百晓学者学者目录

陈万春

北京航空航天大学宇航学院

个人简介

陈万春，男，1964年11月出生于湖南省江华，北京航空航天大学宇航学院教授、博士生导师。1986年和1989年获北京航空航天大学飞行器设计与应用力学系导弹设计专业学士、硕士学位，1995年获该校飞行力学与控制专业博士学位。1991年至今在宇航学院从事教学和科研工作，研究方向包括导弹飞行力学与控制、导弹总体设计、导弹攻防对抗和效能评估。

精选作品

期刊论文

  1. 康林，王新龙，陈万春，雷文贵（2026）. 基于混合式惯导系统构型优化的弹道导弹落点精度研究. 《航空学报》.
  2. 雷霄，周浩，陈万春（2026）. 组合动力高超声速飞行器双模态机动突防策略研究. 《战术导弹技术》.DOI
  3. 李知麟，周浩，陈万春（2026）. 基于神经网络的载机机动策略与攻击时机在线决策方法研究. 《空军工程大学学报》.
  4. Wengui Lei, Wan-Chun Chen, Liang Yang (2026). Ascent Trajectory Optimization with Singular Arc Using Linear Gauss Pseudospectral Model Predictive Control. Aerospace Science and Technology.DOI
  5. Peng Wang, Wan-Chun Chen, Shilei Zhao, Liang Yang (2026). Exoatmospheric optimal midcourse guidance law with coasting phase optimization using linear Gauss pseudospectral model predictive control. Chinese Journal of Aeronautics.DOI
  6. Xin-Miao Liu, Wan-Chun Chen, Wengui Lei, Zijiao Wang (2026). Trajectory Tracking of Reentry Vehicle Based on KalmanNet with Time-Varying Observation Matrix. Actuators.DOI
  7. Chenglin Hou, Xiao-Ming Liu, Liang Yang, Wan-Chun Chen, Tonggang Zhao (2026). Entry Trajectory Optimization With Complex No-Fly Zone Constraints Using Bilinear Interpolation and Augmented MPSP. IEEE Transactions on Aerospace and Electronic Systems.DOI
  8. Wenbin Yu, Yixuan Li, Jin Yang, Wanchun Chen (2026). Analytical entry guidance scheme for multiple complex-shape no-fly zones avoidance. Aerospace Science and Technology.DOI
  9. Muhammad Mushtaq, Wenbin Yu, Wanchun Chen (2026). Field-of-View Constrained Optimal Guidance Law for Impact-Time and Angle Control. International Journal of Aeronautical and Space Sciences.DOI
  10. Nanxiang Wang, Zhongyuan Chen, Wanchun Chen (2026). Acceleration Profile Shapeable Catenary-Based Guidance With Arbitrary Impact Time and Angle Constraints. IEEE Transactions on Aerospace and Electronic Systems.DOI
  11. 张珂洋，王鹏，于琦，余文斌，陈万春（2025）. 运载火箭助推段大攻角剖面高精度弹道解析解. 《北京航空航天大学学报》.DOI
  12. 李响，陈万春，杨良，赵洪，梁雪超（2025）. 高速变形飞行器伪谱在线规划协同再入制导律. 《宇航学报》.
  13. 李政，刘小明，陈万春，刘晓冬，金世鑫，田龙（2025）. 考虑泄漏的火工分离推杆内弹道解析解. 《弹箭与制导学报》.DOI
  14. 陈万春，郑佳，郑学合，于琦，曾鹏，王超（2025）. 拦截弹主动段自适应能量分配弹道规划方法. 《现代防御技术》.
  15. 杨良，杨李俊，陈万春（2025）. “飞行器方向专业课程设计”教学内容深化. 《教育教学论坛》.
  16. 李知麟，周浩，陈万春（2025）. 复杂拦截场景下空地导弹突防策略优化与实时决策研究. 《飞行力学》.DOI
  17. 严胜，周浩，赵涛，毛金娣，陈万春（2025）. 考虑时间和角度约束的再入轨迹快速规划方法. 《飞行力学》.
  18. 刘鑫淼，陈万春（2025）. 基于深度学习神经网络的弹道预报方法研究. 《飞行力学》.DOI
  19. 陈万春，王楠翔，龚晓鹏（2025）. 机动突防/精确打击在线制导方法. 《导弹与航天运载技术(中英文)》.
  20. 陈万春（2025）. TTI/FlightSim跨学科弹道集成设计与仿真教程. 《北京航空航天大学出版社》.
  21. Xiang Li, Wan-Chun Chen, Liang Yang, Hao Liu (2025). Integrated Algorithm for PPO‐Based Intelligent Dynamic Target Assignment and Entry Guidance Using Quasi‐Second‐Order Enhanced Linear Pseudospectral Method. International Journal of Robust and Nonlinear Control.DOI
  22. Peng Wang, Wan-Chun Chen, Chenglong Luo, Zhong-Yuan Chen (2025). A Guidance Law for the Boost Phase of Dual-Pulse Missile Based on Neural Network. International Conference on Mechanical and Aerospace Engineering.DOI
  23. Xiang Xu, Wan-Chun Chen, Liang Yang (2025). Nonlinear Optimal Midcourse Guidance Using Sequential Pseudospectral Model Predictive Control. IEEE Transactions on Aerospace and Electronic Systems.DOI
  24. Li-Jun Yang, Kai Liu, Liang Yang, Wan-Chun Chen, Xiang Li, Xiao Lei (2025). A Multi-Stage Linear Gauss Pseudospectral Successive Convex Method with Costate Information for Solving Optimal Control Problems. International Conference on Mechanical and Aerospace Engineering.DOI
  25. Wengui Lei, Jia Deng, Wan-Chun Chen, Liang Yang (2025). An Efficient Method for Singular Optimal Control of Goddard Problem Based on Radau Pseudospectral Method. International Conference on Mechanical and Aerospace Engineering.DOI
  26. Xiang Xu, Wan-Chun Chen, Liang Yang, Xiao-Ming Liu (2025). Online Suboptimal Ascent Guidance for Electromagnetic Assisted Launch Vehicle. International Conference on Mechanical and Aerospace Engineering.DOI
  27. Zhiqing Gou, Wan-Chun Chen, Liang Yang (2025). Trajectory Optimization and Guidance Strategy for TBCC Powered Vehicles Considering Mode Transition Point. International Conference on Mechanical and Aerospace Engineering.DOI
  28. Chao Xiahou, Hao Zhou, Wan-Chun Chen, Liang Yang (2025). Varying Speed Cooperative Differential Game Guidance Laws With Intercept Angle Constraints. International Journal of Aerospace Engineering.DOI
  29. Tian-You Zhang, Wan-Chun Chen, Liang Yang (2025). Linear Gauss Pseudospectral Method Using Neighboring Extremal for Nonlinear Optimal Control Problems. Aerospace.DOI
  30. Zhaowei Yu, Zhaowei Yu, Wanchun Chen, Wenbin Yu, Shilei Zhao (2025). Analytical solution for three-dimensional skip re-entry trajectory. Advances in Space Research.DOI
  31. Xiangxiang Li, Wanchun Chen, Zhongyuan Chen, Heng Hua Shi (2025). Capturability Analysis for Biased PN-Based Impact Angle Guidance Law. Advances in Astronautics.DOI
  32. Wenjie Yuan, Tonggang Zhao, Qi Hui Yu, Xiaopeng Gong, Wanchun Chen, Xiaoming Liu (2025). Trajectory Prediction Method Under Low Information Support Condition. Lecture notes in electrical engineering.DOI
  33. Peng Wang, Wanchun Chen, Nanxiang Wang, Zhongyuan Chen, Xiaoming Liu (2025). Analytical optimal impact angle control guidance law considering time-varying velocity. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
  34. Xiangxiang Li, Wanchun Chen, Zhongyuan Chen, Heng Hua Shi (2025). Modified circular curve-based impact angle control guidance. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
  35. Jia Hong Zheng, Wanchun Chen, Qi Yu (2025). Multidisciplinary Design Optimization for Launch Vehicle with Solid Motors Based on Sensitivity Analysis. Lecture notes in electrical engineering.DOI
  36. Jiacheng Deng, Wanchun Chen, Xuehe Zheng, Shilei Zhao, Peng Zeng, Chao Wang, Liang Yang (2025). Three-Dimensional Generalized Nominal Effort Miss Guidance Law in Endo-Atmosphere Boost Phase. Lecture notes in electrical engineering.DOI
  37. 王鹏，赵石磊，陈万春（2024）. 基于可达区在线预测的GPI中制导协同拦截策略. 《北京航空航天大学学报》.
  38. 侯成林，许元男，陈万春，孟偲（2024）. 基于FlightSim和PyQt的电视制导系统仿真. 《飞行力学》.
  39. 徐翔，陈万春，杨良（2024）. 拦截弹非线性在线最优中制导方法研究. 《飞行力学》.
  40. 陈万春，陈中原，龚晓鹏（2024）. 智能机动突防策略研究进展. 《飞行力学》.
  41. 雷文贵，周浩，陈万春（2024）. 基于Guass伪谱法的空空导弹中制导方法研究. 《飞行力学》.
  42. 张天佑，陈万春，周韬（2024）. 高速再入飞行器跟踪制导方法对比研究. 《飞行力学》.
  43. 李诚，陈万春，刘小明（2024）. 最大射程滑翔在线制导方法研究. 《飞行力学》.
  44. 陈万春，袁文婕，于琦，刘小明，徐增（2024）. 低信息条件下的机载拦截武器目标分类轨迹预报方法研究. 《空天防御》.
  45. 王楠翔，陈万春，王鹏（2024）. 基于摄动法考虑高度影响的二维末段解析解. 《飞行力学》.
  46. 郑佳，陈万春，于琦（2024）. 导弹通用模型架构数字配装及参数灵敏度分析. 《飞行力学》.
  47. Xiang Li, Wan-Chun Chen, Qiang Sun, Jie Gao, Huiguang Zhao, Liang Yang (2024). Multi-phase trajectory optimization of space-based kinetic impactors for asteroid defense with multi-constraint. Advances in Space Research.DOI
  48. Wengui Lei, Wan-Chun Chen, Liang Yang, Xiaopeng Gong (2024). Singular optimal control of ascent stage for a surface-to-air missile. Chinese Journal of Aeronautics.DOI
  49. Zhaowei Yu, Wanchun Chen, Wenbin Yu (2024). Analytical solution for the skip trajectory of hypersonic vehicles with time-varying aerodynamic coefficients. Journal of Physics Conference Series.DOI
  50. Zhaowei Yu, Zhaowei Yu, Wanchun Chen, Wenbin Yu (2024). Analytical trajectory prediction of high-eccentricity spacecraft transfer orbits considering J2 perturbation. Aerospace Science and Technology.DOI
  51. Qi Hui Yu, Wanchun Chen, Wenbin Yu (2024). Approximate analytical solutions for three-dimensional ascent trajectory of a solid-fuel launch vehicle with time-varying mass flow rate. Chinese Journal of Aeronautics.DOI
  52. Jinyang WANG, Wanchun Chen, Liang YANG, Xiaopeng GONG (2024). An optimal midcourse guidance method for dual pulse air-to-air missiles using linear Gauss pseudospectral model predictive control method. Chinese Journal of Aeronautics.DOI
  53. Qing Li, Wanchun Chen, Zhongyuan Chen, Jinchuan Hu (2024). Jamming effect analysis of point-source infrared decoy on infrared spin-scan seeker. International Conference on Automation and Computing (ICAC).DOI
  54. Xiaopeng Gong, Wanchun Chen, Wengui LEI, Jinyang Wang, Zhongyuan Chen, Yunyun Li (2024). Analytical game strategies for active UAV defense considering response delays. Defence Technology.DOI
  55. Xiaopeng Gong, Wanchun Chen, Zhongyuan Chen (2024). Cooperative Integrated Guidance and Control for Active Target Protection in Three-Player Conflict. Actuators.DOI
  56. Xiaopeng Gong, Wanchun Chen, Zhongyuan Chen, Wenjie Yuan (2024). Closed-Form Solutions of Miss Distance for Higher-Order Guidance System. IEEE Transactions on Aerospace and Electronic Systems.DOI
  57. Xiangxiang Li, Wanchun Chen, Zhongyuan Chen, Xinrui Xu (2024). A Climb-and-dive Guidance Law with the Altitude Constraint. International Journal of Aeronautical and Space Sciences.DOI
  58. Xiangxiang Li, Wanchun Chen, Zhongyuan Chen, Heng Hua Shi (2024). Generalized circular impact time guidance. Aerospace Science and Technology.DOI
  59. Xiaopeng Gong, Wanchun Chen, Zhongyuan Chen (2024). Active Target Defense Differential Game: An Integrated Guidance and Control Approach. International Conference on Automation and Computing (ICAC).DOI
  60. Nanxiang Wang, Wanchun Chen, Zhongyuan Chen (2024). Catenary-based Impact Time and Angle Control Guidance. International Conference on Automation and Computing (ICAC).DOI
  61. Peng Wang, Wanchun Chen, Zhongyuan Chen, Jinchuan Hu (2024). Field-of-view constrained impact time control guidance considering time-varying velocity. International Conference on Automation and Computing (ICAC).DOI
  62. Chenglong Luo, Yuannan Xu, Wanchun Chen, Zhongyuan Chen, Xinrui Xu (2024). Adaptive Parameter Tuning Method for the Pulse-Width Pulse-Frequency modulator of Exoatmosphere Kill Vehicle Based on Reinforcement Learning. International Conference on Automation and Computing (ICAC).DOI
  63. 许昱，贺峥光，薛鹏飞，陈万春，陈峰（2023）. 基于热响应特性的高速飞行器轨迹设计与制导. 《航空学报》.
  64. 周浩，刘小明，陈万春（2023）. “弹道学与动态分析”课程教学改革探索. 《教育教学论坛》.
  65. 赵石磊，陈万春，杨良，冯卓（2023）. 大气层内助推段广义标控脱靶量解析制导律. 《系统工程与电子技术》.
  66. Wentao Qu, Wenbin Yu, Wanchun Chen (2023). Tensorial-formulation-based method for modeling of flight dynamics with generalized coordinates. Aerospace Science and Technology.DOI
  67. Xiangxiang Li, Wanchun Chen, Zhongyuan Chen, Heng Hua Shi (2023). A Guidance Law with Both Impact Time and Impact Angle Constraints Based on Circular Guidance. International Conference on Mechanical and Aerospace Engineering.DOI
  68. Jin Yang, Wenbin Yu, Wanchun Chen, Bo Liao, Hengwei Zhu (2023). Chebyshev-series solutions for nonlinear systems with hypersonic gliding trajectory example. Aerospace Science and Technology.DOI
  69. Qi Hui Yu, Wanchun Chen, Wenbin Yu (2023). Approximate Analytical Solutions for Launch-Vehicle Ascent Trajectory. IEEE Transactions on Aerospace and Electronic Systems.DOI
  70. Xiaopeng Gong, Wanchun Chen, Zhongyuan Chen (2023). Singular-Perturbation-based Intelligent Midcourse Guidance for Air-to-Air Missiles Equipped with Dual-Pulse Motor. International Conference on Mechanical and Aerospace Engineering.DOI
  71. Jin Yang, Wenbin Yu, Wanchun Chen, Wanqing Zhang (2023). Analytical Entry Guidance with Waypoint Constraints. International Conference on Mechanical and Aerospace Engineering.DOI
  72. Yachen Hou, Wenbin Yu, Wanchun Chen (2023). A Celestial Navigation Method for Endo-atmospheric Flight Vehicle Using Starlight Refraction. International Conference on Mechanical and Aerospace Engineering.DOI
  73. Xiaopeng Gong, Wanchun Chen, Zhongyuan Chen (2023). Intelligent Game Strategies in Target-Missile-Defender Engagement Using Curriculum-Based Deep Reinforcement Learning. Aerospace.DOI
  74. Qing Li, Wanchun Chen, Zhongyuan Chen, Zhongyuan Chen, Xinrui Xu (2023). Jamming effect analysis and reticle parameter identification of infrared spin-scan seeker under dynamic engagement environment. Infrared Physics & Technology.DOI
  75. Zhongyuan Chen, Xiaoming Liu, Wanchun Chen (2023). Three-dimensional event-triggered fixed-time cooperative guidance law against maneuvering target with the constraint of relative impact angles. Journal of the Franklin Institute.DOI
  76. Xiangxiang Li, Wanchun Chen, Zhongyuan Chen, Shen Zhang (2023). An Impact Angle Control Guidance via Self-restrained Look Angle Shaping. Lecture notes in electrical engineering.DOI
  77. 程涛，周浩，董晓飞，陈万春（2022）. 多飞行器突防打击一体化微分对策制导律设计. 《北京航空航天大学学报》.
  78. 王鹏，陈万春，陈中原（2022）. 视场约束下攻击角度及时间控制三维协同制导. 《战术导弹技术》.
  79. 龚晓鹏，陈万春，陈中原（2022）. 基于深度强化学习的三体对抗博弈策略研究. 《战术导弹技术》.
  80. 王洲强，陈万春，陈中原（2022）. 基于双层自适应MOEA/D的多阶段武器目标分配方法. 《战术导弹技术》.
  81. 陈万春（2022）. 高超声速飞行器平稳滑翔动力学与制导（英）.
  82. Wenbin Yu, Jin Yang, Wanchun Chen, Hengwei Zhu (2022). Analytical trajectory solutions for atmospheric pull-up phase of interplanetary return flight. Acta Astronautica.DOI
  83. Zonggui Zheng, Chongchong Wang, Xiangdong Sun, Liang Yang, Wanchun Chen (2022). Entry Guidance with No-Fly Zone Avoidance for Hypersonic Glide Vehicle. Lecture notes in electrical engineering.DOI
  84. Wei Zhao, Wanchun Chen, YaNa Wang, Xianfeng Zhang (2022). Path Planning Using Improved RRT for UAV in Narrow Passage Space with Timing Constraints. Lecture notes in electrical engineering.DOI
  85. Yang Li, Wanchun Chen, Liang Yang (2022). Linear Pseudospectral Method with Chebyshev Collocation for Optimal Control Problems with Unspecified Terminal Time. Aerospace.DOI
  86. Yang Li, Wanchun Chen, Liang Yang (2022). Optimal guidance method based on conjugate gradient method and pseudospectral method. Journal of Physics Conference Series.DOI
  87. Shilei Zhao, Wanchun Chen, Liang Yang, Minghao Wang (2022). Optimal midcourse guidance law for the exo-atmospheric interceptor with solid-propellant booster. Aerospace Science and Technology.DOI
  88. Shilei Zhao, Wanchun Chen, Liang Yang (2022). Endoatmospheric Ascent Optimal Guidance with Analytical Nonlinear Trajectory Prediction. International Journal of Aerospace Engineering.DOI
  89. Xiangxiang Li, Wanchun Chen, Zhongyuan Chen, Ting Wang, Heng Hua Shi (2022). Fixed-Time Circular Impact-Time Guidance with Look Angle Constraint. Aerospace.DOI
  90. Xiaopeng Gong, Wanchun Chen, Zhongyuan Chen (2022). All-aspect attack guidance law for agile missiles based on deep reinforcement learning. Aerospace Science and Technology.DOI
  91. Yang Li, Wanchun Chen, Hao Zhou, Liang Yang (2021). Gradient Method for Solving Multisystem Integrated Optimal Control Problem With Undetermined Terminal Time. Ieee Systems Journal, Vol. 150, No. 20.DOI
  92. 张荣升，陈万春（2021）. THAAD增程型拦截弹预测制导方法. 《北京航空航天大学学报》.DOI
  93. 陈中原，韦文书，陈万春（2021）. 基于强化学习的多发导弹协同攻击智能制导律. 《兵工学报》.
  94. 张晚晴，余文斌，李静琳，陈万春（2021）. 基于纵程解析解的飞行器智能横程机动再入协同制导. 《兵工学报》.
  95. 姚禹正，余文斌，杨立军，陈万春（2021）. 多导弹协同制导技术综述. 《空天技术》.DOI
  96. Wenbin Yu, Jin Yang, Wanchun Chen (2021). Entry Guidance Based on Analytical Trajectory Solutions. IEEE Transactions on Aerospace and Electronic Systems.DOI
  97. Wenbin Yu, Jin Yang, Wanchun Chen, Bo Liao, Hengwei Zhu (2021). Analytical trajectory prediction for near-first-cosmic-velocity atmospheric gliding using a perturbation method. Acta Astronautica.DOI
  98. Shilei Zhao, Wanchun Chen, Liang Yang (2021). Optimal Guidance Law with Impact-Angle Constraint and Acceleration Limit for Exo-Atmospheric Interception. Aerospace.DOI
  99. Yang Li, Wanchun Chen, Liang Yang (2021). Successive Chebyshev pseudospectral convex optimization method for nonlinear optimal control problems. International Journal of Robust and Nonlinear Control.DOI
  100. Yang Li, Wanchun Chen, Liang Yang (2021). Multistage Linear Gauss Pseudospectral Method for Piecewise Continuous Nonlinear Optimal Control Problems. IEEE Transactions on Aerospace and Electronic Systems.DOI
  101. Zhongyuan Chen, Wanchun Chen, Xiaoming Liu, Cheng Jin (2021). Three-dimensional fixed-time robust cooperative guidance law for simultaneous attack with impact angle constraint. Aerospace Science and Technology.DOI
  102. 王亚帆，周韬，陈万春，赫泰龙（2020）. 基于脱靶量级数解的最优机动突防策略. 《北京航空航天大学学报》.DOI
  103. 孙建波，潘幸华，杨良，陈万春，赵育善（2020）. 滑翔飞行器线性伪谱模型预测控制三维轨迹规划. 《红外与激光工程》.
  104. Jian-Bo Sun, Xing-Hua Pan, Liang Yang, Wan-Chun Chen, Yu-Shan Zhao (2020). 3D trajectory planning for gliding vehicle using linear pseudospectral model predictive control. Infrared and Laser Engineering.DOI
  105. Wenbin Yu, Wanchun Chen (2020). High-Accuracy Approximate Solutions for Hypersonic Gliding Trajectory With Large Lateral Maneuvering Range. IEEE Transactions on Aerospace and Electronic Systems.DOI
  106. Hao Zhou, Tao Cheng, Xiaoming Liu, Wanchun Chen (2020). Three-Dimensional Geometric Descent Guidance With Impact Angle Constraint. IEEE Access.DOI
  107. Zhongyuan Chen, M. Reza Emami, Wanchun Chen (2020). Connectivity Preservation and Obstacle Avoidance in Small Multi-Spacecraft Formation with Distributed Adaptive Tracking Control. Journal of Intelligent & Robotic Systems.DOI
  108. Wanqing Zhang, Wanchun Chen, Wenbin Yu (2020). Analytical solutions to three-dimensional hypersonic gliding trajectory over rotating Earth. Acta Astronautica.DOI
  109. Mengya Gao, Wanchun Chen, Wenbin Yu (2020). Analytical-Solution-Based Autopilot Design for Airdrop of Cruise Missile Equiped with Parachute. International Conference on Universal Village (UV).DOI
  110. Yang Li, Wanchun Chen, Hao Zhou, Liang Yang (2020). Conjugate gradient method with pseudospectral collocation scheme for optimal rocket landing guidance. Aerospace Science and Technology.DOI
  111. 赫泰龙，陈万春，刘芳（2019）. 高超声速飞行器平稳滑翔弹道扰动运动伴随分析. 《北京航空航天大学学报》.DOI
  112. 魏东辉，程进，陈万春（2019）. 飞行器超低空飞行制导控制技术发展研究. 《战术导弹技术》.DOI
  113. 李章琳，刘小明，陈万春（2019）. 防空导弹雷达导引头性能指标对目标拦截的仿真分析. 《战术导弹技术》.
  114. Cheng Jin, Donghui Wei, Wanchun Chen, Wang Gao (2019). Monocular visual based obstacle distance estimation method for ultra-low altitude flight. IEEE International Conference on Unmanned Systems (ICUS).DOI
  115. Yijun Feng, Wanchun Chen, Liang Yang, Donghui Wei (2019). Optimal Terrain Following Trajectory Regeneration Using Linear Gauss Pseudo-Spectral Method. IEEE International Conference on Unmanned Systems (ICUS).DOI
  116. Yijun Feng, Wanchun Chen, Liang Yang, Donghui Wei (2019). An Optimal Terrain Following Trajectory Online Regeneration Method. IEEE Conference on Control Technology and Applications (CCTA).DOI
  117. Liang Yang, Jin Yang, Xiaoming Liu, Wanchun Chen, Hao Zhou (2019). Gradient method using pseudospectral collocation scheme for two-stage optimal control with an unspecified switching time. International Journal of Control.DOI
  118. Wanqing Zhang, Wanchun Chen, Wenbin Yu, Chaoyue Zhao (2019). Autonomous Entry Guidance based on 3-D Gliding Trajectory Analytical Solution.DOI
  119. Xingcai He, Wanchun Chen, Liang Yang (2019). An Intercept Guidance Law with Impact-Angle-Constrained Based on Linear Gauss Pseudospectral Model Predictive Control.DOI
  120. Wanchun Chen, Wenhao Du, William W. Hager, Liang Yang (2019). Bounds for integration matrices that arise in Gauss and Radau collocation. Computational Optimization and Applications.DOI
  121. Penglei Zhao, Wanchun Chen, Wenbin Yu (2019). Analytical solutions for longitudinal-plane motion of hypersonic skip-glide trajectory. Nonlinear Dynamics.DOI
  122. Liming Huang, Wanchun Chen (2019). Deep Learning Midcourse Guidance for Interceptor Missile. IEEE Information Technology, Networking, Electronic and Automation Control Conference (ITNEC).DOI
  123. Penglei Zhao, Wanchun Chen, Wenbin Yu (2019). Optimal perturbation guidance with constraints on terminal flight-path angle and angle of attack. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
  124. Peng Wang, Wanchun Chen, Xiaoming Liu, Zhongyuan Chen (2019). Design of Hardware-in-the-loop Simulation System based on RTX and FlightSim™. IEEE International Conference on Cybernetics and Intelligent Systems and IEEE Conference on Robotics, Automation and Mechatronics (CIS-RAM).DOI
  125. Zhaowei Yu, Wanchun Chen, Zhongyuan Chen, Xiaoming Liu (2019). TV Guidance Simulation Platform Based on Deep Learning. IEEE International Conference on Cybernetics and Intelligent Systems and IEEE Conference on Robotics, Automation and Mechatronics (CIS-RAM).DOI
  126. Zhongyuan Chen, Wanchun Chen, Xiaoming Liu, Chuang Song (2018). Development of an educational interactive hardware-in-the-loop missile guidance system simulator. Computer Applications In Engineering Education, Vol. 260, No. 2.DOI
  127. 赫泰龙，陈万春，周浩（2018）. 高阶线性比例制导系统脱靶量幂级数解. 《航空学报》.
  128. 谢经纬，陈万春（2018）. 大气层外拦截弹建模与攻防效能分析. 《北京航空航天大学学报》.
  129. 冯逸骏，陈万春，杨良（2018）. 线性伪谱模型预测能量最优姿态机动控制方法. 《北京航空航天大学学报》.
  130. 李伟喆，陈万春（2018）. 双脉冲中程空空导弹弹道优化. 《战术导弹技术》.
  131. 祝姣，陈万春，马洪忠，杨志红（2018）. 考虑输入饱和的高超声速飞行器反步法控制. 《哈尔滨工业大学学报》.
  132. 李静琳，陈万春，闵昌万（2018）. 高超末段机动突防/精确打击弹道建模与优化. 《北京航空航天大学学报》.
  133. 尤志鹏，周韬，陈万春（2018）. 基于IMM算法的容错气动参数辨识. 《飞行力学》.
  134. 裴宇肖，明宝印，郭军，陈万春（2018）. 近距格斗空空导弹Up-Look模式大离轴角目标截获研究. 《弹箭与制导学报》.
  135. Yijun Feng, Wan-Chun Chen, Liang Yang (2018). Fuel-optimal attitude maneuver using linear pseudo-spectral model predictive control method.DOI
  136. Wenbin Yu, Wanchun Chen, Zhiguo Jiang, Wanqing Zhang, Penglei Zhao (2018). Analytical entry guidance for coordinated flight with multiple no-fly-zone constraints. Aerospace Science and Technology.DOI
  137. Wanqing Zhang, Wanchun Chen, Wenbin Yu (2018). Entry guidance for high-L/D hypersonic vehicle based on drag-vs-energy profile. ISA Transactions.DOI
  138. Liang Yang, Xiaoming Liu, Wanchun Chen, Hao Zhou (2018). Autonomous entry guidance using Linear Pseudospectral Model Predictive Control. Aerospace Science and Technology.DOI
  139. Hao Zhou, Elsayed M. Khalil, Tawfiqur Rahman, Wanchun Chen (2018). Waypoints Following Guidance for Surface-to-Surface Missiles. International Journal of Aeronautical and Space Sciences.DOI
  140. Zhongyuan Chen, Wanchun Chen, Xiaoming Liu, Chuang Song (2018). Fault-Tolerant Optical Flow Sensor/SINS Integrated Navigation Scheme for MAV in a GPS-Denied Environment. Journal of Sensors.DOI
  141. Liang Yang, Wanchun Chen, Xiaoming Liu, Hao Zhou (2017). Robust entry guidance using multi-segment linear pseudospectral model predictive control. Journal Of Systems Engineering And Electronics, Vol. 280, No. 10.DOI
  142. 祝姣，陈万春，马洪忠，杨志红（2017）. 带鸭翼的弹性高超声速飞行器非线性控制. 《固体火箭技术》.
  143. Wenbin Yu, Wanchun Chen, Zhiguo Jiang, Ming Liu, Yang Ding, Ming Zhu Yang, Yajie Ge (2017). Analytical entry guidance for no-fly-zone avoidance. Aerospace Science and Technology.DOI
  144. Xie Jingwei, Wanchun Chen (2017). Switching logic design for divert and attitude control system of exoatmospheric kill vehicle. IEEE International Conference on Cybernetics and Intelligent Systems and IEEE Conference on Robotics, Automation and Mechatronics (CIS-RAM).DOI
  145. Penglei Zhao, Wanchun Chen, Wenbin Yu (2017). Guidance law for intercepting target with multiple no-fly zone constraints. The Aeronautical Journal.DOI
  146. Wenbin Yu, Wanchun Chen, Zhiguo Jiang, Hao Zhou, Xiaoming Liu, Ming Liu (2017). Analytical entry guidance based on pseudo-aerodynamic profiles. Aerospace Science and Technology.DOI
  147. HE Tailong, Wanchun Chen (2017). A new interpretation of adjoint method in linear time-varying system analysis. IEEE International Conference on Cybernetics and Intelligent Systems and IEEE Conference on Robotics, Automation and Mechatronics (CIS-RAM).DOI
  148. Zhongyuan Chen, Xiaoming Liu, Wanchun Chen (2017). Design of Real-Time Hardware-in-the-Loop TV Guidance System Simulation Platform. International Journal of Aerospace Engineering.DOI
  149. 胡锦川，张晶，陈万春（2016）. 高超声速飞行器平稳滑翔弹道解析解及其应用. 《北京航空航天大学学报》.
  150. 魏东辉，陈万春，李娜英，徐骋（2016）. 智能变形导弹变形机理及协调控制机制研究. 《战术导弹技术》.
  151. 马树微，李静琳，陈曦，陈万春（2016）. 多级固体运载火箭分级多学科设计优化. 《北京航空航天大学学报》.
  152. 祝姣，陈万春，马洪忠，杨志红（2016）. 高超声速飞行器弹性振动抑制方法研究. 《战术导弹技术》.
  153. Wan-Chun Chen, Peng-Lei Zhao (2016). Singular perturbation suboptimal guidance law with terminal ballistic inclined angle and attack angle constraints.
  154. Yang Liu, Wanchun Chen (2016). Multidisciplinary design optimization of launch vehicle using objective coordination methodology. IEEE Advanced Information Management, Communicates, Electronic and Automation Control Conference (IMCEC).DOI
  155. Wenbin Yu, Wanchun Chen, Zhiguo Jiang, Xiaoming Liu, Hao Zhou (2016). Omnidirectional autonomous entry guidance based on 3-D analytical glide formulas. ISA Transactions.DOI
  156. Xiaoming Liu, Zhongyuan Chen, Wanchun Chen, Xiaolan Xing (2016). Multiple optical flow sensors aiding inertial systems for UAV navigation. UKACC International Conference on Control.DOI
  157. Wenhao Du, Hao Zhou, Wanchun Chen (2016). Trajectory optimization for agile-turn of vertically launched missile. IEEE International Conference on Mechatronics and Automation (ICMA).DOI
  158. Jinglin Li, Wanchun Chen, Changwan Min (2016). Steady glide reentry trajectory optimization with waypoint and no-fly zone constraints. IEEE International Conference on Mechatronics and Automation (ICMA).DOI
  159. Jingwei Meng, Wanchun Chen, Wenbin Yu (2016). Sub-optimal ground-strike guidance based on perturbation method. IEEE International Conference on Mechatronics and Automation (ICMA).DOI
  160. Heng Li, Wanchun Chen (2016). ALCM descending-phase guidance law including derivative of normal acceleration restriction. IEEE International Conference on Mechatronics and Automation (ICMA).DOI
  161. Wenbin Yu, Wanchun Chen, Liang Yang, Xiaoming Liu, Hao Zhou (2016). Optimal terminal guidance for exoatmospheric interception. Chinese Journal of Aeronautics.DOI
  162. Zidu Chen, Xiaoming Liu, Wanchun Chen, Tao Zhou (2016). State estimation of infrared target using particle filter.DOI
  163. Xiaoming Liu, Zhongyuan Chen, Wanchun Chen, Xiaolan Xing (2016). Motion estimation using optical flow sensors and rate gyros. IEEE International Conference on Mechatronics and Automation (ICMA).DOI
  164. 胡锦川，陈万春（2015）. 高超声速飞行器平稳滑翔弹道设计方法. 《北京航空航天大学学报》.
  165. Jinchuan Hu, Jinglin Li, Wanchun Chen (2015). Longitudinal characteristics of steady glide trajectory for hypersonic vehicle. International Conference on Control, Automation and Information Sciences (ICCAIS).DOI
  166. Jing Zhang, Liuqiu You, Wanchun Chen (2015). Boost-phase guidance with neural network for interception of ballistic missile. International Conference on Control, Automation and Information Sciences (ICCAIS).DOI
  167. Hao Zhou, Tawfiqur Rahman, Wanchun Chen (2015). Impact angle and impact velocity constrained terminal guidance for stationary target. Aircraft Engineering and Aerospace Technology.DOI
  168. Wenbin Yu, Wanchun Chen (2015). Entry guidance with real-time planning of reference based on analytical solutions. Advances in Space Research.DOI
  169. 张红文，张科南，陈万春（2014）. 带静态参数的高超声速飞行器轨迹优化算法. 《北京航空航天大学学报》.
  170. 刘小明，饶康麒，陈万春，孟庆春（2014）. 航天飞行器设计专业实验教学改革与实践. 《实验室研究与探索》.
  171. 杨良，郑宗贵，徐衡，陈万春，周浩（2014）. 多约束在线高斯伪谱末制导方法. 《弹道学报》.
  172. Fang Liu, Wei Mao, Jia-Qi Liu, Wan-Chun Chen (2014). Design of neural network base dynamic inversion compound controller.DOI
  173. Wenbin Yu, Wanchun Chen (2014). Trajectory-Shaping Guidance with final speed and load factor constraints. ISA Transactions.DOI
  174. Wenbin Yu, Wanchun Chen (2014). Guidance law with circular no-fly zone constraint. Nonlinear Dynamics.DOI
  175. Hao Zhou, Tawfiqur Rahman, Wanchun Chen (2014). Neural Network Assisted Inverse Dynamic Guidance for Terminally Constrained Entry Flight. The Scientific World JOURNAL.DOI
  176. Elsayed M. Khalil, Hao Zhou, Wanchun Chen (2014). Steepest-Ascent Revisited: Unconstrained Missile Trajectory. International Journal of Aerospace Engineering.DOI
  177. 顾家立，陈万春（2013）. 一种带导引头视角和落角约束的导引方法. 《宇航学报》.
  178. 杜政，王朝志，陈万春（2013）. 巡航导弹群突防舰载反导系统快速分析模型. 《北京航空航天大学学报》.
  179. 马树微，杜斌，陈万春（2013）. 基于代理模型的高超声速飞行器协同优化设计. 《北京航空航天大学学报》.
  180. 刘芳，陈万春（2013）. 应用Lyapunov方法分析自旋导弹动态逆控制器鲁棒性. 《北京航空航天大学学报》.
  181. Liang Yang, Hao Zhou, Wanchun Chen (2013). Application of linear gauss pseudospectral method in model predictive control. Acta Astronautica.DOI
  182. Hao Zhou, Tawfiqur Rahman, Danwei Wang, Wanchun Chen (2013). Onboard pseudospectral guidance for re-entry vehicle. Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering.DOI
  183. Wanchun Chen (2013). Fast terminal trajectory optimization for hypersonic spacecraft. Flight Dynamics.
  184. 覃天，陈万春，邢晓岚（2012）. 一种带落角约束的精确导引方法(英文). 《宇航学报》.
  185. 刘小明，陈万春，邢晓岚，殷兴良（2012）. 光流控制地形跟随与自动着陆. 《北京航空航天大学学报》.
  186. 韩英宏，陈万春（2012）. 新型快速传递对准方法. 《北京航空航天大学学报》.
  187. 宋愿赟，陈万春（2012）. 高精度快速趋近滑模变结构末端导引方法. 《北京航空航天大学学报》.
  188. 刘小明，陈万春，邢晓岚，殷兴良（2012）. 光流/惯导多传感器信息融合方法. 《北京航空航天大学学报》.
  189. 徐衡，陈万春（2012）. 满足多约束的主动段能量管理制导方法. 《北京航空航天大学学报》.
  190. 张科南，周浩，陈万春（2012）. 高超声速飞行器多约束多种机动突防模式弹道规划. 《弹道学报》.
  191. Ying-Hong Han, Wan-Chun Chen (2012). Analysis of Three Velocity Plus Attitude Matching Methods for Transfer Alignment.DOI
  192. Ying-Hong Han, Wan-Chun Chen (2012). New method for rapid transfer alignment.
  193. Jia-Li Gu, Wan-Chun Chen (2012). Optimal proportional navigation guidance based on generalized predictive control. International Conference on System Theory, Control and Computing.
  194. Wan-Chun Chen (2012). Reserch on the surrogate of model aerodynamic performance of cone derived waverider.
  195. Wan-Chun Chen (2012). PAC-3 interceptor 6DOF antimissile modeling and intercept simulation analysis.
  196. Han Yinghong, Chen Feng, Wanchun Chen (2012). Ballistic boost phase guidance using nominal effort miss steering.
  197. Guannan Liu, Zhou Hao, Wanchun Chen (2012). A study on the multiple-phrase reentry guidance method of hypersonic vehicle. Flight Dynamics.
  198. 乔清青，陈万春（2011）. 基于动态逆的空空导弹奇异摄动中制导律. 《北京航空航天大学学报》.
  199. 韩英宏，邢晓岚，陈万春（2011）. 空空导弹性能指标体系与评估方法. 《战术导弹技术》.
  200. 王烁，姜欢，李萍，陈万春（2011）. 乘波体MDO子学科动态代理建模方法. 《战术导弹技术》.
  201. 斗计华，余良盛，陈万春（2011）. 舰空导弹武器系统作战效能评估综述. 《现代防御技术》.
  202. 斗计华，陈万春，钟志通（2011）. 舰空导弹武器系统使用可靠性评估. 《系统工程与电子技术》.
  203. 覃天，陈万春，邢晓岚（2011）. 基于光流信息的圆弧偏置比例导引规律. 《北京航空航天大学学报》.
  204. Wenbin Yu, Wanchun Chen (2011). Guidance Scheme for Glide Range Maximization of a Hypersonic Vehicle. AIAA Guidance, Navigation, and Control Conference and Exhibit.DOI
  205. Heng Xu, Wanchun Chen (2011). An Energy Management Ascent Guidance Algorithm for Solid Rocket-Powered Launch Vehicles. AIAA International Space Planes and Hypersonic Systems and Technologies Conference.DOI
  206. Cai Yong, Wanchun Chen, Shiming Liu, Feng He (2011). State estimation of spiral maneuvering target and simulation of three-dimensional intercept. International Conference on Consumer Electronics, Communications and Networks (CECNet).DOI
  207. 张科南，陈万春（2010）. CFE方法在导弹发射动力学建模中的应用. 《北京航空航天大学学报》.
  208. 陈峰，肖业伦，陈万春（2010）. 基于需用速度增益曲面的大气层外超远程拦截导引方法. 《航空学报》.
  209. 刘恒军，姜欢，陈万春（2010）. 防空导弹动能杀伤多层弹道优化MDO算法应用. 《北京航空航天大学学报》.
  210. Wanchun Chen (2010). Maximum cross range trajectory optimization based on quasi-equilibrium glide conditions. Flight Dynamics.
  211. Ping Li, Wanchun Chen, Hao Zhou (2010). Quasi-equilibrium glide trajectory design of waverider-based hypersonic vehicle.DOI
  212. 李佳峰，姜欢，陈万春（2009）. 基于拟勒让德谱变换的防空导弹弹道优化. 《弹道学报》.
  213. 姜欢，周浩，陈万春，杨宝奎（2009）. 基于全局灵敏度方程的多层次弹道优化设计. 《北京航空航天大学学报》.
  214. 李佳峰，陈万春（2009）. 防空导弹最优弹道的协态估计优化算法. 《北京航空航天大学学报》.
  215. 李佳峰，陈万春（2009）. 带约束的高超声速飞行器最优弹道的数值算法. 《航空学报》.
  216. 邢立旦，陈万春，殷兴良（2009）. 最优/经典综合法设计直接力/气动力复合控制器. 《北京航空航天大学学报》.
  217. 陈峰，肖业伦，陈万春（2009）. 基于零控脱靶量的大气层外超远程拦截制导. 《航空学报》.
  218. Wanchun Chen (2009). Indirect Method for the Hypersonic Vehicle Maximum-Glide Problem. Flight Dynamics.
  219. Wanchun Chen (2009). Midcourse Trajectory Optimization Design for a Surface-to-Air Missile Based on Legendre Pseudospectral Method. Journal of Ballistics.
  220. 王进，陈万春，殷兴良（2008）. 具有脉冲姿控发动机的自旋导弹动态分析与控制设计. 《宇航学报》.
  221. 周浩，陈万春，殷兴良（2008）. 高超声速飞行器多段弹道优化设计. 《宇航学报》.
  222. 周国峰，王朝志，陈万春（2008）. 机动弹头引入段弹道优化设计. 《战术导弹技术》.
  223. 金光军，王朝志，陈万春（2008）. 激光引信启动点的简化计算模型. 《战术导弹技术》.
  224. 邢立旦，陈万春，殷兴良（2008）. 应用最优/经典综合设计法设计三回路BTT自动驾驶仪. 《宇航学报》.
  225. 陈峰，王育林，肖业伦，陈万春（2008）. 基于预测脱靶量的远程拦截速度增益导引. 《航空学报》.
  226. 周浩，陈万春，殷兴良（2008）. 高超声速飞行器多段弹道协作优化. 《北京航空航天大学学报》.
  227. 姜欢，周浩，陈万春，杨宝奎（2008）. 多层次法防空导弹弹道优化设计. 《北京航空航天大学学报》.
  228. 姜欢，周浩，周韬，陈万春，杨宝奎（2008）. 拦截TBM/ASM多层次弹道优化设计研究. 《宇航学报》.
  229. Wan-Chun Chen (2008). Calculation of the Number of Fragmentation Hitting on Target by Polynomial Fitting.
  230. 周浩，陈万春，殷兴良，刘洪甜（2007）. 高超声速飞行器时间最短弹道优化设计. 《弹道学报》.
  231. 王进，陈万春，殷兴良（2007）. 大气层内拦截弹脉冲姿控发动机快响应控制. 《北京航空航天大学学报》.
  232. Wan-Chun Chen (2007). Dynamic and Static Weapon-Target Assignments of Air Defense.
  233. 周浩，周韬，陈万春，殷兴良（2006）. 高超声速滑翔飞行器引入段弹道优化. 《宇航学报》.
  234. 周浩，陈万春，殷兴良（2006）. 基于matlab的飞行器并行MDO方法的研究与实现. 《宇航学报》.
  235. 周韬，黄运平，陈万春，殷兴良（2006）. 导弹质量矩控制技术建模与静态性能分析. 《宇航学报》.
  236. 周浩，陈万春，殷兴良（2006）. 高超声速飞行器滑行航迹优化. 《北京航空航天大学学报》.
  237. 李扬，陈万春（2006）. 高超声速飞行器BTT非线性控制器设计与仿真. 《北京航空航天大学学报》.
  238. Wan-Chun Chen (2006). The Research and Implementation of Flight Vehicle BLISS Distributed Platform.
  239. Hao Zhou, Wanchun Chen, Xingliang Yin (2006). Hypersonic vehicle trajectory design based on optimal control theory. Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE.DOI
  240. Lidan Xing, Wanchun Chen, Xingliang Yin (2006). The control system of hypersonic missile using state-dependent Riccati equation. Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIE.DOI
  241. 丁建超，王朝志，陈万春，鲁志刚（2005）. 反TBM导弹动能杆战斗部优化设计. 《战术导弹技术》.
  242. 王鹏，陈万春，殷兴良（2005）. 空空导弹大角度姿态反作用喷气控制. 《航空学报》.
  243. Wan-Chun Chen (2005). Analysis of Network Centric Air Defense Operation Using Stochastic Service System Theory.
  244. 王鹏，陈万春，邹晖，殷兴良（2004）. 空空导弹敏捷转弯反作用喷气控制研究. 《北京航空航天大学学报》.
  245. 邹晖，陈万春，王鹏，殷兴良（2004）. 敏捷导弹气动力/侧向推力复合控制特性分析研究. 《北京航空航天大学学报》.
  246. 王鹏，陈万春，殷兴良（2004）. 空空导弹大角度姿态推力矢量控制研究. 《宇航学报》.
  247. 邢晓岚，陈万春，尹健（2003）. 任意两个动坐标系中张量的运动描述间的关系. 《北京航空航天大学学报》.
  248. 陈万春，骆冬伶（2001）. FL-7风洞M数的模糊控制方法. 《实验流体力学》.
  249. 陈万春，肖业伦，杨健敏（2001）. 矢阵及其在目标状态测量建模中的应用. 《宇航学报》.
  250. 陈万春，赵丽红，刘佳琪，黄皎仁（1999）. 反战术弹道导弹总体优化设计研究. 《北京航空航天大学学报》.
  251. 聂蓉梅，夏人伟，陈万春（1999）. 飞行器总体设计中主要参数的神经网络估算. 《北京航空航天大学学报》.
  252. 陈万春，肖业伦（1997）. 矢阵与四元数的关系及其在飞行力学中的应用. 《宇航学报》.
  253. 陈万春，高和（1996）. 防空导弹总体方案设计的系统分析. 《系统工程理论与实践》, Vol. 16, No. 4.下载原文
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书籍章节

  1. Xiang Li, Zhishi Chen, Bohao Li, Zheng Liu, Jiacheng Deng, Wanchun Chen, Liang Yang (2026). A Guidance Law with Impact Time and Angle Constraints Under Nonlinear Varying Velocity Using Pseudospectral Online Planning. Advances in transdisciplinary engineering.DOI
  2. Tianyou Zhang, Wanchun Chen, Liang Yang (2025). Neighboring Extremal Method Using Gauss Pseudospectral Collocation Scheme for Trajectory Optimization. Advances in transdisciplinary engineering.DOI
  3. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). 3-D Reentry Guidance with Real-Time Planning of Reference using New Analytical Solutions Based on Spectral Decomposition Method. Springer eBooks.DOI
  4. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Analytical Solutions of Steady Glide Reentry Trajectory in Three Dimensions and Their Application to Trajectory Planning. Springer eBooks.DOI
  5. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Direct Method for Gliding Trajectory Optimization Problem. Springer eBooks.DOI
  6. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Omnidirectional Autonomous Reentry Guidance Based on 3-D Analytical Glide Formulae Considering Influence of Earth’s Rotation. Springer eBooks.DOI
  7. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Mathematical Description of Glide-Trajectory Optimization Problem. Springer eBooks.DOI
  8. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Trajectory Damping Control Technique for Hypersonic Glide Reentry. Springer eBooks.DOI
  9. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Linear Pseudospectral Reentry Guidance with Adaptive Flight Phase Segmentation and Eliminating General Nominal Effort Miss Distance. Springer eBooks.DOI
  10. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Concept of Steady Glide Reentry Trajectory and Stability of Its Regular Perturbation Solutions. Springer eBooks.DOI
  11. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Analytical Steady-Gliding Guidance Employing Pseudo-Aerodynamic Profiles. Springer eBooks.DOI
  12. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Linear Pseudospectral Guidance Method for Eliminating General Nominal Effort Miss Distance. Springer eBooks.DOI
  13. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Trajectory-shaping Guidance with Final Speed and Load Factor Constraints. Springer eBooks.DOI
  14. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Introduction. Springer eBooks.DOI
  15. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Mathematical Fundamentals. Springer eBooks.DOI
  16. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Singular Perturbation Guidance of Hypersonic Glide Reentry. Springer eBooks.DOI
  17. Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang (2020). Indirect Approach to the Optimal Glide Trajectory Problem. Springer eBooks.DOI

研究方向

航空航天科学与工程武器工业与军事技术化学物理学

此主页由公开资料整理，尚未经学者本人认领。