代洪华


的个人主页 http://teacher.nwpu.edu.cn/honghuadai

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基本信息 The basic information

代洪华

航天学院

博士研究生毕业

博士

教授

院长助理

航空宇航科学-飞行器设计,航空宇航科学-空间应用科学与工程

hhdai@nwpu.edu.cn

工作经历 Work Experience

2019.07 - 至今, 西北工业大学,航天学院,教授、博导

2016.12 - 2018.12, 香港理工大学,机械工程系,博士后

2014.11 - 2019.06, 西北工业大学,航天学院,副教授

2014.11 - 2019.06, 航天飞行动力学技术重点实验室,副教授

教育经历 Education Experience

2009.09 - 2014.11,西北工业大学,航天学院,博士
2010.09 - 2012.08,University of California, Irvine,机械与宇航工程学院,联合培养博士
2005.09 - 2009.07,西北工业大学,机电学院,本科

教育教学 Education And Teaching

课程教学

1. 本科生课程:Flight Dynamics(英文课程40学时)

2. 本科生课程:在轨服务技术基础(40学时)

3. 硕士生课程:航天器非线性动力学(40学时)

招生信息 Admission Information

博士招生专业:飞行器设计、空间应用科学与工程、力学、控制科学与工程 博士生 2-3 名

硕士招生专业:飞行器设计、航天工程、机械、力学 硕士生 3-4 名

欢迎积极进取、有上进心,具备扎实力学、数学基础学生报考(推免及竞赛获奖者优先)。学生培养方面:团队与加拿大多伦多大学、英国曼彻斯特大学、意大利都灵理工大学、香港理工大学等高校建立了硕士联培、博士联培、联培双学位(2+2)、攻读博士学位的合作项目,鼓励优秀研究生留学深造。对于专业硕士、工程博士,将推荐赴中科院微小卫星研究院、航天八院、中科院空间工程中心、上海交通大学等单位进行3-6个月的实习和访学机会。培养研究生解决工程问题的能力。

常年招收动力学与控制、力学和计算方法背景的博士后。联系方式:hhdai@nwpu.edu.cn(请附简历)


研究方向包括:

1、空间目标抓捕与控制理论与地面实验

2、非线性动力学与控制

3、计算方法及其在工程中的应用

4、航天器微振动抑制理论与实验研究

荣誉获奖 Awards Information

军科委“青托”(2019)

陕西省技术发明一等奖(2020)

Outstanding Young Investigator Award, 第23届ICCES国际会议, 葡萄牙(2017)

陕西省科学技术一等奖(2015)

西工大“翱翔新星”(2016)

“香江学者”博士后(2016)

国家863十二五优秀创新团队(2016)

陕西省优秀博士论文(2017)

国家奖学金(2008,2012,2013,2014)

科学研究 Scientific Research

代洪华,男,教授,博士生导师,山东聊城人,航天学院空间操作技术研究所副所长。从事研究领域有:(1)在轨服务动力学仿真与高性能计算;(2)航天器动力学与控制;(3)空间抓捕与控制地面试验;(4)非线性动力学。截至目前,已在MSSP, JGCD, Journal of Computational Physics,Journal of Fluids and Structures, Nonlinear Dynamics, JSV, AIAA J.等国际著名力学期刊上发表SCI论文40余篇,其中ESI高被引论文2篇。作为项目负责人主持JCJQ项目课题、国家自然基金面上项目、青年项目、JKW创新特区项目、国家863项目等13项。

学术成果 Academic Achievements

论文:

  • H.H. Dai*, X.Y. Cao, X.J. Jing, X. Wang, X.K. Yue. Bio-inspired anti-impact manipulator for capturing non-cooperative spacecraft: theory and experiment, Mechanical Systems and Signal Processing, 142: 106785, 2020. (WOS:000430627700008)

  • H.H. Dai*, X.K. Yue. Preface: Nonlinear Computational and Control Methods in Aerospace Engineering, Computer Modeling in Engineering & Sciences, 122(1): 1~4, 2020. WOS:000509734200001

  • H.H. Dai*, X.J. Jing*, C. Sun, Y. Wang, X.K. Yue. Accurate modeling and analysis of a bio-inspired isolation system: with application to on-orbit capture, Mechanical Systems and Signal Processing, 109: 111~133, 2018. WOS:000430627700008

  • H.H. Dai*, X.J. Jing, Y. Wang, X.K. Yue, J.P. Yuan. Post-capture vibration suppression of spacecraft via a bio-inspired isolation system, Mechanical Systems and Signal Processing, 105: 214~240, 2018. WOS:000424188600013

  • H.H. Dai, X.K. Yue, J.P. Yuan, D. Xie. Dealiasing harmonic balance method for obtaining periodic solutions of an aeroelastic system, Aerospace Science and Technology, 77: 244~255, 2018. WOS:000434744700023

  • H.H. Dai*, X.C. Wang*, S. Matt, S.N. Atluri. Analysis of internal resonance in a two-degree-of-freedom nonlinear dynamical system, Communications in Nonlinear Science and Numerical Simulation, 49: 176~191, 2017. WOS:000396974900015

  • H.H. Dai*, X.K. Yue, J.P. Yuan, D. Xie. Half-order optimally scaled Fourier expansion method for solving nonlinear dynamical system, International Journal of Non-Linear Mechanics, 87: 21~29, 2016. WOS:000388048500002

  • H.H. Dai*, X.K. Yue, J. Yuan, D. Xie, S.N. Atluri. A comparison of classical Runge-Kutta and Henon’s methods for capturing chaos and chaotic transients in an aeroelastic system with freeplay nonlinearity. Nonlinear Dynamics, 81(1-2):  169-1882015. WOS:000355919700013

  • H.H. Dai*, X.K. Yue, J. Yuan, S.N. Atluri. A time domain collocation method for studying the aeroelasticity of a two dimensional airfoil with a structural nonlinearity. Journal of Computational Physics, 270: 214-237, 2014. WOS:000336406200012

  • H.H. Dai, X.K. Yue*, J. Yuan, D. Xie. A fast harmonic balance technique for periodic oscillations of an aeroelastic airfoil. Journal of Fluids and Structures, 50:  231-252, 2014. WOS:000343614000014

  • H.H. Dai*, X.K. Yue, D. Xie, S.N. Atluri. Chaos and chaotic transients in an aeroelastic system. Journal of Sound and Vibration, 333(26): 7267-7285, 2014. WOS:000343555900012

  • H.H. Dai*, X.K. Yue, S.N. Atluri. Solutions of the von Karman plate equations by a Galerkin method, without inverting the tangent stiffness matrix. Journal of Mechanics of Materials and Structures, 9(2): 195-226, 2014. WOS:000338425200004

  • H.H. Dai*, X.K. Yue, C.S. Liu. A multiple scale time domain collocation method for obtaining approximate solutions for nonlinear dynamical systems. International Journal of Non-Linear Mechanics, 67: 342-351, 2014. WOS:000347022100038

  • H.H. Dai*, X.K. Yue, J. Yuan. A time domain collocation method for obtaining the third superharmonic solutions to the Duffing oscillator. Nonlinear Dynamics, 73(1-2): 593-609, 2013. WOS:000320954900048

  • H.H. Dai*, M. Schnoor, S.N. Atluri. A Simple Collocation Scheme for Obtaining the Periodic Solutions of the Duffing Equation, and its Equivalence to the High Dimensional Harmonic Balance Method. Computer Modeling in Engineering & Sciences, 84(5): 459-497, 2012. WOS:000305925900004

  • H.H. Dai*, J. Paik, S.N. Atluri. The Global Nonlinear Galerkin Method for the Analysis of Elastic Large Defections of Plates under Combined Loads: A Scalar Homotopy Method for the Direct Solution of Nonlinear Algebraic Equations. Computers, Materials & Continua, 23(1): 69-99, 2012. WOS:000293611400004

  • H.H. Dai*, J. Paik, S.N. Atluri. The Global Nonlinear Galerkin Method for the Solution of von Karman Nonlinear Plate Equations: An Optimal & Faster Iterative Method for the Direct Solution of Nonlinear Algebraic Equations. Computers, Materials & Continua, 23(2): 155-185, 2011. WOS:000294099500004

  • C. Wei, J.J. Luo*, H.H. Dai*, Z.L. Bian, J.P. Yuan. Learning-based adaptive prescribed performance control of postcapture space robot-target combination without inertia identifications, Acta Astronautica, 146: 228~242, 2018. WOS:000432508700026

  • J.J. Luo, C. Wei*, H.H. Dai*, Z.Y. Yin, X. Wei, J.P. Yuan. Robust inertia-free attitude takeover control of postcapture combined spacecraft with guaranteed prescribed performance, ISA transactions, 74: 28~44, 2018. WOS:000428971100003

  • C. Wei, J.J. Luo*, H.H. Dai*, Z.Y. Yin, J.P. Yuan. Low-complexity differentiator-based decentralized fault-tolerant control of uncertain large-scale nonlinear systems with unknown dead zone, Nonlinear Dynamics, 89(4): 2573~2592, 2017. WOS:000407970600019

  • C. Ma, H.H. Dai*, J.P. Yuan*. Estimation of inertial characteristics of tumbling spacecraft using constant state filter, Advances in Space Research, 60(3): 513~530, 2017. WOS:000404793400002

  • X.C. Wang, X.K. Yue*, H.H. Dai*, J.P. Yuan. Analysis of a Two-Dimensional Aeroelastic System Using the Differential Transform Method, Journal of Computational and Nonlinear Dynamics, 11(6):1~16, 2016. WOS:000394148900015

  • X.K. Yue, H.H. Dai*, C.S. Liu. Optimal scale polynomial interpolation technique for obtaining periodic solutions to the Duffing oscillator. Nonlinear Dynamics, 77(4): 1455-1468, 2014. WOS:000340564600027

  • D. Xie, M. Xu, H.H. Dai*, E.H. Dowell. Observation and Evolution of Chaos for a Cantilever Plate in Supersonic Flow. Journal of Fluids and Structures, 50: 271-291, 2014. WOS:000343614000016

  • D. Xie, M. Xu, H.H. Dai*, T. Chen. New look at nonlinear aerodynamics in analysis of hypersonic panel flutter, Mathematical Problems in Engineering, 2017: 6707092, 2017. WOS:000398480400001

  • X. Wang*, X.K. Yue*, H.H. Dai, J.P. Yuan. Vibration suppression for post-capture spacecraft via a novel bio-inspired Stewart isolation system, Acta Astronautica, 168: 1~22, 2020. WOS: 000514016900001

  • D. Xie*, M. Xu, H.H. Dai. Effects of damage parametric changes on the aeroelastic behaviors of a damaged panel, Nonlinear Dynamics, 97(2): 1035~1050, 2019. WOS: 000479263300009

  • C. Ma, H.H. Dai, C.S. Wei, J.P. Yuan*. Two-stage filter for inertia characteristics estimation of high-speed tumbling targets, Aerospace Science and Technology, 89: 333~344, 2019. WOS: 000469896800028

  • Y. Wang*, X.J. Jing*, H.H. Dai, F.M. Li. Subharmonics and ultra-subharmonics of a bio-inspired nonlinear isolation system, International Journal of Mechanical Sciences, 152: 167~184, 2019. WOS: 000459837400012

  • C.S. Wei, J.J. Luo*, C. Ma*, H.H. Dai, J.P. Yuan. Event-triggered neuroadaptive control for postcapture spacecraft with ultralow-frequency actuator updates, Neurocomputing, 315: 310~321, 2018. WOS: 000445934400030

  • X.K. Yue*, T. Zhang, H.H. Dai, X. Ning, J.P. Yuan. Postcapture stabilization of space robots considering actuator failures with bounded torques, Chinese Journal of Aeronautics, 31(10): 2034~2048, 2018. WOS: 000446502300009

  • C.S. Wei*, J.J. Luo, H.H. Dai, J.P. Yuan. Adaptive model-free constrained control of postcapture flexible spacecraft: a Euler–Lagrange approach, Journal of Vibration and Control, 24(20): 4885~4903, 2018. WOS: 000445778100016

  • C.S. Wei*, J.J. Luo, H.H. Dai, G.R. Duan. Learning-based adaptive attitude control of spacecraft formation with guaranteed prescribed performance, IEEE transactions on cybernetics, 49(11): 4004~4016, 2018. WOS: 000476811000015

  • J.J. Luo, C.S. Wei*, H.H. Dai, J.P. Yuan. Robust LS-SVM-based adaptive constrained control for a class of uncertain nonlinear systems with time-varying predefined performance, Communications in Nonlinear Science and Numerical Simulation, 56: 561~587, 2018. WOS: 000412682700041

  • C.S. Wei, J.J. Luo*, H.H. Dai, Z.Y. Yin, W.H. Ma, J.P. Yuan. Globally robust explicit model predictive control of constrained systems exploiting SVMbased approximation, International Journal of Robust and Nonlinear Control, 27(16): 3000~3027, 2017. WOS: 000413011200020

  • X.C. Wang*, X.K. Yue, H.H. Dai, S.N. Atluri. Feedback-accelerated Picard iteration for orbit propagation and Lambert’s problem, Journal of Guidance, Control, and Dynamics, 40(10): 2442-2451, 2017. WOS: 000410701500004

  • B. Zhang, J.F. Pan*, J.P. Yuan, W.F. Rao, L. Qiu, J.J. Luo, H.H. Dai. Tracking control with zero phase-difference for linear switched reluctance machines network, Energies, 10(7): 949, 2017. WOS: 000406700200120

  • C.S. Wei, J.J. Luo*, H.H. Dai, J.P. Yuan, J.F. Xie. Efficient adaptive constrained control with time-varying predefined performance for a hypersonic flight vehicle, International Journal of Advanced Robotic Systems, 14(2): 1729881416687504, 2017. WOS: 000400496000001

  • X.K. Yue*, J. Chen, H.H. Dai, J.P. Yuan, J.W. Hou. Pseudospectral control for 6-DOF electromagnetic formation flying, Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 229(12): 2231~2241, 2015. WOS: 000361593300007

  • D. Xie*, M. Xu, H.H. Dai, E.H. Dowell. Proper orthogonal decomposition method for analysis of nonlinear panel flutter with thermal effects in supersonic flow, Journal of Sound and Vibration, 337: 263~283, 2015. WOS: 000345634800016

  • X.K. Yue*, H.H. Dai, J.P. Yuan. Stochastic bifurcation in a model of love with colored noise, International Journal of Modern Physics C, 26(02): 1550021, 2015. WOS: 000350338800010

  • X.K. Yue, X.C. Wang*, H.H. Dai. A simple time domain collocation method to precisely search for the periodic orbits of satellite relative motion, Mathematical Problems in Engineering, 2014: 854967, 2014. WOS: 000344297600001

  • P. Li*, X.K. Yue, H.H. Dai, X.B. Chi. Real-time terminal guidance for autonomous spacecraft capture of free floating objects using model predictive control, International Journal of Space Science and Engineering 5, 2(2): 190~204, 2014.

  • C.S. Liu*, H.H. Dai, S.N. Atluri. A Further Study on Using  and  in Iteratively Solving the Nonlinear System of Algebraic Equations F(x) = 0, Computer Modeling in Engineering and Sciences, 81(2): 195~227, 2011. WOS:000301207600003

  • C.S. Liu*, H.H. Dai, S.N. Atluri. Iterative Solution of a System of Nonlinear Algebraic Equations F(x) = 0, Using  or  is a Normal to a Hyper-Surface Function of F, P Normal to R, and P* Normal to F, Computer Modeling in Engineering & Sciences, 81(3-4): 335~362, 2011. WOS:000301207800006

 

专利:

  • 代洪华,马川,侯翔昊,王姣,袁建平,一种非接触式的翻滚卫星的惯性参数的测算方法,专利号CN 2016108645808。(已授权)

  • 马川,代洪华,张军华,葛菊祥,袁建平,一种用于空间对接的陀螺式能量转换装置及方法,专利号CN 2016108649777。(已授权)

  • 代洪华,张滕,马川,岳晓奎,袁建平,一种适用于空间机器人执行器故障下的快速姿态稳定方法,专利号CN 2017100940468。(已授权)

  • 代洪华,魏才盛,马川,汪雪川,基于LS-SVM的高超声速飞行器自适应时变预设性能控制方法,专利号CN 2016111808641。(已授权)

  • 代洪华,孙冲,袁建平,陈建林,张军华,葛菊祥,日-地三体引力场中的晕轨道航天器偏置轨道设计方法,专利号CN 2016104961666。(已授权)

  • 代洪华,陈建林,袁建平,孙冲,一种基于太阳帆推进技术的航天器日心椭圆悬浮轨道设计方法,专利号CN 2016104968171。(已授权)

  • 代洪华,汪雪川,孙冲,岳晓奎,袁建平,地球摄动引力场中近地航天器相对运动轨道的保持方法,专利号CN 2016108604333。(已授权)

项目:

  • 军委科技委,基础加强项目课题,***高性能算法,2020-07至2023-06,350万元,主持

  • 家自然科学基金委,面上项目,12072270 , 空间旋转非合作航天器柔顺消旋动力学与控制,2021-01至2024-12,62万元,主持

  • 军委科技委,国防创新特区项目,***柔顺消旋动力学与控制,2019-09至2020-12,80万元,主持

  • 军委科技委,青托人才项目,***控制技术,2019-09至2021-12,120万元,主持

  • 装备发展部,装备预研基金,61422100319,空间轨道转移问题的高效高精度数值方法研究,2019-01至2020-12,10万元,主持

  • 航天八院,横向课题,TW-1星星间分离机构研制,2018-09至2018-12,40万元,参与

  • 陕西省科技厅,陕西省自然科学基金,2017JM1006,非合作目标的逼近/抓捕动力学研究,2017-07至2019-06,3万元,主持

  • 国家自然科学基金委,重大项目(子课题),61690211,空间非合作目标交会的多约束智能自主规划与控制,2017-01至2020-12,304.5万元,参与

  • 总装备部,国家973项目(子课题),***在轨抓捕动力学与镇定,2016-07至2020-06,827万元,参与

  • 国家自然科学基金委,青年项目,11502203,间隙非线性颤振系统的极限环及响应分析方法研究,2016-01至2018-12,20万元,主持

  • 总装备部,国家863项目,2015AA**504,航天器***抓捕及***协同控制,2015-07至2016-06,70万元,主持

  • 总装备部,国家863重点项目,***碎片清理技术,2015-07至2016-06,450万元,参与

  • 总装备部,重点实验室基金,***自主交会凸优化制导方法,2016-07至2017-06,5万元,主持

社会兼职 Social Appointments

国际SCI期刊Computer Modeling in Engineering and Sciences编委(2019-)

《应用力学学报》编委(2021-)

《动力学与控制学报》青年编委(2021-)

中科院青年创新促进会首批特邀会员(2019)

国际ICCES会议组委会委员(2017、2019、2020)

AIAA Senior Member(2017-)
国际ICCES会议Aerospace Flight Dynamics and Control分会主席(2017)
陕西省振动工程学会常务理事(2017-)

团队信息 Team Information

所在团队航天飞行动力学技术重点实验室成立于2010年12月,由北京航天飞行控制中心和西北工业大学联合设立。研究生培养采用工程型号与国际化培养两种模式。对于硕士研究生,给予赴航天八院、中科院微小卫星中心、北京航天飞控中心实习3-6个月的机会,接触航天型号任务,培养解决实际问题的能力。此外,鼓励学习优异的学生出国深造,博士生出国率(联培、攻读学位)近半数,主要留学国家为美国、德国、加拿大、澳大利亚、西班牙等。团队与美国、德国、香港等国家和地区建立了长期学生互访和学术交流。欢迎有志从事航天事业的学生加入团队,勇攀航天科技高峰,联系方式:hhdai@nwpu.edu.cn