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副教授

教师姓名:张尧
出生日期:1985.1
所在学科:航空宇航科学与技术
职      称:副教授      
联系电话:13811230365
邮      箱:zhangyao@bit.edu.cn
通讯地址:12博BET官方网站宇航楼403
邮      编:100081

教育经历

  2007年9月----2012年6月    北京航空航天大学 飞行器设计专业  博士学历

      2003年9月----2007年7月    12博BET官方网站        飞行器设计专业  学士学历

工作经历

  2012年7月至今    12博BET官方网站。

主要研究领域

  在轨服务航天器动力学及高精度高稳定度控制

获奖情况

社会兼职

  1.   北京力学会青年工作委员会会员;

  2.  宇航学报,航空学报期刊审稿人;

  3.  Acta Astronautica, Journal of Aerospace Engineering期刊审稿人。

教学工作

  1.  本科生《自动控制原理》;

  2.   本科生《Matlab及其在航空航天中的应用》。

近年来主要发表论文

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

  [2] Li Mou, Zhang Yao*, Wang Youyi, Hu Quan, Qi Rui. The pointing and vibration isolation integrated control method for optical payload. Journal of Sound and Vibration. 438(2019): 441-456.

  [3] Guo Zixi, Zhang Yao*, Hu Quan. Integrated vibration isolation and attitude control for spacecraft with uncertain or unknown payload inertia parameters. Acta Astronautica Volume 151, October 2018, Pages 107-119

  [4] Xiaoyu Chu , Jingrui Zhang , Yao Zhang *, Quan Hu , Guang Zhai , Yanyan Li. Safety Trajectory Optimization and Tracking Control in Ultra-close Proximity to a Failed Satellite. Acta Astronautica. Volume 144,March 2018,Pages 339-352

  [5] Zhang Y*, Sheng C, Hu Q, et al. Dynamic analysis and control application of vibration isolation system with magnetic suspension on satellites[J]. Aerospace Science & Technology, 2018, 75:99–114.

  [6] Zhang Yao*, Sheng Chao, Guo Zixi, Wang Youyi, Li Wenbo. Dynamic characteristics and performance evaluation for the part strut failure of the vibration isolation platform on satellites. Acta Astronautica. 133(2017): 403-415. 2017.

  [7] Zhang Yao*, Zang Yue, Li Mou, Wang Youyi, Li Wenbo. Active-passive integrated vibration control for control moment gyros and its application to satellites. Journal of Sound and Vibration. 394(2017):1-14. 2017.

  [8] Zhang Yao*, Li Mou, Zhang Jingrui. Vibration control for rapid attitude stabilization of spacecraft. IEEE Transactions on Aerospace and Electronic Systems. 53(3):1308- 1320. 2017.

  [9] Zhang Jingrui, Guo Zixi, Zhang Yao*, Tang Liang, Guan Xin. Inner structural vibration isolation method for a single control moment gyroscope. Journal of Sound and Vibration. 361, pp 78-98, 2016

  [10] Zhang Yao*, Li Mou, Song Zhuoyue, Shan Jinjun, Guan Xin, Tang Liang. Design and analysis of a moment control unit for agile satellite with high attitude stability requirement. Acta Astronautica. 122, 2016.