梁子璇 - 北京理工大学

个人简介

教育经历 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　工作经历 2018年12月至今，北京理工大学，教师 2016年11月-2018年12月，北京航空航天大学，博士后获奖情况国家级青年人才中国科协“青年人才托举工程”入选者中国宇航学会首届“卓越托举人才” 部级科技进步一等奖

研究领域

行星进入与着陆制导深空自主导航与制导多约束飞行轨迹优化

近期论文

查看导师最新文章（温馨提示：请注意重名现象，建议点开原文通过作者单位确认）

Lateral entry guidance with terminal time constraint. IEEE Transactions on Aerospace and Electronic Systems, 2023, 59 (3): 2544-2553 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 Guidance for precision landing on asteroid using active hopping trajectory. Acta Astronautica, 2022, 198: 320-328. Constrained predictor-corrector guidance via bank saturation avoidance for low L/D entry vehicles. Aerospace Science and Technology, 2021, 109: 106448. 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. Entry guidance with terminal approach angle constraint. Aerospace Science and Technology, 2020, 102: 105876. Precision guidance for Mars entry with a supersonic inflatable aerodynamic decelerator. Journal of Guidance, Control, and Dynamics, 2019, 42 (7): 1571-1578. Evolved atmospheric entry corridor with safety factor. Acta Astronautica, 2018, 143: 82-91. Tentacle-based guidance for entry flight with no-fly zone constraint. Journal of Guidance, Control, and Dynamics, 2018, 41 (4): 991-1000. Lateral entry guidance with no-fly zone constraint. Aerospace Science and Technology, 2017, 60: 39-47. Distributed cooperative guidance for multiple missiles with fixed and switching communication topologies. Chinese Journal of Aeronautics, 2017, 30 (4): 1570-1581. Virtual terminal-based adaptive predictor-corrector entry guidance. Journal of Aerospace Engineering, 2017, 30 (4): 04017013. 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. Mars entry guidance based on an adaptive reference drag profile. Advances in Space Research, 2017, 60 (3): 692-701. Waypoint constrained guidance for entry vehicles. Aerospace Science and Technology, 2016, 52: 52-61. Onboard planning of constrained longitudinal trajectory for reusable launch vehicles in terminal area. Advances in Space Research, 2016, 57 (3): 742-753. 小天体柔性附着技术. 宇航学报, 2023, 44 (6): 805-816 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. 不规则小行星附着可达区生成方法. 宇航学报, 2021, 42 (12): 1548-1556. 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

学术兼职

《航空学报》《Chinese Journal of Aeronautics》青年编委《深空探测学报（中英文）》青年编委中国宇航学会青年科学家俱乐部副主席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国家自然科学基金项目函评专家中国博士后科学基金项目函评专家