新莆京游戏app大厅(澳门)股份公司-Maigoo百科

飞行器工程系

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副高级职称（按拼音排序）

张尧

所在学科：航空宇航科学与技术

联系电话：010-68918054

通讯地址：中关村南大街5号

职称：副教授

邮箱：zhangyao@bit.edu.cn

邮编：100081

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，澳门新莆京游戏app大厅，副教授
2012年7月-2015年6月，澳门新莆京游戏app大厅，讲师

主要研究领域

1、航天器高精度高稳定度姿态控制及应用
2、失效卫星的接近、消旋和捕获策略研究

获奖情况

1、军队科技进步二等奖1项

社会兼职

1、国家自然科学基金评审专家
2、北京力学会青年工作委员会成员
3、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

近年来主要发表论文

[1] 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.

[2] 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.

[3] 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.

[4] Kunpeng Zhang, Yao Zhang*. Optimal reconfiguration with collision avoidance for a granular spacecraft using laser pressure. ActaAstronautica. 2019.

[5] Kai Li, Yao Zhang*, Quan Hu. Dynamic modelling and control of a Tendon-Actuated Lightweight Space Manipulator. Aerospace Science & Technology, 84(2019):1150-1163.

[6] 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.

[7] 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.

[8] 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.

[9] 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.

[10] 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.

[11] 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.

[12] 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.

[13] 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.

[14] 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.

[15] 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.