荆武兴，于本水，李君龙（2010）. 质量矩导弹构型及自适应控制律设计. 《航空学报》.
204. 高长生，李君龙，荆武兴，李瑞康（2010）. 导弹质量矩控制技术发展综述. 《宇航学报》.
205. 钱霙婧，荆武兴，高长生（2010）. 多航天器部署问题中的自主导航方法研究. 《哈尔滨工业大学学报》.
206. 李瑞康，高长生，荆武兴，钱霙婧（2010）. 飞行器变质心控制及性能分析. 《宇航学报》.
207. 荆武兴，高长生（2010）. 月球探测器精确相对动力学模型及其应用. 《中国科学:物理学 力学 天文学》.
208. 李瑞康，荆武兴，高长生，杜华军（2010）. 基于布局优化的飞行器变质心控制性能研究. 《上海航天(中英文)》.
209. Maodeng Li, Wuxing Jing, Malcolm Macdonald, Colin Robert McInnes (2010). Adaptive backstepping control for optimal descent with embedded autonomy. Aerospace Science and Technology.DOI
210. Weiyue Chen, Wuxing Jing (2010). Dynamics Equations of Relative Motion around an Oblate Earth with Air Drag. Journal of Aerospace Engineering.DOI
211. Weiyue Chen, Wuxing Jing (2010). Differential Equations of Relative Motion under the In uence of J2 Perturbation and Air Drag. AIAA SPACE Conference & Exposition.DOI
212. Xiwang Xia, Wuxing Jing, Chaoyong Li, Changsheng Gao (2010). Time-shared scheme design for attitude control system during space separation. Aerospace Science and Technology.DOI
213. Changsheng Gao, Ying-Jing Qian, Ruikang Li, Wuxing Jing (2010). Research on remanence calibration and orbit determination for satellite. International Symposium on Systems and Control in Aeronautics and Astronautics.DOI
214. Changsheng Gao, Ruikang Li, Wuxing Jing (2010). A re-entry guidance method for vehicle using virtual displacement concept. Chinese Control and Decision Conference (CCDC).DOI
215. Chaoyong Li, Wuxing Jing, Hui Wang, Zhiguo Qi (2010). Gain-Varying Guidance Algorithm using Differential Geometric Guidance Command. IEEE Transactions on Aerospace and Electronic Systems.DOI
216. Wuxing Jing (2010). Optimal orbit design of returning from the moon. Ha'erbin gongye daxue xuebao.
217. 赵英彪，荆武兴（2009）. 柔性航天器单轴姿态机动的鲁棒稳定性分析. 《哈尔滨工业大学学报》.
218. 高长生，李瑞康，荆武兴（2009）. 新型制导律在变质心再入飞行器中的应用. 《哈尔滨工业大学学报》.
219. 夏喜旺，荆武兴，李超勇（2009）. 火箭助推器在空间中对雷达观测的影响. 《哈尔滨工业大学学报》.
220. 荆武兴，李瑞康，高长生（2009）. 最优控制在变质心再入飞行器滚动稳定中的应用. 《宇航学报》.
221. 陈伟跃，荆武兴，程博（2009）. 小推力速度闭环交会制导律设计. 《宇航学报》.
222. 李瑞康，荆武兴，高长生，杜华军（2009）. 变质心飞行器姿态与弹道性能分析. 《宇航学报》.
223. 夏喜旺，荆武兴，李超勇（2009）. 火箭助推器对雷达观测的影响研究. 《飞行力学》.
224. 荆武兴，高桦，陈旭，刘青松（2009）. 基于相平面法的飞行器大角度机动控制技术研究. 《实验技术与管理》.
225. 李瑞康，荆武兴，高长生，杜华军（2009）. 再入弹头质量矩复合控制系统设计. 《航天控制》.
226. Weiyue Chen, Wuxing Jing, Chaoyong Li (2009). Attitude recovery for microsatellite via magnetic torque.DOI
227. Wuxing Jing, Changsheng Gao (2009). Large-angle attitude acquisition and tracking of a lunar probe with on-off jets. IEEE International Conference on Automation and Logistics (ICAL).DOI
228. Weiyue Chen, Wuxing Jing (2009). Robust attitude acquisition for micro‐satellite. Aircraft Engineering and Aerospace Technology.DOI
229. Wuxing Jing (2009). Robust stability of flexible spacecraft during attitude maneuver. Ha'erbin gongye daxue xuebao.
230. 高长生，荆武兴，李瑞康（2008）. 提高变质心飞行器可操纵性的方法研究. 《宇航学报》.
231. 程博，荆武兴，陈伟跃（2008）. 远程自主交会改进制导算法. 《宇航学报》.
232. 黄琳，荆武兴（2008）. 卫星姿态确定与三轴磁强计校正. 《宇航学报》.
233. 郑立伟，荆武兴（2008）. 大气层外拦截器近最优中制导律设计. 《宇航学报》.
234. 高长生，荆武兴，李瑞康（2008）. 质量矩再入飞行器的参数优化和性能分析. 《航空学报》.
235. 夏喜旺，荆武兴，李超勇，郑立伟（2008）. 美国地基中段防御系统部署及作战分析. 《现代防御技术》.
236. Xiwang Xia, Wuxing Jing, Weiyue Chen (2008). Study on the influence of Rocket booster to radar observation. International Symposium on Systems and Control in Aeronautics and Astronautics.DOI
237. Weiyue Chen, Wuxing Jing, Xiwang Xia (2008). Autonomous robust orbital and attitude coupling control of final proximity in rendezvous. International Symposium on Systems and Control in Aeronautics and Astronautics.DOI
238. Ruikang Li, Wuxing Jing, Changsheng Gao (2008). A design on moving-mass actuated reentry vehicle with predictive guidance law. International Symposium on Systems and Control in Aeronautics and Astronautics.DOI
239. Y. Zhang, Wuxing Jing, Lixia Liu (2008). Autonomous orbit and attitude determination of satellite using SEMOI. Aircraft Engineering and Aerospace Technology.DOI
240. Wuxing Jing, Weiyue Chen (2008). Robust Attitude Acquisition for Microsatellite via Magnetic Torquers and Moment Bias flywheel. AIAA Guidance, Navigation, and Control Conference and Exhibit.DOI
241. Chaoyong Li, Wuxing Jing, Changsheng Gao (2008). Adaptive backstepping-based flight control system using integral filters. Aerospace Science and Technology.DOI
242. Lin Huang, Wuxing Jing (2008). Attitude-Independent Geomagnetic Navigation Using Onboard Complete Three-Axis Magnetometer Calibration. Proceedings - IEEE Aerospace Conference.DOI
243. Wuxing Jing (2008). Spacecraft Attitude Determination and Three-Axis Magnetometer Calibration. Journal of Astronautics.
244. Chaoyong Li, Wuxing Jing (2008). Analysis of 3D Geometric Guidance Problem. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES.DOI
245. Wuxing Jing (2008). Design of a Near Optimal Midcourse Guidance Law for Exoatmospheric Interceptor. Journal of Astronautics.
246. 李超勇，齐治国，荆武兴（2007）. 平面微分几何制导律应用研究. 《哈尔滨工业大学学报》.
247. 黄琳，荆武兴（2007）. 平均地磁控制器的研究. 《哈尔滨工业大学学报》.
248. 高长生，荆武兴，郑立伟（2007）. 再入弹道解析算法在新型制导律上的应用研究. 《宇航学报》.
249. 李超勇，荆武兴，齐治国，王辉（2007）. 空间微分几何制导律应用研究. 《宇航学报》.
250. 郑立伟，荆武兴，谷立祥（2007）. 一种适用于大气层外动能拦截器的末制导律. 《航空学报》.
251. 高长生，荆武兴（2007）. 同地迹八颗IGSO卫星区域导航星座分析. 《哈尔滨工业大学学报》.
252. 郑立伟，荆武兴（2007）. 适用于大气层外拦截器的近最优中制导律. 《第二十六届中国控制会议论文集》.
253. 郑立伟，荆武兴，张建英（2007）. 适用于大距离拦截场景的零控脱靶量计算方法. 《第二十六届中国控制会议》.
254. 李瑞康，荆武兴，高长生（2007）. 再入体变质心动力学建模与仿真分析. 《第二十六届中国控制会议论文集》.
255. 高桦，王艳奎，荆武兴，齐乃明（2007）. 基于DSP的飞行器大角度机动控制实验技术研究. 《计算机测量与控制》.
256. 黄琳，荆武兴 (2007). Study on autonomous satellite navigation from SHAR observations. Journal of Harbin Institute of Technology(New series).
257. Maodeng Li, Wuxing Jing (2007). Translunar low-energy trajectories via Earth-Moon L1 Lyapunov orbit. IEEE International Conference on Robotics and Biomimetics (ROBIO).DOI
258. Weiyue Chen, Wuxing Jing (2007). LMI-based H2/H ∞ terminal proximity guidance algorithm for autonomous rendezvous and docking. Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE.DOI
259. Chaoyong Li, Wuxing Jing (2007). Application of PID controller to 2D differential geometric guidance problem. Journal of Control Theory and Applications.DOI
260. Chaoyong Li, Wuxing Jing (2007). Geometric approach to capture analysis of PN guidance law. Aerospace Science and Technology.DOI
261. Chaoyong Li, Wuxing Jing (2007). Fuzzy PID controller for 2D differential geometric guidance and control problem. IET Control Theory and Applications.DOI
262. Chaoyong Li, Wuxing Jing, Hui Wang, Zhiguo Qi (2007). Development of flight control system for 2D differential geometric guidance and control problem. Aircraft Engineering and Aerospace Technology.DOI
263. Chaoyong Li, Wuxing Jing, Zhiguo Qi, Hui Wang (2007). A Novel Approach to the 2D Differential Geometric Guidance Problem. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES.DOI
264. 张燕，荆武兴（2006）. 一种利用双DSP实现卫星SEMOI自主导航方法. 《哈尔滨工业大学学报》.
265. 黄琳，荆武兴（2006）. 关于剩磁对卫星姿态确定与控制影响的研究. 《航空学报》.
266. 高长生，郑建华，荆武兴，吴霞（2006）. 基于地球引力变轨的日冕探测器轨道设计. 《宇航学报》.
267. 黄琳，荆武兴（2006）. 利用并行多处理器的卫星自主导航方法研究. 《哈尔滨工业大学学报》.
268. 郑立伟，荆武兴，张燕（2006）. 基于高斯问题的近最优再入预测制导方法研究. 《航天控制》.
269. 郑立伟，荆武兴（2006）. 基于零作用误差的自适应变结构制导律. 《第25届中国控制会议论文集（中册）》.
270. 张燕，荆武兴（2006）. 朔月期间基于SEMOI的卫星自主导航方法研究. 《上海航天(中英文)》.
271. 高长生，荆武兴，张燕，黄翔宇（2006）. 基于Unscented卡尔曼滤波器的近地卫星磁测自主导航. 《中国空间科学技术(中英文)》.
272. 张燕，荆武兴（2006）. 基于紫外月球敏感器和测高仪测量信息的月球探测器自主导航. 《第25届中国控制会议论文集（下册）》.
273. Chaoyong Li, Wuxing Jing, Hui Wang, Zhiguo Qi (2006). Iterative solution to differential geometric guidance problem. Aircraft Engineering and Aerospace Technology.DOI
274. Chaoyong Li, Wuxing Jing, Hui Wang, Zhiguo Qi (2006). Application of 2D Differential Geometric Guidance to Tactical Missile Interception. Proceedings - IEEE Aerospace Conference.DOI
275. Chaoyong Li, Wuxing Jing, Hui Wang, Zhiguo Qi (2006). Iterative Solution to Three-dimensional Differential Geometric Guidance Problem. Proceedings - IEEE Aerospace Conference.DOI
276. Chaoyong Li, Wuxing Jing (2006). Application of PID Controller to 2D Differential Geometric Guidance and Control Problem. Chinese Control Conference (CCC).DOI
277. Chaoyong Li, Wuxing Jing (2006). New Results on Three-dimensional Differential Geometric Guidance and Control Problem. AIAA Guidance, Navigation, and Control Conference and Exhibit.DOI
278. Liwei Zheng, Wuxing Jing (2006). Application of Predictive Guidance to Reentry Vehicle. International Symposium on Systems and Control in Aeronautics and Astronautics.DOI
279. Chaoyong Li, Wuxing Jing, Hui Wang, Zhiguo Qi (2006). Analytical Solution to 3D Differential Geometric Guidance Problem. International Symposium on Systems and Control in Aeronautics and Astronautics.DOI
280. Lin Huang, Wuxing Jing (2006). Attitude Stabilization of Averaging Magnetic Torque. International Symposium on Systems and Control in Aeronautics and Astronautics.DOI
281. Changsheng Gao, Wuxing Jing (2006). Autonomous Satellite Navigation Using Magnetic Measurements. International Symposium on Systems and Control in Aeronautics and Astronautics.DOI
282. Wuxing Jing (2006). Effects of Remanence on Attitude Determination and Control of Satellites. Acta Aeronautica Et Astronautica Sinica.
283. Wuxing Jing (2006). A study on autonomous satellite navigation scheme using parallel computers. Ha'erbin gongye daxue xuebao.
284. Wuxing Jing (2006). Research on Autonomous Navigation for Satellite during New-Moon Period Based on SEMOI. Aerospace Shanghai.
285. Wuxing Jing (2006). Realization of satellite autonomous navigation with double DSPs based on SEMOI. Ha'erbin gongye daxue xuebao.
286. 黄琳，荆武兴（2005）. 利用雷达高度计及星敏感器的多处理器卫星导航. 《宇航学报》.
287. 张燕，荆武兴（2005）. 基于日地月方位信息的月球卫星自主导航. 《宇航学报》.
288. 荆武兴，高长生（2005）. 亚太区域导航八星星座分析. 《航天控制》.
289. 黄琳，荆武兴，李应波，景前峰（2005）. 利用雷达高度计的卫星自主导航. 《上海航天(中英文)》.
290. 黄琳，荆武兴（2005）. 关于磁强计与磁力矩器分时工作方案的研究. 《航天控制》.
291. Wuxing Jing (2005). Relation equations among the parameters of tracking - differentiator and the amplitude and frequency of its input - output signals. Dianji yu kongzhi xuebao.
292. Wuxing Jing (2005). Autonomous Navigation for Lunar Satellite based on the Optical Information of Sun-Earth-Moon. Journal of Astronautics.
293. Wuxing Jing (2005). Autonomous Navigation Using Radar Altimeter and Star Sensor Based on Parallel Navigation Computer. Journal of Astronautics.
294. 龙兵，宋立辉，荆武兴，姜兴渭，李志（2003）. 航天器故障诊断技术回顾与展望. 《导弹与航天运载技术(中英文)》.
295. 贾英宏，徐世杰，荆武兴（2003）. 带弹性附件的航天器的动力学与变结构控制. 《哈尔滨工业大学学报》.
296. 彭冬亮，徐世杰，荆武兴（2003）. 充液挠性飞行器的变结构控制. 《哈尔滨工业大学学报》.
297. 荆武兴（2003）. 基于日地月方位信息的近地轨道卫星自主导航. 《宇航学报》.
298. 黄翔宇，荆武兴（2002）. 基于“日-地-月”信息的卫星自主导航技术研究. 《哈尔滨工业大学学报》.
299. 彭冬亮，荆武兴，徐世杰（2002）. 停靠阶段轨道姿态耦合动力学与控制研究. 《飞行力学》.
300. Wuxing Jing, Colin Robert McInnes (2002). Memorised quasi-time–fuel-optimal feedback control of perturbed double integrator. Automatica.DOI
301. Wuxing Jing, Shijie Xu (2002). Nonlinear Attitude Tracking Control of a Spacecraft with Thrusters Based on Error Quaternions. Chinese Journal of Aeronautics.DOI
302. 缪协兴，陈占清，荆武兴（2001）. 变质量挠性体动力学普遍方程(二). 《哈尔滨工业大学学报》.
303. 荆武兴，徐世杰，吴瑶华（2000）. 连续力矩作用下的柔性航天器再定向与振动抑制. 《宇航学报》.
304. 聂润兔，荆武兴，徐世杰，邵成勋（1999）. 中继卫星对目标的跟踪规律研究. 《哈尔滨工业大学学报》.
305. 王学孝，荆武兴，袁英莉（1998）. 再入体气动参数辨识. 《导弹与航天运载技术(中英文)》.
306. 荆武兴，吴瑶华（1997）. 卫星轨道圆化的有限推力点火控制策略. 《宇航学报》.
307. 荆武兴，吴瑶华，杨涤（1997）. 基于交会概念的最省燃料共面有限推力轨道转移方法. 《哈尔滨工业大学学报》.
308. 荆武兴，韩品尧，王学孝，吴瑶华（1996）. 基于拟欧拉角信号的连续力矩姿态机动控制. 《宇航学报》.
309. 于泳，荆武兴，栾泽威，杨涤（1996）. 基于Loh常数假设的AOTV最优闭环导引律的设计. 《导弹与航天运载技术(中英文)》.
310. 荆武兴，杨涤，吴瑶华（1993）. 对接飞行器大角度姿态机动控制. 《哈尔滨工业大学学报》.
311. 荆武兴，杨涤，吴瑶华（1993）. 相对运动有限推力轨道控制. 《宇航学报》.
312. 荆武兴，杨涤，吴瑶华（1992）. AOTV的最优控制问题研究. 《哈尔滨工业大学学报》.
313. 荆武兴，杨涤，吴瑶华（1992）. AOTV的极小时间控制. 《宇航学报》.
314. 王明春，荆武兴，杨涤，吴瑶华（1992）. 能量最省有限推力同平面轨道转移. 《宇航学报》.
315. 荆武兴，杨涤，吴瑶华，王学孝（1991）. 引力引起的空间站轨道与姿态耦合动力学方程的建立和计算. 《哈尔滨工业大学学报》.

会议论文

1. Lin Huang, Wuxing Jing (2006). Correction of Remanent Disturbance Torque. International Symposium on Systems and Control in Aeronautics and Astronautics.DOI

预印本

1. Xinru Liang, Yudong Hu, Yiting Tan, Changsheng Gao, Wuxing Jing (2022). An Adaptive Variational Bayesian Student-T Mixture Filter Under Non-Gaussian Noise with Unknown Priori Statistical Information. SSRN Electronic Journal.DOI

书籍章节

1. Biao Yang, Wuxing Jing, Changsheng Gao (2021). Design of Midcourse Trajectory for Boost Phase Interception. Lecture notes in electrical engineering.DOI
2. Yudong Hu, Junlong Li, Zhao Zhang, Wuxing Jing, Changsheng Gao (2020). Parametric modeling of hypersonic ballistic data based on time varying auto-regressive model. Science China Technological Sciences.DOI