1.个人简介
阎坤,男,博士,教授,硕士生导师,目前是中国自动化学会会员和中国航空学会会员,并担任IEEE Transactions on SMC: Systems、IEEE Transactions on Cybernetics、ISA Transactions、IET Control Theory and Applications、International Journal of Systems Science等多个国际期刊的审稿人。
办公地点:西安工业大学未央校区工5楼306办公室
电子邮箱:yankun@xatu.edu.cn
通信地址:陕西省西安市未央区学府中路2号(365体育官方唯一入口)
2.教育背景
2016-04至2020-06,南京航空航天大学,自动化学院,博士
2012-09至2015-06,兰州理工大学,电气工程与信息工程学院,硕士
2008-09至2012-06,兰州理工大学,电气工程与信息工程学院,本科
3.学科领域、研究方向领域
学科领域:控制理论与控制工程、导航制导与控制、控制工程、人工智能
研究方向领域:1.无人机的抗扰容错控制;
2.多约束条件下的无人机安全优化飞行控制;
3.多无人机自主避障与路径规划。
4.主持或参加的科研项目
1.国家自然科学基金委员会,青年项目, 62103315,多约束条件下的无人直升机系统安全优化飞行控制研究, 2022-01至2024-12, 30万元,在研,主持
2.陕西省教育厅,一般项目, 21JK0686,复杂环境下的中型无人直升机鲁棒容错与最优跟踪控制研究, 2021-01至2022-12, 2万元,在研,主持
3.国家自然科学基金委员会,杰出青年基金项目, 61825302,大机动无人机智能控制基础理论与应用, 2019-01至2023-12, 350万,在研,参与
5.代表论著、专著、教材与学术论文(如发表SCI、EI论文被检索,请将检索号备注在该篇论文后)
[1] Kun Yan, Haipeng Ren. Fault identification and fault-tolerant control for unmanned autonomous helicopter with global neural finite-time convergence.Neurocomputing, 2021, 459:165-175.(SCI二区:000711066300015)
[2] Mou Chen,Kun Yan, Qingxian Wu.Multi-approximatorbasedfaulttoleranttrackingcontrol forunmannedautonomoushelicopter withinputsaturation.IEEE Transactions on Systems, Man, and Cybernetics: Systems.(SCI一区:已录用)
[3] Kun Yan, Qingxian Wu.Adaptivetrackingflightcontrol forunmannedautonomoushelicopter withfullstateconstraints andactuatorfaults.ISATransactions. (SCI二区:已录用)
[4] Kun Yan, Mou Chen, Qingxian Wu, Bin Jiang. Extended state observer-based sliding mode fault-tolerant control for unmanned autonomous helicopter with wind gusts.IET Control Theory & Applications, 2019, 13(10): 1500-1513. (SCI二区: 000471712200009)
[5] Kun Yan, Mou Chen, Qingxian Wu, Ronggang Zhu.Robust adaptive compensation control for unmanned autonomous helicopter with input saturation and actuator faults.Chinese Journal of Aeronautics, 2019, 32(10): 2299-2310. (SCI二区: 000496245700007)
[6] Kun Yan, Mou Chen, Qingxian Wu, Yuhui Wang, Ronggang Zhu. Prescribed performance fault tolerant control for uncertain nonlinear systems with input saturation.International Journal of System Science, 2020, 51(2): 258-274. (SCI三区: 000504361500001)
[7] Kun Yan, Mou Chen, Bin Jiang, Qingxian Wu.Robust adaptive active fault-tolerant control of UAH with unknown disturbances and actuator faults.International Journal of Adaptive Control and Signal Processing, 2019, 33(4): 684-711.(SCI三区: 000462886600007)
[8] Kun Yan, Mou Chen, Qingxian Wu, Ke Lu. Robust attitude fault-tolerant control for unmanned autonomous helicopter with flapping dynamics and actuator faults.Transactions of the Institute of Measurement and Control, 2019, 41(5): 1266-1277.(SCI四区: 000459877200007)
[9] Kun Yan, Mou Chen, Qingxian Wu.Neural network-based adaptive fault tolerant tracking control for unmanned autonomous helicopters with prescribed performance.Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2019, 233(12): 4350-4362. (SCI四区: 000482461700005)
[10]Kun Yan, Mou Chen, Qingxian Wu, Yuhui Wang. Adaptive flight control for unmanned autonomous helicopter with external disturbance and actuator fault. IET The Journal of Engineering, 2019, 22: 8359-8364. (EI: 19176194)
[11]Kun Yan, Qingxian Wu, Mou Chen. Robust adaptive backstepping control for unmanned autonomous helicopter with flapping dynamics. 13th IEEE International Conference on Control and Automation, 2017: 1027-1032, Ohrid, Macedonia, 2017.07.03-06. (EI收录)
[12]Kun Yan, Qingxian Wu, Mou Chen(*). LQR-based optimal tracking fault tolerant control for a helicopter with actuator faults. 7th IEEE International Conference on Data Driven Control and Learning Systems, 2018: 1022-1027, Enshi, China, 2018.05.25-27. (EI收录)
[13]Kun Yan, Qingxian Wu, Mou Chen. Robust fault tolerant tracking control for unmanned autonomous helicopter with disturbance. 37th Chinese Control Conference, 2018: 375-380, Wuhan, China, 2018.07.25-27. (EI收录)
[14]Kun Yan, Qingxian Wu, Chenguang Yang, Mou Chen. Backstepping-based adaptive fault-tolerant control design for satellite attitude system. 2020 International Conference on Unmanned Aircraft Systems, 2020: 176-181, Athens, Greece, 2020.09.01-04. (EI收录)
6.授权/受理发明专利(实用新型、软著)
[1] 阎坤,陈超波,张玉芳。一种执行器故障下的无人直升机姿态控制方法,2021-04-25,已受理,中国,专利号:202110445982.5.
[2] 阎坤,陈超波,张玉芳。一种无人直升机自抗扰容错控制方法,2021-04-25,已受理,中国,专利号:202110446006.1.
[3] 阎坤,陈超波,韩士成。一种无人直升机预设性能控制方法,2021-04-30,已受理,中国,专利号:202110480646.4.
[4] 阎坤,陈超波,韩士成。一种基于预设性能的不确定非线性系统抗饱和容错控制方法,2021-04-30,已受理,中国,专利号:202110480634.1.
[5] 陈谋,阎坤,吴庆宪,姜斌,盛守照,邵书义,张柯。一种无人直升机鲁棒容错跟踪方法,2020-03-20,中国,专利号:ZL 2019 1 0139758.6.
[6] 陈谋,阎坤,吴庆宪,姜斌,盛守照,邵书义。一种无人直升机鲁棒容错跟踪控制方法,2020-03-17,中国,专利号:ZL 2019 1 0129260.1.
[7] 陈谋,阎坤,吴庆宪,姜斌,盛守照,邵书义,甑子洋。一种无人直升机鲁棒自适应补偿控制方法,2020-03-17,中国,专利号:ZL 2019 1 0132355.9.
7.获得奖励/荣誉(科研、教学等)
阎坤(1/3);最佳会议论文奖,江苏省自动化学会, 2019.06