[1] WANG X, SHI P, WEN C. Design of Parameter-self-tuning Controller Based on Reinforcement Learning for Tracking Non-cooperative Targets in Space[J]. IEEE Transactions on Aerospace and Electronic Systems, 2020: 1.
[2] CHEN Q, QIAO D, WEN C. Orbital Element Reachable Set After Gravity Assists of Planets in Elliptical Orbits[J]. Journal of Guidance, Control, and Dynamics, 2020: 1–9.
[3] WEN C, MA J. Reachable domain for satellite relative motion along elliptic orbit with uncertainty and process noise[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2020: 0954410019900726.
[4] WANG X, SHI P, WEN C. An Algorithm of Reinforcement Learning for Maneuvering Parameter Self-Tuning Applying in Satellite Cluster[J]. Mathematical Problems in Engineering, 2020, 2020: 1836159.
[5] CHEN Q, QIAO D, WEN C. Reachable Domain of Spacecraft After a Gravity-Assist Flyby[J]. Journal of Guidance, Control, and Dynamics, 2019, 42(4): 931–940.
[6] WEN. C, GAO. Y, SHI. H. Three-dimensional relative reachable domain with initial state uncertainty in Gaussian distribution[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, 233(5): 1555–1570.
[7] WANG X, SHI P, WEN C. Adaptive control of coupled position and attitude for tracking characteristic point of disabled satellite[J]. ZhongguoKongjianKexueJishu/Chinese Space Science and Technology, 2018, 38(1).
[8] 王逍, 温昶煊, 赵育善等. 翻滚目标安全走廊内的碰撞可能性判断方法[J]. 哈尔滨工业大学学报, 2018(4).
[9] WEN C, PENG C, GAO Y. Reachable domain for spacecraft with ellipsoidal Delta-V distribution[J]. Astrodynamics, 2018, 2(3): 265–288.
[10] LEI B, SHI P, WEN C. Gain-Scheduling Attitude Control for Complex Spacecraft Based on HOSVD[J]. Journal of Dynamic Systems, Measurement, and Control, 2018.
[11] WEN C, GURFIL P. Guidance, navigation and control for autonomous R-bar proximity operations for geostationary satellites[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2016, 231(3): 452–473.
[12] WEN C, GURFIL P. Relative Reachable Domain for Spacecraft with Initial State Uncertainties[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(3): 462–473.
[13] WEN C, GURFIL P. Modeling Early Medium-Term Evolution of Debris Clouds Using the Reachable Domain Method[J]. Journal of Guidance, Control, and Dynamics, 2016, 39(12): 2649–2660.
[14] WEN C, ZHANG H, GURFIL P. Orbit Injection Considerations for Cluster Flight of Nanosatellites[J]. Journal of Spacecraft and Rockets, 2015, 52(1): 196–208.
[15] WEN C, ZHAO Y, SHI P. Derivative Analysis and Algorithm Modification of Transverse-Eccentricity-Based Lambert Problem[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(4): 1195–1201.
[16] WEN C, ZHAO Y, SHI P. Orbital Accessibility Problem for Spacecraft with a Single Impulse[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(4): 1260–1271.
[17] WEN C, ZHAO Y, SHI P. Precise Determination of Reachable Domain for Spacecraft with Single Impulse[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(6): 1767–1779.
[18] WEN C, ZHAO Y, LI B. Solving the Relative Lambert’s Problem and Accounting for Its Singularities[J]. Acta Astronautica, 2014, 97(0): 122–129.
