（1）Yueying Wang(#), Pingfang Zhou(*), Ji-an Chen, Dengping Duan, Finitetime attitude tracking control of an autonomous airship，Transactions of the Institute of Measurement and Control, 2016, 99: 1~8

（2）Yueying Wang(#), Yuanqing Xia, Pingfang Zhou(*), Fuzzy-model-based sampled-data control of chaotic systems: a fuzzy time-dependent Lyapunov- Krasovskii functional approach，IEEE Transactions on Fuzzy Systems，2016, Publication online

（3）Yueying Wang (#),Yuanqing Xia, Pingfang Zhou(*), Dengping Duan, A New Result on Hinfinity State Estimation of Delayed Static Neural Networks, IEEE Trans Neural Netw Learn Syst, 2016, Publication online

（4）Yueying Wang (#)，Pingfang Zhou(*), Quanbao Wang, Dengping Duan, Reliable Robust Sampled-Data H-infinity Output Tracking Control with Application to Flight Control, Information Technology and Control, 2014, 43(2): 175~182

（5）Y. Y. Wang, (#)，P. F. Zhou, (*)，Q. B. Wang, D. P. Duan, State Estimation and Reliable Control of Singular Markovian Systems with Distributed State Delays and Input Delays, Journal of Optimization Theory and Applications, 2014, 162(1): 313~328

（6）Pingfang Zhou#, Yueying Wang, Quanbao Wang, Ji-an Chen, Dengping Duan, Stability and passivity analysis for Lur'e singular systems with Markovian switching, International Journal of Automation and Computing, 2013, 10(1): 79~84

（7）Zhou, Pingfang(#), Wang, Yueying, Duan, Dengping, Adaptive fault-tolerant directional control of an autonomous airship against actuator fault, 35th Chinese Control Conference, CCC 2016，成都，2016.7.27- 2016.7.29

（8）Zhou P.(#)(*), Wang Y., Wang Q., Chen J.-A., Ren J., Duan D., H∞ Non-fragile observer-based sliding mode control of singular Markovian jump systems with state delay, 51st IEEE Conference on Decision and Control, CDC 2012, Maui, HI, 2012.12.10-2012.12.13

专利

（1）周平方, 王曰英, 龚德仁, 周狄, 无人浮空器应急控制系统及其方法, 申请, 2016年3月公开, 中国, CN201510970389.7

（2）周平方, 王曰英, 段登平. 用于无人飞艇系统地面站的遥测数据存取方法, 2012年7月授权, 中国, CN 101826106 B

（3）段登平, 周平方, 王晓亮, 赵海涛, 陈吉安等. 基于欧拉体的浮空器平台及其装配方法, 申请, 2016年8月公开, 中国, CN201610163685.0