基本信息
电话: 0755-26915894
地址: 哈尔滨工业大学(深圳)L栋信息楼0719
邮箱: yuechengfei@hit.edu.cn
科研领域: 主要从事新概念航天器设计、航天器动力学与控制、空间机器人系统等研究。
个人简介
岳程斐,男,汉族,教授,博士生导师。先后承担参与国家自然科学基金、173领域基金等项目多项。获聘担任中国空间科学学会空间智能专业委员会委员。是《宇航学报》《空天技术》等学术期刊青年编委。先后发表SCI/EI论文50余篇,授权专利16项。
研究方向
1. 新概念航天器设计
2. 航天器动力学与控制
3. 基于微小卫星平台的航天器在轨操控
教育经历
2009年-2013年, 哈尔滨工业大学, 飞行器设计,本科
2013年-2015年, 哈尔滨工业大学,航空宇航与科学技术,硕士
2015年-2019年,新加坡国立大学,电子与计算机工程,博士
(Selected Journal Publications:)
1. 岳程斐,张枭,王宏旭,李宗凌,曹喜滨.在轨操控机器人拓邻域搜索三维路径规划[J].宇航学报,2022,(02):206-213.
2. 王宏旭,柳子然,岳程斐,曹喜滨.变拓扑多臂航天器高效统一动力学建模[J].宇航学报,2022,(12):1606-1617.
3. 李宁,岳程斐,郭海波,邱实,曹喜滨.大规模卫星星群域管控策略设计[J].中国空间科学技术,2023,(01):18-28.
4. Yan P. T., Hou R.Z., Duan X. G., Yue C.F., Wang X., Cao X. B. STDMANet: Spatio-Temporal Differential Multiscale Attention Network for Small Moving Infrared Target Detection[J]. IEEE Transactions on Geoscience and Remote Sensing, 2023, 99(1):1-10. (JCR Q1)
5. Yu Y. J., Yue C. F., Li N., Wang F., Li H. Y. Onboard Estimation of Mean Orbital Elements Extended to State Jumping Case[J]. Journal of Guidance, Control, and Dynamics, 2022, 45(2):1-17 (JCR Q1)
6. Yue C.F., Lin T., Zhang X., Chen, X.Q. and Cao, X. B.. Hierarchical Path Planning for Multi-arm Spacecraft with General Translational and Rotational Locomotion Mode[J]. Science China Technological Sciences. 2022. (JCR Q1)
7. Yue C. F., Shen Q., Cao X.B., Wang F., Goh C.H., Lee T.H. Fault Modeling of General Momentum Exchange Devices in Spacecraft Attitude Control Systems. Journal of the Franklin Institute. 2020 Apr 10. (JCR Q1)
8. Yue C. F., Wu F., Wang F., Cao X.B., Shen Q., Kumar K.D. Two Parallel Single Gimbal Control Moment Gyros Actuated Spacecraft Attitude Maneuver. IEEE Transactions on Aerospace and Electronic Systems. 2020 Feb 14. (JCR Q1)
9. Yue C. F. Wang F, Cao X, Shen Q, Chen X. Robust fault-tolerant attitude tracking with guaranteed prescribed performance. Journal of the Franklin Institute. 2020 Jan 1;357(1):229-53. (JCR Q1)
10. Yue C. F., Kumar KD, Shen Q, Goh CH, Lee TH. Attitude stabilization using two parallel single-gimbal control moment gyroscopes. Journal of Guidance, Control, and Dynamics. 2019 Jun;42(6):1353-64. (JCR Q1)
11. Cao X. B., Yue C. F., Liu M., Wu B.L. Time efficient spacecraft maneuver using constrained torque distribution. Acta Astronautica,2016, 123:320-329. (JCR Q1)
12. Shen Q, Yue C. F.*, Yu X, Goh CH. Fault Modeling, Estimation, and Fault-Tolerant Steering Logic Design for Single-Gimbal Control Moment Gyro. IEEE Transactions on Control Systems Technology. 2020 Feb 18. (JCR Q1)
13. Shen Q, Yue C. F., Goh C. H., Wang D. W., Active fault-tolerant control system design for spacecraft attitude maneuvers with actuator saturation and faults." IEEE Transactions on Industrial Electronics,2019,66(5): 3763-3772. (JCR Q1)
14. Shen Q., Yue C. F., Goh C. H., Wu B. L., Wang D. W. Rigid-body attitude stabilization with attitude and angular rate constraints. Automatica. 2018, 90: 157-163.(JCR Q1)
15. Cao X. B., Yue C. F., Liu M. Flexible satellite attitude maneuver via constrained torque distribution and active vibration suppression. Aerospace Science and Technology. 2017, 67(August): 387-397.(JCR Q1)