当前位置: X-MOL首页全球导师 国内导师 › 张尧

个人简介

教育经历 2007年9月-2012年6月,在北京航空航天大学获得飞行器设计专业博士学位 2003年9月-2007年7月,在北京理工大学获得飞行器设计与工程专业学士学位 工作经历 2015年7月至今,北京理工大学宇航学院,副教授 2012年7月-2015年6月,北京理工大学宇航学院,讲师 获奖情况 军队科技进步二等奖1项

研究领域

航天器高精度高稳定度姿态控制及应用 失效卫星的接近、消旋和捕获策略研究

近期论文

查看导师新发文章 (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)

Mou Li, Yao Zhang*, Jingrui Zhang, Houyuan Lin and Furen Yang. Detumbling Method for Uncontrolled Satellite Based on Eddy Currents. Journal of Guidance, Control, and Dynamics. 24 April 2020. doi.org/10.2514/1.G004234. Yue Zang, Yao Zhang*, Jingrui Zhang, ZixiGuo, Yujun Chen, Shiming Chen. Multipoint Contact Dynamics and the Detumbling Strategy for a Fast-tumbling Target. IEEE Transaction on Aerospace and Electronic Systems, 2019. doi: 10.1109/TAES.2019.2960681. Chao Sheng, Yao Zhang*, Quan Hu, Jingrui Zhang. Configuration design and collision avoidance control of an electromagnetic vibration isolation system on satellites considering environmental disturbances.ActaAstronautica. Volume 165, December 2019, Pages 229-241. Kunpeng Zhang, Yao Zhang*. Optimal reconfiguration with collision avoidance for a granular spacecraft using laser pressure. ActaAstronautica. 2019. Kai Li, Yao Zhang*, Quan Hu. Dynamic modelling and control of a Tendon-Actuated Lightweight Space Manipulator. Aerospace Science & Technology, 84(2019):1150-1163. MouLi, Yao Zhang*, YouyiWang,Quan Hu, RuiQi. The pointing and vibration isolation integrated control method for optical payload. Journal of Sound and Vibration. 438(2019): 441-456. ZixiGuo,Yao Zhang*, QuanHu. Integrated vibration isolation and attitude control for spacecraft with uncertain or unknown payload inertia parameters. ActaAstronautica. Volume 151, October 2018, Pages 107-119. XiaoyuChu, Jingrui Zhang, Yao Zhang*, Quan Hu, GuangZhai, Yanyan Li. Safety Trajectory Optimization and Tracking Control in Ultra-close Proximity to a Failed Satellite. ActaAstronautica. Volume 144,March 2018,Pages 339-352. Yao Zhang*, Chao Sheng, QuanHu, et al. Dynamic analysis and control application of vibration isolation system with magnetic suspension on satellites. Aerospace Science & Technology. 2018, 75:99–114. Yi Zhao, Jingrui Zhang, Yao Zhang*, Jun Zhang, Quan Hu. Gravitational force and torque on a solar power satellite considering the structural flexibility. ActaAstronautica. 140 (2017) 322–337. Yao Zhang*, Chao Sheng, ZixiGuo, YouyiWang,Wenbo Li. Dynamic characteristics and performance evaluation for the part strut failure of the vibration isolation platform on satellites. ActaAstronautica. 133(2017): 403-415. 2017. Yao Zhang*, Yue Zang, MouLi, YouyiWang, WenboLi. Active-passive integrated vibration control for control moment gyros and its application to satellites. Journal of Sound and Vibration. 394(2017):1-14. 2017. Yao Zhang*,Mou Li, JingruiZhang. Vibration control for rapid attitude stabilization of spacecraft. IEEE Transactions on Aerospace and Electronic Systems. 53(3):1308-1320. 2017. JingruiZhang, ZixiGuo, Yao Zhang*, Tang Liang, Guan Xin. Inner structural vibration isolation method for a single control moment gyroscope. Journal of Sound and Vibration. 361(2016): 78-98. Yao Zhang*, MouLi, ZhuoyueSong, JinjunShan, Xin Guan, Liang Tang. Design and analysis of a moment control unit for agile satellite with high attitude stability requirement. ActaAstronautica. 122, 2016.

学术兼职

国家自然科学基金评审专家 北京力学会青年工作委员会成员 Journal of Guidance Control and Dynamics, Journal of Sound and Vibration, 宇航学报、航空学报等期刊审稿人

推荐链接
down
wechat
bug