西北工业大学航天学院研究生导师代洪华介绍如下：

基本信息 The basic information

姓名: 代洪华
学院: 航天学院
学历: 博士研究生毕业
学位: 博士
职称: 副教授
学科: 航空宇航科学-飞行器设计
邮箱: hhdai@nwpu.edu.cn
电话: 029-88493685-807

工作经历 Work Experience

2014 - 至今，西北工业大学，航天学院，副教授

2014 - 至今，航天飞行动力学技术重点实验室，副教授

教育经历 Education Experience

2009 - 2014，西北工业大学，航天学院，博士
2010 - 2012，University of California, Irvine，MAE，联合培养博士
2005 - 2009，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. 硕士生课程：非线性动力学（40学时）

招生信息 Admission Information

招收飞行器设计专业硕士生。研究方向包括：

1、非线性动力学与控制

2、计算方法及其在工程中的应用

3、航天器微振动抑制理论与实验研究

荣誉获奖 Awards Information

Outstanding Young Investigator Award, 国际计算与实验科学工程大会, 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（2016）

陕西省优秀博士论文（2017）

陕西省科学技术二等奖（2013）

陕西省高等学校科学技术一等奖（2013） 

科学研究 Scientific Research

代洪华，男，山东聊城人，副教授，硕士生导师。从事的研究领域有：（1）计算结构动力学；（2）柔性航天器动力学与控制；（3）流固耦合力学。截至目前，已在Journal of Computational Physics，Journal of Fluids and Structures, Nonlinear Dynamics, JSV, JGCD, AIAA J.等国际著名力学期刊上发表SCI论文20余篇，其中ESI高被引论文2篇。作为项目负责人主持国家自然基金项目、国家863项目等5项。

学术成果 Academic Achievements

1. 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, in press.
 2. H.H. Dai, X.C. Wang, M. Schnoor, X.C. Wang, S.N. Atluri. Analysis of internal resonance in a two-degree-of-freedom nonlinear dynamical system, Communications in Nonlinear Science and Numerical Simulation, 49, pp.176-191, 2017.
 3. 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), pp.513-530, 2017.
 4. X. Wang, X. 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), pp.2442-2451, 2017.
 5. C. Wei, J. Luo, H.H. Dai, Z. Yin, J. Yuan. Low complexity differentiator based decentralized fault-tolerant control of uncertain large-scale nonlinear systems with unknown dead zone, Nonlinear Dynamics, 89 (4), pp.2573-2592, 2017.
 6. H.H. Dai, X.K. Yue, J.P. Yuan. Half-order optimally scaled Fourier expansion method for solving nonlinear dynamical system, International Journal of Non-Linear Mechanics, 87, pp.21-29, 2016.
 7. H.H. Dai, X.K.Yue, J.P. 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, 2015.
 8. H.H. Dai, X.K. Yue, J.P. 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, pp.214-237, 2014.
 9. 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), pp. 7267-7285, 2014.
 10. 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), pp.195-226, 2014.
 11. 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, pp.342-351, 2014.
 12. 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), pp.1455-1468, 2014.
 13. H.H. Dai, X.K. Yue, J.P. Yuan, D. Xie. A fast harmonic balance technique for periodic oscillations of an aeroelastic airfoil. Journal of Fluids and Structures, 50, pp. 231-252, 2014.
 14. 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, pp. 271-291, 2014.
 15. X.K. Yue, X.C. Wang, H.H. Dai. A Simple Time Domain Collocation Method to Precisely Search for Periodic Orbits of Satellite Relative Motions. Mathematical Problems in Engineering, 2014, pp.1-15, 2014.
 16. P. Li, X.K. Yue, H.H. Dai. 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.
 17. H.H. Dai, X.K. Yue, J.P. Yuan. A time domain collocation method for obtaining the third superharmonic solutions to the Duffing oscillator. Nonlinear Dynamics, 73(1-2), pp.593-609, 2013.
 18. 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: Subharmonic Oscillations. CMES: Computer Modeling in Engineering & Sciences, 84(5), pp.459-497, 2012.
 19. H.H. Dai, J.K. 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), pp.69-99, 2011.
 20. H.H. Dai, J.K. 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), pp.155-185, 2011.
 21. C.S. Liu, H.H. Dai, S.N. Atluri. Iterative Solution of a System of Nonlinear Algebraic Equations. CMES: Computer Modeling in Engineering & Sciences, 81(4), pp.335-362, 2011.
 22. C.S. Liu, H.H. Dai, S.N. Atluri. A Further Study on Iteratively Solving the Nonlinear System of Algebraic Equations. CMES: Computer Modeling in Engineering & Sciences, 81(2), pp.195-227, 2011.
 23. X.K. Yue, J. Chen, H.H. Dai.  Pseudospectral control for 6-DOF electromagnetic formation flying. Journal of Aerospace Engineering: Part G, 2015.

社会兼职 Social Appointments

AIAA Senior Member
国际ICCES会议Aerospace Flight Dynamics and Control分会主席
 陕西省振动工程学会常务理事
 国际期刊AIAA J., JGCD, Journal of Fluids and Structures, Nonlinear Dynamics, Journal of Sound and Vibration, IJNM等20多个国际期刊审稿人

团队信息 Team Information

本人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。实验室以提高空间平台机动性能以及综合应用能力为目标，开展航天飞行动力学和控制应用基础理论与关键技术研究，进行新概念、新理论、新方法、新技术的探索性和开创性研究与实验。一直以来，实验室秉承“开放、流动、联合、竞争”的宗旨，开拓创新，锐意进取，各项事业取得长足发展。为了推动实验室建设，加强人才培养，实验室充分发挥西北工业大学的教育特色和优势，吸引更多的优秀人才了解航天、热爱航天、投身航天事业。团队给学习科研优异的学生提供出国深造的机会，并与美国、德国、香港等国家和地区建立了学生互访和学术交流。欢迎有志从事航天事业的学生加入我们的团队。