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[1]Wenya Zhou, Xiaoming Wang, Wei Qian, Wenhua Wu. Optimization of Locations and Fiber Orientations of Piezocomposite Actuators on Flexible Wings for Aeroelastic Control. Journal of Aerospace Engineering, 2019, 32(5): 04019056-1-12.
[2]Wenya Zhou, Zongyu Zhang, Xiaoming Wang, Weiliang Lv, Xinhan Hu,Structure-Actuator Integrated Design of Piezo-Actuated Composite Plate Wing for Active Shape Control.Journal of Aerospace Engineering, 2021, 34(6): 04021070-1-15.
[3]周文雅, 张宗宇, 王晓明, 吕维梁, 钱卫, 机翼中小尺度主动变形研究进展及关键技术, 机械工程学报, 2021, 57(2): 121-138.
[4]周文雅, 聂振涛, 刘凯, 高度-速度剖面内再入轨迹快速规划, 宇航学报, 2019, 40(11):1341-1347.
[5]周文雅, 李哲, 许勇, 杨峰, 贾涛, 基于双目视觉的无人机编队相对定位算法, 宇航学报, 2022, 43(1): 122-130.
[6]周文雅, 王恩美*, 吴志刚. 高可靠性再入轨迹快速规划方法[J]. 系统工程与电子技术. 2016, 38(8): 1867-1872.
[7]Xiaoming Wang, Wenya Zhou, Zongyu Zhang, Jianping Jiang, Zhigang Wu, Theoretical and experimental investigations on modified LQ terminal control scheme of piezo-actuated compliant structures in finite time. JOURNAL OF SOUND AND VIBRATION, 2021, 491, 115762: 1-17.
[8]Xiaoming Wang, Wenya Zhou, Ruinan Mu, Zhigang Wu, A new deformation control approach for flexible wings using moving masses. AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 106, 106118: 1-12.
[9]Xiaoming Wang, Wenya Zhou, Zhigang Wu, Xiaohu Zhang, Integrated design of laminated composite structures with piezocomposite actuators for active shape control. COMPOSITE STRUCTURES. 2019, 215: 166-177.
[10]Xiaoming Wang, Wenya Zhou, Zhigang Wu, Optimal unimorph and bimorph configurations of piezocomposite actuators for bending and twisting vibration control of plate structures, JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2018, 29(8): 1685-1696.
[11]Xiaoming Wang, Wenya Zhou, Zhigang Wu, Feedback tracking control for dynamic morphing of piezocomposite actuated flexible wings, JOURNAL OF SOUND AND VIBRATION, 2018, 416: 17-28.
[12]Xiaoming Wang, Wenya Zhou, Guangbin Xun, Dynamic shape control of piezocomposite-actuated morphing wings with vibration suppression, JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2018, 29(3): 358-370.
[13]Zehui Mu, Wenya Zhou, Duo Xu, Nan Gao, Control reattachment of backward-facing step flow using a row of mini-jets in recirculation bubble, PHYSICS OF FLUIDS, 2022, 34(8): 081702-1-7.
[14]Jinzhao Yang, Haijun Peng, Wenya Zhou, Zhigang Wu, Integrated Control of Continuum-Manipulator Space Robots with Actuator Saturation and Disturbances, JOURNAL OF GUIDANCE, CONTROL, AND DYNAMICS, 2022,
[15]Jinzhao Yang, Haijun Peng, Wenya Zhou, Jie Zhang, Zhigang Wu, A modular approach for dynamic modeling of multisegment continuum robots, MECHANISM AND MACHINE THEORY, 2021, 165:104429-1-22.
[16]Wenya Zhou*, Kuilong Yin, Rui Wang, Yuee Wang. Design of Attitude Control System for UAV Based on Feedback Linearization and Adaptive Control[J]. Mathematical Problems in Engineering. Volume 2014, Article ID 492680.
[17]Wenya Zhou*, Haixu Wang, Zhengwei Ruan, Zhigang Wu, Enmei Wang. High Accuracy Attitude Control System Design for Satellite with Flexible Appendages[J]. Mathematical Problems in Engineering. Volume 2014, Article ID 695758.
[18]Wenya Zhou*, Haixu Wang, Hongtu Ma, Zhigang Wu. Longitudinal Reentry Guidance Based on Receding Horizon Control[J]. ICIC Express Letters. 2015, 9(2): 461-468.
[19]Wenya Zhou, Enmei Wang, Yutao Wang, Shunan Wu*. Rapid Planning of Reliable Reentry Trajectory[J]. ICIC Express Letters. 2016, 7(4): 881-886.
[20]Wenya Zhou, Hongtu Ma, Shunan Wu*, Nana Meng. INS/GPS Integrated Navigation Technology for Hypersonic UAV[J]. TELKOMNIKA Indonesian Journal of Electrical Engineering. 2014, 12(1): 398-405.
[21]Kai Liu, Jianghai Hu, Wenya Zhou, A Piecewise Envelope Approach to Hinfinity Control of Nonlinear Systems, Asian Journal of Control, 2018, 20(5): 1881-1890 .
[22]Tan Shujun, Peng Haijun, Zhou Wenya*, Wu Zhigang. A novel extended precise integration method based on Fourier series expansion for the H2-norm of linear time-varying periodic systems[J]. International Journal of Control. March 1, 2016: 1-13.
[23]Rui Wang, Xu Li, Wenya Zhou*. Guaranteed cost load frequency control for a class of uncertain power systems with large delay periods[J]. Neurocomputing, 2015, 168: 269-275.
[24]Wu Shunan, Zhou Wenya, Tan Shujun*, Wu Guoqiang. Robust H-infinity Control for Spacecraft Rendezvous with a Noncooperative Target[J]. Scientific World Journal. Article Number: 579703, 2013.
[25]Wang Zhi, Xie Bing, Zhou Wenya*, Shi Guodong, Wu Zhanjun. Thermophysical Properties of TiB2-SiC Ceramics form 300 Degrees C to 1700 Degrees C[J]. International Journal of Refractory Metals &Hard Materials. 2013, 41: 609-613.
[26]王晓明, 周文雅, 吴志刚. 压电纤维复合材料驱动的机翼动态形状控制[J]. 航空学报, 2017, 38(1): 220313.
[27]王晓明, 周文雅, 寻广彬, 吴志刚. 带有振动抑制的压电结构动态形状主动控制[J]. 宇航学报, 2017, 38(2): 185-191.
[28]李昕泽, 周文雅, 刘凯, 王博, 可达区域内最佳着陆场的筛选方法[J], 系统工程与电子技术, 2022.
[29]周文雅, 马瑞鑫, 胡欣涵, 王冠珺, 圆形降落伞下降轨迹控制研究, 兵器装备工程学报, 2021,42(1): 26-30.
[30]柯肇捷, 周文雅, 基于灰自助和未确知有理数的小样本试验数据估计, 兵工学报, 2019, 40(4): 874-879.
[31]刘凯, 郭健, 周文雅, 佘智勇, 吸气式组合动力高超声速飞行器上升段制导方法研究, 宇航学报, 2020, 41(8): 1023-1031.
[32]Xiaoming Wang, Zhigang Wu, Wenya Zhou*. Nonlinear aeroelastic analysis and control of airfoil section with control surface freeplay[J]. ICIC Express Letters. 2016, 10(5): 1151-1156.
[33]张宗宇, 周文雅, 吕维梁, 王晓明, 马瑞鑫, 压电柔性结构形状复合控制方法研究, 压电与声光, 2020, 42(4): 550-556.
[34]张磊, 杨凤田, 周文雅, 黄俊, 基于DATCOM 承载电动无人机纵向稳定性和操纵性, 科学技术与工程, 2020, 20(36): 15127-15131.
[35]李冰玉, 阚子云, 彭海军, 周文雅, 吴志刚, 基于张拉整体结构的连续型弯曲机械臂设计与研究, 机器人, 2020, 42(6): 686-696.
[36]刘宽, 赵梓舒, 武文华, 周文雅, 王晓明, 宏纤维复合材料 MFC 作动器迟滞非线性分析与补偿方法研究, 机械工程学报, 2019, 55(14): 178-185.
[37]刘宽, 武文华, 周文雅, 王晓明, 基于MFC的结构静态形状控制研究, 应用力学学报, 2018, 35(3): 571-576.
[38]庞岩, 周文雅, 彭嗣婷, 基于二级倒立摆的现代控制理论课程设计, 实验室科学, 2017, 20(6): 41-44.
[39]孙振, 汪锐, 周文雅, 倾转旋翼机过渡飞行模式的有限时间切换控制, 控制与决策, 2018, 33(2): 381-384.
[40]阮政委, 杨秦敏, 周文雅, 基于反馈线性化的高速无人机自适应控制系统设计, 宇航总体技术, 2018, 2(3): 25-32.
[41]阮政委, 周文雅*, 张大力, 秦黎博. 基于反馈解耦法的旋转火箭弹自适应控制系统设计[J]. 火力与指挥控制, 2017, 42(3): 161-165.
[42]Zhou Wenya, Yang Di, Chen Hongbo. Maneuver strategy of lifting reentry vehicle[J]. Journal of Harbin Institute of Technology, 2010, 17(3): 333-337.
[43]周文雅*, 杨涤, 李顺利. 利用高斯伪谱法求解具有最大横程的再入轨迹[J]. 系统工程与电子技术, 2010, 32(5): 1038-1042.
[44]谭述君*, 周文雅, 吴志刚. 线性定常系统非齐次两点边值问题的扩展精细积分方法[J]. 应用数学和力学, 2015, 36(11): 1145-1157.
[45]周文雅*, 杨涤, 李顺利. 利用高斯伪谱法求解升力航天器最优再入轨迹[J]. 南京理工大学学报(自然科学版), 2010, 43(1): 85-90.
[46]周文雅*, 杨涤, 梁新刚. 利用高斯伪谱法求解最优气动辅助轨道转移[J]. 吉林大学学报工学版. 2010, 40(5): 1454-1459.
[47]周文雅, 刘恒, 李顺利, 陈洪波. 基于空间交会的天基反卫作战方案[J]. 上海航天, 2009(3): 12-17.
[48]周文雅, 雷涛, 杨涤, 薛东彬. 通用航空飞行器再入大气的热流峰值、最大过载和动压峰值研究[J]. 导弹与航天运载技术, 2009(6): 19-22.
[49]周文雅, 何朕, 王毅. 扰动观测器和等价性[J]. 电机与控制学报, 2006(5): 256-259.
[50]周文雅, 李立涛, 杨涤. 倾转旋翼航空器建模方法研究[J]. 飞行力学, 2008, 26(3): 5-9.
[51]周文雅*, 殷奎龙, 赵东阳. “猎鹰”计划中“2h内全球可达”的可行性分析[J]. 现代防御技术, 2013, 41(2): 35-39.
[52]阮政委, 何志强, 周文雅*, 邢健. 稀薄气体效应对常规布局导弹气动特性的影响[J]. 航空兵器, 2016, (5): 3-7.
[53]何朕, 王毅, 周文雅, 周长浩. 控制系统中随机信号的仿真与分析[J]. 系统仿真学报, 2006, 18(7): 2014-2016.