
一、 个人基本信息
出生日期:1990年6月
籍贯:黑龙江省哈尔滨市
性 别:男
民 族:汉
职称:讲师
最高学历:博士研究生
工作单位:taptap下载安装安卓电子信息与自动化学院
通信地址:天津市taptap下载安装安卓南院海航科技大厦E106
邮政编码:300300
电 话:022-24092719
电子邮箱:wangyx@cauc.edu.cn
二、 学习和工作经历简介
●2008.09-2012.07:哈尔滨工业大学,自动化,工学学士
●2012.09-2014.07:哈尔滨工业大学,控制科学与工程,工学硕士
●2014.09-2019.07:哈尔滨工业大学,控制科学与工程,工学博士
●2019.07-至今:taptap下载安装安卓,电子信息与自动化学院,教师
三、 主要研究方向和科研业绩
主要研究方向包括:
飞行器导航制导与控制、复杂系统建模仿真与优化评估、人工智能技术
科研项目:
1. 非最小相位高超声速飞行器轨迹跟踪控制方法,国家自然科学基金,主持,在研;
2. 基于微分平坦的飞行器模型线性化方法研究,横向课题,主持,在研;
3. 基于属性层次模型的民用飞机飞行控制系统性能评估方法研究,中央高校,主持,在研;
4. 民用航空飞行器航迹跟踪控制技术研究,科研启动,主持,在研;
5. 基于混杂逻辑的飞行器姿态控制建模方法,横向课题,参与,在研;
6. 基于深度学习的民用舵机故障预测关键技术研究,中央高校,参与,在研;
7. 面向机载惯性元件的随机误差建模及自适应滤波方法研究,科研启动,参与,在研。
四、 论著目录
学术论文:
[1] Wang Y, Chao T, Wang S, et al. Dynamic Sliding-Mode Control for Nonminimum Phase Hypersonic Vehicles Based on Byrnes-Isidori Normalized Form[J]. Aerospace Science and Technology, 2019. (SCI检索)
[2] Wang Y, Yang M, Wang S, et al. Dynamic Sliding-mode Control Scheme for Hypersonic Vehicles Considering Nonminimum Phase Characteristics and Performance Recovery[J]. IEEE Access, 2019. (SCI检索)
[3] Wang Y, Chao T, Wang S, et al. Trajectory tracking control of hypersonic vehicle considering modeling uncertainty[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019. (SCI检索)
[4] Zhao Y, Wang Y. Remaining Useful Life Prediction for Multi-sensor Systems Using a Novel End-to-end Deep-Learning Method. Measurement, 2021. (SCI检索)
[5] Wang Y, Feng H, Zhao Y, et al. Trajectory Tracking Control for Hypersonic Vehicle Based on Differential Flatness and ADRC[C]. 40th Chinese Control Conference, 2022. (EI检索)
[6] Wang Y, Zhao Y. A Data-based Performance Evaluation Method for Aircraft Attitude Control System[C]. 40th Chinese Control Conference, 2021. (EI检索)
[7] Wang Y, Zhao Y, Li X . Finite-time Flight Path Tracking Control Based on Differential Flatness[C]. IEEE 9th Joint International Information Technology and Artificial Intelligence Conference, 2020. (EI检索)
[8] Zhao Y, Wang Y. Remaining Useful Life Prediction via Attention Mechanism-based LSTM Neural Networks. IEEE Joint International Information Technology and Artificial Intelligence Conference, 2020. (EI检索)
[9] Wang Y, Chao T, Wang S, et al. Research on credibility evaluation for radio frequency guided Hardware-In-the-Loop Simulation system[C]. 36th Chinese Control Conference, IEEE, 2017. (EI检索)
[10] Wang Y, Chao T, Wang S, et al. Trajectory tracking control based on differential flatness[C]. 35th Chinese Control Conference, 2016. (EI检索)
[11] Wang Y, Chao T, Wang S, et al. Trajectory tracking control based on improved particle swarm optimization[C]. IEEE Chinese Guidance, Navigation and Control Conference, 2016. (EI检索)
[12] Wang Y, Wang S, Chao T, et al. Performance Evaluation Methods of the Guidance and Control System[C]. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015. (EI检索)
[13] Wang Y, Chao T, Wang S, et al. Reliability evaluation methods for RF guided HILS system with uncertain index values[C]. 34th Chinese Control Conference, IEEE, 2015. (EI检索)
[14] 晁涛, 王雨潇, 王松艳, 等. 考虑非最小相位特性的高超声速飞行器轨迹跟踪控制[J]. 系统工程与电子技术, 2018. (EI检索)
[15] 王雨潇, 王松艳, 晁涛, 等. 制导控制系统的多准则变权综合评估方法[J]. 系统仿真学报, 2018. (重要核心)
专利:
[1] 赵昱宇, 王雨潇, 等. 陀螺飞轮标定基准误差溯源分析方法. 2022.
[2] 王雨潇, 晁涛, 等. 一种基于系统分类的制导控制半实物仿真系统可信度评估方法. 2018.