梁子璇

2011年09月-2016年07月，在北京航空航天大学获得导航、制导与控制专业博士学位
2014年11月-2015年11月，在加州大学欧文分校访学（航空航天工程专业，联合培养博士）
2007年09月-2011年07月，在北京航空航天大学获得自动化专业学士学位　

1、《航空学报》《Chinese Journal of Aeronautics》青年编委
2、《深空探测学报（中英文）》青年编委
3、中国宇航学会青年科学家俱乐部副主席
4、中国宇航学会深空探测技术专业委员会学术秘书兼办公室主任
5、中国指挥与控制学会集群智能与协同控制专业委员会委员
6、国家自然科学基金项目函评专家
7、中国博士后科学基金项目函评专家

[1]Lateral entry guidance with terminal time constraint. IEEE Transactions on Aerospace and Electronic Systems, 2023, 59 (3): 2544-2553

[2]Closed-loop guidance for asteroid landing using stability-related control and three-dimensional convex curvature constraints. IEEE Transactions on Aerospace and Electronic Systems, 2023, 59 (3): 2807-2822

[3]Guidance for precision landing on asteroid using active hopping trajectory. Acta Astronautica, 2022, 198: 320-328.

[4]Constrained predictor-corrector guidance via bank saturation avoidance for low L/D entry vehicles. Aerospace Science and Technology, 2021, 109: 106448.

[5]Rapid generation of the fuel-optimal trajectory for landing on irregularly shaped asteroids. IEEE Transactions on Aerospace and Electronic Systems, 2021, 57 (6): 4390-4400.

[6]Entry guidance with terminal approach angle constraint. Aerospace Science and Technology, 2020, 102:  105876.

[7]Precision guidance for Mars entry with a supersonic inflatable aerodynamic decelerator. Journal of Guidance, Control, and Dynamics, 2019, 42 (7): 1571-1578.

[8]Evolved atmospheric entry corridor with safety factor. Acta Astronautica, 2018, 143: 82-91.

[9]Tentacle-based guidance for entry flight with no-fly zone constraint. Journal of Guidance, Control, and Dynamics, 2018, 41 (4): 991-1000.

[10]Lateral entry guidance with no-fly zone constraint. Aerospace Science and Technology, 2017, 60: 39-47.

[11]Distributed cooperative guidance for multiple missiles with fixed and switching communication topologies. Chinese Journal of Aeronautics, 2017, 30 (4): 1570-1581.

[12]Virtual terminal-based adaptive predictor-corrector entry guidance. Journal of Aerospace Engineering, 2017, 30 (4): 04017013.

[13]Decoupled three-dimensional entry trajectory planning based on maneuver coefficient. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2017, 231 (7): 1281–1292.

[14]Mars entry guidance based on an adaptive reference drag profile. Advances in Space Research, 2017, 60 (3): 692-701.

[15]Waypoint constrained guidance for entry vehicles. Aerospace Science and Technology, 2016, 52: 52-61.

[16]Onboard planning of constrained longitudinal trajectory for reusable launch vehicles in terminal area. Advances in Space Research, 2016, 57 (3): 742-753.

[17]小天体柔性附着技术. 宇航学报, 2023, 44 (6): 805-816

[18]带落速落角约束的高超声速飞行器俯冲轨迹规划方法. 宇航学报, 2022, 43 (8): 1052-1060.

[19]不规则小行星附着可达区生成方法. 宇航学报, 2021, 42 (12): 1548-1556.

[20]高超声速目标拦截末段交战窗口快速生成方法[J]. 宇航学报, 2021, 42 (3): 333-343

网址：梁子璇 https://mxgxt.com/news/view/362139

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