孙明玮

2019年06月24日 13:45  点击:[]

基本信息

                   

姓名:孙明玮

性别:

所属部门:自动化与智能科学系

行政职务:                        

职称:教授

学历:博士

所学专业:自动化

办公电话:85358191

电子邮件:smw_sunmingwei@163.com

研究方向:预测控制、自抗扰控制、飞行器制导与控制和非线性优化等

个人简介

1972年生,北京市人。1995年本科毕业于北方交通大学通信与控制工程系交通信号与控制专业,1995--2000年硕博连读于学院控制理论与控制工程专业,获得工学博士学位。2000--2008年从事制导、导航与飞行控制研究与工程实践工作,2002年获得高工职称,同时担任制导、导航与控制专业硕士研究生导师。2009年转入学院从事教学科研工作。主要研究兴趣为预测控制、自抗扰控制、飞行器制导与控制和非线性优化等。

科研项目、成果、获奖、专利

2003年国防科技进步二等奖;                                                                                                                                            
2006年国防科技进步二等奖、三等奖(排名第一);                                                                                                                                            
2006年航天╳╳个人预研二等功                                                                                                                                            
                                                                                                                                         
   

国家发明专利ZL 2015 1 0416028.8 飞行器俯仰姿态的线性自抗扰控制器设计与参数整定方法 孙明玮,王源

国家发明专利ZL 2016 1 0946142.6 攻角的线性自抗扰控制方法 马顺健,孙明玮

国防发明专利ZL 2012╳╳╳╳╳╳╳╳.0,第6发明人。                                                                                                                                            
                                                                                                                                         
   

国家自然科学基金面上项目:高超声速飞行本体约束下典型控制结构的优化与分析,61573197。


   

欢迎具有力学基础的学生攻读研究生,如飞行力学、空气动力学、流体力学、材料力学、动力学建模和飞行器制导与导引等                                                                                                                                            
                                                                                                                                         
除了传统方向,目前正在开拓的新方向为高空翼伞风能发电和智能变形飞行器。

撰写论文、专著、教材等

第一作者或者通信作者作品    

Gao Haitao, Chen Zhigang, Sun Mingwei, Huang Jian, Wang Zenghui, Chen Zengqiang. An Efficient Fast Altitude Control for Hypersonic Vehicle. Control Engineering Practice, https://doi.org/10.1016/j.conengprac.2020.104426.

Gao Haitao, Chen Zhigang, Sun Mingwei, Wang Zenghui, Chen Zengqiang. General Periodic Cruise Guidance Optimization for Hypersonic Vehicles. Applied Sciences, 2020, 10, doi:10.3390/app10082898 .

Piao Minnan, Wang Ying, Sun Mingwei, Chen Zengqiang. Friction Compensation and Limit Cycle Suppression at Low Velocities Based on Extended State Observer. IFAC 2020 World Congress, accepted, Berlin, Germany.

朴敏楠,陈志刚,孙明玮,陈增强。高超声速飞行器气动伺服弹性的自适应抑制。航空学报,https://doi.org/10.7527/S1000-6893.2020.23698。

Tan Panlong, Sun Mingwei, Sun Qinglin, Chen Zengqiang. Dynamic Modeling and Experimental Verification of Powered Parafoil with Two Suspending Points. IEEE Access, 2020, 8(1): 12955-12966.

Gao Haitao, Sun Mingwei, Chen Zengqiang. Hypersonic Periodic Cruise Trajectory Optimization Based on Flexible Use of Pseudo-Spectral Method. Proceedings of 2019 Chinese Intelligent Systems Conference, Lecture Notes in Electrical Engineering 593, 2019, Haikou, China: 107-116, 2020.

朴敏楠,王科磊,孙明玮,黄建,陈增强。基于积分泄露的机电伺服系统摩擦力补偿。中南大学学报(自然科学版),2020, 51(3):668-677。

Piao Minnan, Sun Mingwei, Huang Jian, Wang Zenghui, Chen Zengqiang. Partial Integrated Guidance and Control Design for Supersonic Missile Based on Disturbance Rejection. Measurement and Control, 2019, 52(9-10): 1445-1460.

Piao Minnan, Zhang Youan, Sun Mingwei, Yang Zhihong, Wang Zenghui, Chen Zengqiang. Adaptive Aeroservoelastic Mode Stabilization of Flexible Airbreathing Hypersonic Vehicle. Journal of Vibration and Control, 2019, 25(15): 2124-2142.

Liu Junjie, Chen Zengqiang, Sun Mingwei, Sun Qinglin. Practical Coupling Rejection Control for Herbst Maneuver with Thrust Vector. AIAA Journal of Aircraft, 2019, 56(4): 1726-1734.

Piao Minnan, Yang Zhihong, Sun Mingwei, Huang Jian, Chen Zengqiang. A Practical Attitude Control Scheme for Hypersonic Vehicle Based on Disturbance Observer. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, 233(12): 4523-4540.

Sun Mingwei, Zhang Youan, Liu Jingmao, Huang Jian, Wang Zenghui, Chen Zengqiang. Explicit Parameterized Energy Management for Scramjet Transition. IEEE Transactions on Aerospace and Electronic Systems, 2019, 55(2): 798-809.

Piao Minnan, Yang Zhihong, Sun Mingwei, Huang Jian, Wang Zenghui, Chen Zengqiang. Synthesis of Attitude Control for Statically Unstable Hypersonic Vehicle with Low-Frequency Aero-Servo-Elastic Effect. Aerospace Science and Technology, 2018, 60, 67-77.

Sun Mingwei, Wang Zenghui, Chen Zengqiang. Parametric Trajectory Optimization of Boost-Glider. Proceedings of the 15th International Conference on Space Operations, May 28- June 1, 2018, Marseille, France: Paper AIAA-2018-2593.

朴敏楠,杨志红,孙明玮,黄建,陈增强。弹性静不稳定高超声速飞行器姿态综合控制。中国科学:技术科学,2019, 49(7): 825-839。

孙明玮,马顺健,陈增强,胡超芳。飞行器定时航迹规划及其交互仿真平台设计。系统仿真学报,2018,30(8):2966-2972。

孙明玮,马顺健,朴敏楠,王永坤,李毅。高超声速飞行器自抗扰控制方法。北京:科学出版社,2018。

Li Junfang, Sun Mingwei, Wang Zenghui, Chen Zengqiang. Chaotic Optimization of Tethered Kites for Wind Energy Generator. Proceedings of the 13th International Conference on Intelligent Computing, August 7-10, 2017, Liverpool, UK: 587-599.

Liu Yajie, Yang Zhihong, Sun Mingwei, Chen Zengqiang. Penetration Design for the Boost Phase of Near Space Aircraft. Proceedings of the 36th Chinese Control Conference, July 26-28, 2017, Dalian, China: 5975-5979.

Wang Yongkun, Liu Zhongxin, Sun Mingwei, Wang Zenghui, Chen Zengqiang. Practical MPC Solution to Attitude Control Independent of Angular Velocity Measurements. Proceedings of the 13th IEEE International Conference on Control and Automation, July 3-5, 2017, Ohrid, Macedonia: 630-635.

Wu Qixia, Sun Mingwei, Yang Zhihong, Wang Zenghui, Chen Zengqiang. Tuning of Active Disturbance Rejection Attitude Controller for Statically Unstable Launch Vehicle. AIAA Journal of Spacecraft and Rockets, 2017, 54(6): 1383-1389.

Ma Shunjian, Sun Mingwei, Chen Zengqiang. Interactive ADRC Design for Flight Attitude Control. Proceedings of 2017 IEEE 6th Data Driven Control and Learning Systems Conference, May 26-27, 2017, Chongqing, China: 611-616.

Piao Minnan, Zhu Kai, Sun Mingwei, Wang Zenghui, Chen Zengqiang. Quantitative Relationship in Terms of Time-Delay Tolerance of Two Kinds of Extended State Observers. Proceedings of 2017 IEEE 6th Data Driven Control and Learning Systems Conference, May 26-27, 2017, Chongqing, China: 9-15.

Ma Shunjian, Zhu Kai, Sun Mingwei, Wang Zenghui, Chen Zengqiang. On Active Decoupling Control for Horizontal-Lateral Direction of Hypersonic Flight Based on HIFOO. Proceedings of the 21st AIAA International Space Plane and Hypersonic Systems and Technology Conference, March 6-9, 2017, Xiamen, China: Paper AIAA-2017-2255.

Piao Minnan, Zhu Kai, Sun Mingwei, Chen Zengqiang. A Unified Angle Control Scheme for Hypersonic Vehicle Based on Disturbance Rejection. Proceedings of the 21st AIAA International Space Plane and Hypersonic Systems and Technology Conference, March 6-9, 2017, Xiamen, China: Paper AIAA-2017-2175.

Yang Zhihong, Zhu Kai, Sun Mingwei, Wang Zenghui. Practical Guidance Design for the Boost Phase of Hypersonic Vehicle Subject to Terminal Scramjet Transition Constraints. Proceedings of the 21st AIAA International Space Plane and Hypersonic Systems and Technology Conference, March 6-9, 2017, Xiamen, China: Paper AIAA-2017-2139.

Sun Mingwei, Gao Zhiqiang, Wang Zenghui, Zhang Yuan, Chen Zengqiang. On the Model-Free Compensation of Coulomb Friction in the Absence of the Velocity Measurement. ASME Journal of Dynamic Systems, Measurement and Control, 2017, 139(12): 125001(1-6).

Wang Yongkun, Liu Zhongxin, Sun Mingwei, Wang Zenghui, Chen Zengqiang. Adaptive Backstepping Attitude Control with Disturbance Rejection Subject to Amplitude and Rate Saturations of the Elevator. ASCE's Journal of Aerospace Engineering, 2017, 30(3): 04016095.

Wang Yongkun, Sun Mingwei, Du Shengzhi, Chen Zengqiang. Comparative Investigations of Nonlinear and Linear Observers for A Highly Manoeuvrable Target in Sliding Mode Guidance. Bulletin of the Polish Academy of Sciences: Technical Sciences, 2017, 65(2): 233-245.

吴其霞,马顺健,孙明玮,陈增强。静不稳定运载飞行器自抗扰姿态控制的参数整定研究。战术导弹技术,2016,(2):63-69。

Wu Qixia, Sun Mingwei, Wang Zenghui, Chen Zengqiang. Practical Solution to Efficient Flight Path Control for Hypersonic Vehicle. Transactions of the Japan Society for Aeronautical and Space Sciences, 2016, 59(4): 195-204.

Li Yi, Sun Mingwei, Wang Zenghui, Chen Zengqiang. PID Attitude Control Subject to Dynamic Rate Saturation of Elevator through Explicit Command Reshaping: An Engineering Approach. Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering, 2016, 230(6): 562-577.

Zhang Yuan, Sun Mingwei, Chen Zengqiang. Unified Linear Time-Invariant Model Predictive Control for Strong Nonlinear Chaotic Systems. Nonlinear Analysis: Modelling and Control, 2016, 21(5): 587-599.

Wang Yuan, Wang Yongkun, Sun Mingwei, Du Shengzhi, Chen Zengqiang. Neural Networks Based Formation Control of Anti-Ship Missiles with Constant Velocity. Proceedings of the 13th IEEE International Conference on Pervasive Intelligence and Computing (PICom-2015), October 26-28, 2015, Liverpool, England, UK.

Liu Wei, Ma Shunjian, Sun Mingwei, Yi Haidong, Wang Zenghui, Chen Zengqiang. Sequential Quadratic Programming-Based Fast Path Planning Algorithm Subject to No-Fly Zone Constraints. Engineering Optimization, 2016, 48(8): 1401-1418.

张园,孙明玮,陈增强。强制循环蒸发系统线性自抗扰解耦控制的鲁棒设计。化工学报,2015,66(S2):263-270。

Wang Yongkun, Liu Zhongxin, Sun Mingwei, Chen Zengqiang. A Continuous Second-Order Sliding Mode Guidance againnst Highly Maneuverable Targets. Proceedings of SICE Annual Conference 2015, July 28-30, 2015, Hangzhou, China: 991-996.

Sun Mingwei, Gao Zhiqiang, Du Shengzhi, Chen Zengqiang. On Active Disturbance Rejection Based Framework for Flight Control: Principle And Applications. Proceedings of the 6th European Conference for Aeronautics and Space Sciences (EUCASS), June 29-July 3, 2015, Krakow, Poland.

Li Yi, Sun Mingwei, Wang Zenghui, Chen Zengqiang. Quantitative Analysis of Critical Limitation in Using Extended State Observer. International Journal of Control, Automation and Systems, 2016, 14(3): 876-882.

张利民,孙明玮,刘东辉,全胜,陈增强。翼伞发电系统的GPU并行轨迹优化。电机与控制学报,2015,19(8):88-94。

Sun Mingwei, Zhang Yuan, Zhang Limin, Wang Zenghui, Chen Zengqiang. Numerical Solving Method for Specific Dynamic Performance of Unstable Flight Dynamics with PD Attitude Control. Proceedings of the ICCSAM 2015: 17th International Conference on Computer Science and Applied Mathematics, April 13-14, 2015, Venice, Italy: 313-319.

孙明玮,张利民,陈增强。导弹三回路过载驾驶仪设计频带的灵敏度分析方法。兵工学报,2014,35(12):2023-2029。

Sun Mingwei, Zhang Limin, Wang Zenghui, Chen Zengqiang. PID Pitch Attitude Control for Unstable Flight Vehicle in the Presence of Actuator Delay: Tuning and Analysis. Journal of the Franklin Institute, 2014, 351(12): 5523-5547.

张园,孙明玮,陈增强,袁著祉。基于扩张状态观测器的广义预测控制。系统科学与数学,2014,34(11):1366-1378。

王永坤,孙明玮,刘忠信,陈增强。调节速度方向实现导弹编队的预测控制设计。Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference, August 8-10, 2014, Yantai, China: 652-657.

张园,徐琦,孙明玮,陈增强。基于快速全线性预测控制的混沌系统控制与同步。物理学报,2015,64(1):010512(1-7)。

周昆,孙明玮,陈增强。快速显式预测控制在倒立摆系统中的应用。仪器仪表学报,2014,35(9):2037-2044。

张利民,孙明玮,陈增强。基于伪谱法优化预测的导弹攻击时间匹配策略。Proceedings of the 11th World Congress on Intelligent Control and Automation, June 29-July 4, 2014, Shenyang, China: 1670-1675.

王永坤,孙明玮,刘忠信,陈增强。挠性系统谐振频率摄动范围的几何解法。哈尔滨工业大学学报,2015,47(1):86-91。

Zhang Limin, Sun Mingwei, Chen Zengqiang, Wang Zenghui, Wang Yongkun. Receding Horizon Trajectory Optimization with Terminal Impact Specifications. Mathematical Problems in Engineering, vol. 2014, Article ID 604705, 2014. doi:10.1155/2014/604705.

孙明玮,徐琦,陈增强,张德贤。自抗扰三回路过载驾驶仪的设计。北京理工大学学报,2015,35(6):592-596。

Qiu Demin, Sun Mingwei, Wang Zenghui, Wang Yongkun, Chen Zengqiang. Practical Wind Disturbance Rejection for Large Deep Space Observatory Antenna. IEEE Transactions on Control System Technology, 2014, 22(5): 1983-1990.

Wang Yongkun, Sun Mingwei, Wang Zenghui, Liu Zhongxin, Chen Zengqiang. A Novel Disturbance-Observer Based Friction Compensation Scheme for Ball and Plate System. ISA Transactions, 2014, 53(2): 671-678.

Sun Mingwei, Xu Qi, Du Shengzhi, Chen Zengqiang, Zhang Dexian. Practical Solution to Impact Angle Control in Vertical Plane. AIAA Journal of Guidance, Control, and Dynamics, 2014, 37(3): 1022-1027.

徐琦,孙明玮,陈增强,张德贤。扩张状态观测器的内模控制分析与设计。Proceedings of the 32nd Chinese Control Conference, July 26-28, 2013, Xi’an, China: 5408-5413.

Sun Mingwei, Chen Zengqiang, Du Shengzhi. Graphical Description of Autopilot Robustness to Aerodynamic Uncertainties. The 2013 Asian Control Conference, Istanbul, Turkey, June 23-26, 2013.

孙明玮,邱德敏,王永坤,陈增强。大口径深空探测天线抗风干扰伺服系统设计。光学 精密工程,2013,21(6):1568-1575。

Sun Mingwei, Wang Zenghui, Chen Zengqiang. Practical Solution to Attitude Control within Wide Envelope. Aircraft Engineering and Aerospace Technology, 2014, 86(2), 117-128.

孙明玮,刘东辉,全胜,陈增强。翼伞发电系统的GPU并行轨迹优化设计。2012年中国飞行力学学术年会,云南腾冲,2012年10月。

Sun Mingwei, Wang Zenghui, Wang Yongkun, Chen Zengqiang. On Low-Velocity Compensation of Brushless DC Servo in the Absence of Friction Model. IEEE Transactions on Industrial Electronics, 2013, 60(9): 3897 - 3905.

孙明玮,焦纲领,陈增强。基于混沌优化的再入飞行器滚动时域轨迹设计。宇航学报,2012,33(12):1711-1718。

Sun Mingwei, Jiao Gangling, Yang Ruiguang, Chen Zengqiang. ADRC for Statically Unstable Longitudinal Flight Dynamics. Proceedings of the 30th Chinese Control Conference, July 22-24, 2011, Yantai, China: 6274-6280.

Sun Mingwei, Yang Ruiguang, Wang Zenghui, Chen Zengqiang. Stability Margin Based PD Attitude Control Tuning for Unstable Flight Vehicle. International Journal of Systems Science, 2013, 44(2): 240-251.

Sun Mingwei, Yang Ruiguang, Chen Zengqiang. Genuine Feasible Stability Margin Region for Integrating Unstable Processes with PD Control. IET Control Theory Appl., 2011, 5(10): 1228–1234.

孙明玮,焦纲领,杨瑞光,陈增强。PI控制下开环不稳定对象可行稳定裕度范围的研究。自动化学报, 2011, 37(3): 385-388.

孙明玮。我的祖国。

Yang Ruiguang, Sun Mingwei, Chen Zengqiang. Performance Analysis of Active Disturbance Rejection Control on the First-Order-Plus-Dead-Time Plant. ICIC Express Letters, 2010, 5(4B): 1249-1254.

孙明玮,焦纲领,杨瑞光,陈增强。滑翔飞行器阻力-能量剖面制导的自抗扰跟踪。Proceedings of the 29th Chinese Control Conference, July 29-31, 2010, Beijing China: 3260-3264.

孙明玮,焦纲领,杨瑞光,陈增强。自抗扰控制在飞行器控制与制导上的应用与分析—不同时间尺度问题的摸索。Proceedings of the 29th Chinese Control Conference, July 29-31, 2010, Beijing China: 6167-6172.

孙明玮,杨瑞光,陈增强。飞行自抗扰姿态控制设计与性能分析。2010年WCICA,济南, July, 2010.

Sun Mingwei,Chen Zengqiang and Z. Z. Yuan. A Practical Solution to Some Problems in Flight Control. Proceedings of IEEE Control & Decision Conference, Shanghai, P. R. China, Dec. 16-18, 2009, 1482-1487.

孙明玮。为了我们的青年----写在“五四”运动九十周年之际。

孙明玮,史莹晶,马广富。基于指令分解的导弹复合控制方法研究。弹道与制导学报,2008,28(1):1-3。

陈志刚,孙明玮,马洪忠。基于误差反馈补偿的攻击无人机角度和时间控制。航空学报,2008,29(增刊),S33-S38。

孙明玮。论国防科技部门科研氛围与科技创新的关系。航天工业管理,2007(3):5-6。

孙明玮,刘丽,杨明。飞航导弹双平面纵向综合制导技术。中国工程科学,2007,9(9):52-57。

孙明玮。反舰导弹机动与导引配合的弹道设计研究。现代防御技术,2007,35(1):23-26。

孙明玮,刘丽,薛丽华。一种简化的综合制导设计技术。战术导弹技术,2007(1):62-66。

孙明玮。21世纪对精确打击弹药制导技术的需求。飞航导弹,2006(2):49-59。

孙明玮,彭楠南,杨明。导弹最优滑翔弹道的设计及存在的问题。飞行力学,2006,24(1):26-29。

孙明玮,刘丽。导弹侧向机动控制的优化设计。战术导弹控制技术,2006(4):3-6。

孙明玮。利用惯性垂速进行飞航导弹纵向导引设计。战术导弹控制技术,2006(4):25-27。

孙明玮,陈志刚。基于虚拟导引的程序弹道快速生成技术。战术导弹控制技术,2006(4):28-29。

孙明玮,陈志刚。指定倾角的小视场角攻击导引技术。战术导弹控制技术,2006(4):30-33。

彭楠南,孙明玮,魏毅寅,马洪忠,杨明。导弹姿态的反演控制器设计。兵工自动化,2006,25(3):6-8。

孙明玮,杨明。飞航导弹新型工程化控制方法研究的一些思考。战术导弹技术,2005(5):38-43。

孙明玮,杨勇,陈增强,袁著祉,刘丽。导弹机动的混沌特性与控制能力分析。战术导弹控制技术,2005(3):9-16。

孙明玮,陈增强,袁著祉,任强,杨明。飞航导弹高精度自适应预测控制设计。中国工程科学,2005,7(10):23-27。

孙明玮,陈增强,袁著祉,杨明。不引起非最小相位现象的极点配置方法。第24届中国控制会议论文集,2005年7月,广州:44-46。

孙明玮,彭楠南,魏毅寅,杨明。指定入射角的飞航导弹末段俯冲弹道设计。航天控制,2005,23(1):62-64。

孙明玮,程凤舟,杨明。双星导航与捷联惯导系统在快速载体组合制导中的应用研究。战术导弹控制技术,2004(3):40-45。

孙明玮,韩京梅,王新华,陈增强,袁著祉。混合控制系统的稳定裕度分析与计算。计算机测量与控制,2004,12(6):527-528。

彭楠南,孙明玮,魏毅寅,马洪忠。导弹大空域俯冲中的机动与马赫数调节。中国航空学会控制与应用第11届学术年会论文集,2004年8月,山东烟台:241-247。

孙明玮,王健,薛丽华。飞航导弹动力装置的预测控制设计。推进技术,2004,25(3):230-232。

薛丽华,孙明玮。反舰导弹串级离散变结构姿态控制。海军航空工程学院学报,2003,18(6):617-620。

张奇,孙明玮,邵继法。基于最小二乘法的飞航导弹速度信息融合研究。海军航空工程学院学报,2003,18(6):621-625。

孙明玮,张奇,邵继法,陈增强,袁著祉。鲁棒递推阻尼最小二乘算法。航空计算技术,2003,33(1):22-25。

孙明玮,韩京梅,陈增强,袁著祉。利用Matlab优选PID参数及其在飞控系统设计中的应用。计算机仿真,2003,20(1):47-49。

孙明玮,陈增强,袁著祉。变结构控制中滑模与模型选取的若干原则。控制工程,2003,10(6):481-483。

孙明玮,张奇,邵继法。双星定位与惯导系统的高效实用融合方法。导航,2003,39(2):22-29。

孙明玮。建立新型弹性用人机制。航天工业管理,2002(11):30-31。

孙明玮,陈增强,袁著祉。输出增量反馈思想。信息与控制,2002,31(1):5-8。

孙明玮。发展跨海登陆作战武器的新思路。舰船论证参考,2001(2):16-18。

孙明玮。关于选取飞航导弹控制方法的思考—兼论继承与创新的关系。飞航导弹,2001(9):52-53。

孙明玮,陈增强,袁著祉。具有稳定性的约束预测控制。系统工程学报,2000,15(3):262-266。

孙明玮,陈增强,袁著祉。无限时域预测控制的直接求解方法。应用数学,2000,13(3):5-9。

孙明玮,陈增强,袁著祉。β增量型广义预测控制。控制理论与应用,2000,17(2):165-168。

孙明玮,陈增强,袁著祉。典型工业过程的无超调预测控制设计。控制与决策,2000,15(2):213-216。

Sun Mingwei, Chen Zengqiang, Yuan Zhuzhi. Recursive Algorithm for Constrained Receding Horizon Predictive Control. Proceedings of the 3rd World Congress on Intelligent Control and Automation, 2000, June, Hefei, P. R. China: 3461-3464.

孙明玮,陈增强,袁著祉。基于小波分频设计的自适应PID控制器。学院学报(自然科学版),2000,33(2):48-52。

Sun Mingwei, Chen Zengqiang, Yuan Zhuzhi. The Principle of Robustness in Generalized Predictive Control. Applied Mathematics-A Journal of Chinese Universities. 1999, Ser. B, 14(2): 293-300.

孙明玮,陈增强,袁著祉。广义预测控制的鲁棒性机理分析。中国控制会议论文集,1998年9月,浙江宁波:361-364。

孙明玮,陈增强,袁著祉。基于频域辨识的广义预测控制。中国控制会议论文集,1997年8月,江西庐山:467-470。



其他作品

Luo Shuzhen, Sun Qinglin, Tan Panlong, Sun Mingwei, Chen Zengqiang, He Yingping. Soft Landing Control of Unmanned Powered Parafoils in Unknown Wind Environments. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, 233(3): 949-968.

陈增强, 吴瑕, 孙明玮, 孙青林。基于频域的自抗扰广义预测控制的稳定性分析。哈尔滨工程大学学报,2018,39(6):1046-1051。

陈增强, 吴瑕, 孙明玮, 孙青林。时滞系统的自抗扰广义预测控制的性能分析。中南大学学报(自然科学版),2018,49(8):1960-1970。

董方酉,孙青林,张晓雷,蒋玉新,孙明玮,陈增强。基于死区补偿的氧调器平稳切换自抗扰控制。航空学报,2018,39(5):321875(1-12)。

张勇,陈增强,张兴会,孙明玮,孙青林。四旋翼无人机系统PD-ADRC串级控制。系统工程与电子技术,2018,40(9):2055-2061。

张勇,陈增强,张兴会,孙青林,孙明玮。基于自抗扰的四旋翼无人机动态面姿态控制。吉林大学学报(工学版),2018,42(1)。

Luo Shuzhen, Sun Qinglin, Sun Mingwei, Tan Panlong, Wu Wannan, Sun Hao, Chen Zengqiang. On Decoupling Trajectory Tracking Control of Unmanned Powered Parafoil Using ADRC-Based Coupling Analysis and Dynamic Feedforward Compensation. Nonlinear Dynamics, 2018, 92(4): 1619-1635.

Cheng Yun, Chen Zengqiang, Sun Mingwei, Sun Qinglin. Cascade Active Disturbance Rejection Control of a High-Purity Distillation Column with Measurement Noise. Industrial & Engineering Chemistry Research, 2018, 57(13): 4623-4631.

Wu Wannan, Sun Qinglin, Luo Shuzhen, Sun Mingwei, Chen Zengqiang, Sun Hao. Accurate Calculation of Aerodynamic Coefficients of Parafoil Airdrop System Based on Computational Fluid Dynamic. International Journal of Advanced Robotic Systems, 2018, 15(2): 1729881418766190.

Chen Zengqiang, Wang Yongshuai, Sun Mingwei, Sun Qinglin. Convergence and Stability Analysis of Active Disturbance Rejection Control for First-Order Nonlinear Dynamic Systems. Transactions of the Institute of Measurement and Control, 2019, 41(7): 2064-2076.

Zhang Yong, Chen Zengqiang, Zhang Xinghui, Sun Qinglin, Sun Mingwei. A Novel Control Scheme for Quadrotor UAV Based upon Active Disturbance Rejection Control. Aerospace Science and Technology, 2018, 79: 601-609.

Wu Xia, Li Yi, Chen Zengqiang, Sun Mingwei. On The Design and Realization of Active Disturbance Rejection Generalized Predictive Control. IMA Journal of Mathematical Control and Information, DOI: 10.1093/imamci/dny027.

Wu Xia, Chen Zengqiang, Zhao Yue, Sun Lijun, Sun Mingwei. A Comprehensive Decoupling Control Strategy for A Gas Flow Facility Based on Active Disturbance Rejection Generalized Predictive Control. The Canadian Journal of Chemical Engineering, 2019, 97(3): 762-776.

Tao Jin, Sun Qinglin, Sun Hao, Chen Zengqiang, Dehmer Matthias, Sun Mingwei. Dynamic Modelling and Trajectory Tracking Control of Parafoil System in Wind Enviroment. IEEE/ASME Transactions on Mechatronics, 2017, 22(6): 2736-2745.

陈增强,程赟,孙明玮,孙青林。线性自抗扰控制理论及工程应用的若干进展。信息与控制,2017,46(3):257-266。

程赟,陈增强,孙明玮,孙青林。多变量逆解耦自抗扰控制及其在精馏塔过程中的应用。自动化学报,2017,43(6):1080-1088。

Wu Xia, Chen Zengqiang, Sun Mingwei, Sun Qinglin. Active Disturbance Rejection Generalized Predictive Control and Application on Large Time-delay System. Proceedings of 2017 IEEE 6th Data Driven Control and Learning Systems Conference, May 26-27, 2017, Chongqing, China: 1-8.

Li Junfang, Li Yi, Gao Qiang, Sun Mingwei, Chen Zengqiang. On Trajectory Tracking for an Under-Actuated Helicopter. Proceedings of the 35th Chinese Control Conference, July 27-29, 2016, Chengdu, China: 10944-10949.

陈上上,何英姿,张钊,孙明玮。再入飞行器鲁棒自抗扰跟踪律设计。航天控制,2016,34(2):49-53。

Wang Yuanguang, Wang Changhui, Xiao Yingchao, Chen Bing, Zhou Shuo, Guo Jingtao, Sun Mingwei. Construction Methodology for Lip Surface of A Submerged Inlet. Aerospace Science and Technology, 2016, 54(July): 340-352.

李毅,陈增强,孙明玮,刘忠信,张青。离散型自抗扰控制器在四旋翼飞行姿态控制中的应用。控制理论与应用,2015,32(11):1470-1477。

陈增强,李毅,袁著祉,孙明玮,刘忠信,孙青林。串级自抗扰控制器在纵列式双旋翼直升机飞行姿态控制中的应用。控制理论与应用,2015,32(9):1219-1225。

陈增强,王辰璐,李毅,张青,孙明玮。基于积分滑模的四旋翼飞行器控制系统设计。系统仿真学报,2015,27(9):2181-2186。

Li Yi, Chen Zengqiang, Sun Mingwei, Liu Zhongxin, Zhang Qing. ADRC Based Attitude Control of A Quad-Rotor Robot. Lecture Notes in Electrical Engineering, 2015, 337: 503-512.

Huang Yi, Xue Wenchao, Zhiqiang Gao, Hebert Sira-Ramirez, Wu Dan, Sun Mingwei. Active Disturbance Rejection Control: Methodology, Practice and Analysis. Proceedings of the 33rd Chinese Control Conference, July 28-30, 2014, Nanjing, China: 1-5 (Plenary Talk).

胡彬,应小昆,孙青林,孙明玮,陈增强。线性自抗扰技术在热处理电阻炉中的应用。Proceedings of the 33rd Chinese Control Conference, July 28-30, 2014, Nanjing, China: 3585-3590.

徐琦,孙明玮,陈增强,张德贤。内模控制框架下时延系统扩张状态观测器参数整定。控制理论与应用,2013,30(12):1641-1645。

Wang Haitao, Zhao Dongbin, Sun Mingwei. Optimization of Periodic Optimal Cruise for a Hypersionic Vehicle. 2013 Chinese Automation Congress, November, 2013, Changsha, China.

Zhang Xuebo, Fang Yongchun, Sun Ning, Sun Mingwei. A Pseudospectral Time-Optimal Motion Planner for Underactuated Overhead Crane Systems. Proceedings of the 32nd Chinese Control Conference, July 26-28, 2013, Xi’an, China: 4397-4402.

高海涛,张利民,孙青林,孙明玮,陈增强,亢晓峰。基于伪谱法的翼伞系统归航轨迹容错设计。控制理论与应用,2013,30(6):702-708。

陈增强,孙明玮,杨瑞光。线性自抗扰控制器的稳定性研究。自动化学报,2013,39(5): 574-580。

张利民,孙明玮,陈增强,张兴会。基于伪谱法的定时定向航路规划方法研究。弹道学报,2013,25(3): 1-5。

张运喜,孙明玮,陈增强。滑模变结构有限时间收敛制导律。控制理论与应用,2012,29(11): 1413-1418。

Zhang Yunxi, Sun Mingwei, Chen Zengqiang. Finite-Time Convergent Guidance Law with Impact Angle Constraint Based on Sliding-Mode Control. Nonlinear Dynamic, 2012, 70(1): 619-625.

Du Shengzhi, Tu Chunling, Sun Mingwei. High Accuracy Hough Transform Based on Butterfly Symmetry. Electronic Letters, 2012, 48(4): 199-201.

高海涛,孙青林,亢晓峰,孙明玮,陈增强。基于数据扩充的ADRC翼伞航迹跟踪控制。Proceedings of the 31st Chinese Control Conference, July 25-27, 2012, Heifei, China: 2975-2980.

Sun Mingwei, Jiao Gangling, Yang Ruiguang, Chen Zengqiang. ADRC for Statically Unstable Longitudinal Flight Dynamics. Proceedings of the 30th Chinese Control Conference, July 22-24, 2011, Yantai, China: 6274-6280.

张运喜,孙明玮,陈增强。基于变结构控制的导弹制导律研究进展。第七届全国多智能体系统与控制会议,山东烟台,2011年10月。

Yang Ruiguang, Sun Mingwei, Chen Zengqiang. Graphical Design of Linear Active Disturbance Rejection Controller for Uncertain First-order-Plus-Dead-Time Plant. Proceedings of 2011 International Conference on Modeling, Identification and Control, Shanghai, China, June 26-29, 2011.

Yang Ruiguang, Sun Mingwei, Chen Zengqiang. Active Disturbance Rejection Control on First-Order Plant. Journal of Systems Engineering and Electronics, 2011, 22(1): 95-102.

Yang Ruiguang, Sun Mingwei, Chen Zengqiang. Performance Analysis of Active Disturbance Rejection Control on the First-Order-Plus-Dead-Time Plant. ICIC Express Letters, 2010, 5(4B): 1249-1254.

杨瑞光,孙明玮,陈增强。飞行器自抗扰姿态控制优化与仿真研究。系统仿真学报,2010,22(11): 2689-2693。

杨瑞光,孙明玮,陈增强。典型惯性环节的自抗扰控制性能分析。Proceedings of the 29th Chinese Control Conference, July 29-31, 2010, Beijing China: 3576-3580.

Wang Jian, He Linshu, Sun Mingwei. Application of Active Disturbance Rejection Control to Integrated Flight-Propulsion Control. Proceedings of the Chinese Control and Decision Conference, Xuzhou, China, 2010: 4397-4402.

徐颖珊,孙明玮。自抗扰控制在飞航导弹上的应用背景研究。战术导弹控制技术,2008,30(2):8-11。

李红春,蔡洪,孙明玮。基于制导一体化设计实现大入射角攻击目标的技术研究。战术导弹技术,2008,(5):54-58。

许阳,李常平,孙明玮。自抗扰控制在无人机过载控制中的应用研究。第一届中国导航、制导与控制学术会议,2007年11月,北京:53-57。

任强,孙明玮,陈增强,袁著祉。非线性PID控制在导弹纵向飞行控制中的应用。江南大学学报(自然科学版),2006,5(4):411-414。

任强,陈增强,孙明玮,袁著祉。连续时间广义预测控制在纵向飞行控制中仿真。系统仿真学报,2006,18(2):814-816。

Lu Zhao, Sun Mingwei. Neuromorphic Continuous-time State Space Pole Placement Adaptive Control. Journal of Systems Engineering and Electronics. 2003,14(1): 58-62.

陈增强,孙明玮,袁著祉,陈春艳。基于模糊神经网络的PI自适应控制器。华东理工大学学报,2002,28(增刊),45-48。

陈增强,孙明玮,袁著祉。采样系统预测控制的设计与分析。控制理论与应用,2002,19(2):268-270。

贺江峰,王群仙,刘浩,章春利,孙明玮,李少远,陈增强,袁著祉。涤纶片基拉膜生产线控制系统设计与实现。中国控制会议论文集,1997年8月,江西庐山:1095-1098。

讲授课程

大一《自动化概论》,大三《动力学、制导与控制》;科学硕士研究生《飞行器制导、导航与控制》,专业硕士《控制工程》和《控制科学前沿》

社会兼职

中国自动化学会数据驱动控制、学习与优化专业委员会委员                                                                                                                                                                                                        
中国自动化学会控制理论专业委员会模型预测控制学组委员                                                                                                                                                                                                        
中国系统仿真学会智能物联系统建模与仿真专业委员会委员                                                                                                                                                                                                        
中国自动化学会控制理论专业委员会抗干扰控制及应用学组委员



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