个人简历

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》
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 北京理工大学 飞行器设计专业 学士学历
工作经历
　　2012年7月至今 北京理工大学宇航学院

研究领域

在轨服务航天器动力学及高精度高稳定度控制

近期论文

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.
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