朱宏玉
职称\职位:讲师/硕士研究生指导教师
出生年月:
电子邮箱:henry.jewel@buaa.edu.cn 办公地点:北航新主楼C座1023
办公电话:


基本情况


教育经历
2004.09. - 2009.07. 哈尔滨工业大学飞行器设计专业博士
2002.09. - 2004.07. 哈尔滨工业大学飞行器设计专业硕士
1995.09. - 1999.07. 哈尔滨工业大学航天工程与力学系本科
工作经历
2010.03. - 现在 讲师/硕士研究生指导教师
北京航空航天大学宇航学院航天制导导航与控制系
1999.07. - 2002.08. 设计员/主管设计师
江西洪都航空工业集团有限责任公司六六〇设计研究所

Gender: Male Degree: Ph.D. Position: Lecturer
Office Add: B1023, NMB Tel: ** E-mail: henry.jewel@buaa.edu.cn
Research Interests: Dynamics and Control of Spacecraft
Education History
2009.07. Ph.D. in Aeronautics and Astronautics at Harbin Institute of Technology
2004.07. M.Sc. in Aeronautics and Astronautics at Harbin Institute of Technology
1999.07. B.Sc. in Astronautic Engineering and Mechanics at Harbin Institute of Technology
Work Experiences
2010.03. - Today Lecture
Department of Guidance, Navigation and Control, School of Astronautics, Beihang University
1999.07. - 2002.08. Engineer
Liuliuling Institute, Hongdu Aviation Industry Group LTD
Paper Published
a. Academic Journal Papers：
ZHU Hong-Yu. Normal-Matrix-Based Nonlinear H∞ Attitude Tracking for Spacecraft. Aircraft Engineering and Aerospace Technology, 2010, 82(3): 175-183.
ZHU Hong-Yu. Feedback-perturbation-based normal matrix approach for spacecraft attitude control. Aerospace Control and Application, 2009, 35(3): 53-57. (in Chinese)
ZHU Hong-Yu, CUI Ping-Yuan, CUI Hu-tao. Normal matrix design approach for autonomous attitude control of spacecraft. Journal of Jilin University (Engineering and Technology Edition), 2008, 38(Sup.2): 275-280. (in Chinese)
b. Academic Conference Papers：
XU Hong, ZHU Hong-Yu. Approach of robust pole assignment based on normal matrix. 2nd International Conference on Electrical and Control Engineering, Yichang, Hubei, China, September 16-18, 2011: 3377-3380.
ZHU Hong-Yu, XU Shi-Jie. Feedback-linearization-based spacecraft attitude maneuver normal-matrix control. 14th National Academic Conference on Space and Moving-body Control Technology, Jiuzhaigou, Aba, Sichuan, China, July 24-25, 2010: 225-230. (in Chinese)
ZHU Hong-Yu. Robust attitude control for spacecraft based on normal matrix and pattern search. 6th AIAA Infotech@Aerospace Conference, Atlanta, Georgia, America, April 20-22, 2010: AIAA-2010-3494.
ZHU Hong-Yu. Normal matrix design methodology of spacecraft robust attitude control, AIAA Guidance, Navigation, and Control Conference, Chicago, Illinois, America, August 10-13, 2009: AIAA-2009-6208.
CUI Ping-Yuan, ZHU Hong-Yu. Nonlinear H∞ normal matrix attitude control of spacecraft. 2009 Chinese Control and Decision Conference, Guilin, Guangxi, China, June 17-19, 2009: 1404-1409.
ZHU Hong-Yu, CUI Ping-Yuan, CUI Hu-Tao, Autonomous design of spacecraft attitude control based on normal matrix and genetic algorithm. 2008 Chinese Control and Decision Conference, Yantai, Shangdong, China, 2-4 July 2008, 3415-3420.


研究方向


飞行器动力学与控制


发表论文


a. 学术期刊：
ZHU Hong-Yu. Normal-Matrix-Based Nonlinear H∞ Attitude Tracking for Spacecraft. Aircraft Engineering and Aerospace Technology, 2010, 82(3): 175-183.
朱宏玉. 基于反馈摄动的航天器姿态正规矩阵控制. 空间控制技术与应用, 2009, 35(3): 53-57.
朱宏玉, 崔平远, 崔祜涛. 航天器自主姿态控制的正规矩阵设计方法. 吉林大学学报（工学版）, 2008, 38(增刊2): 275-280.
b. 学术会议：
XU Hong, ZHU Hong-Yu. Approach of robust pole assignment based on normal matrix. 2nd International Conference on Electrical and Control Engineering, Yichang, Hubei, China, September 16-18, 2011: 3377-3380.
朱宏玉, 徐世杰. 基于反馈线性化的航天器姿态机动正规矩阵控制. 全国第十四届空间及运动体控制技术学术会议, 四川省阿坝藏族羌族自治州九寨沟县, 2010年7月24-25日: 225-230.
ZHU Hong-Yu. Robust attitude control for spacecraft based on normal matrix and pattern search. 6th AIAA Infotech@Aerospace Conference, Atlanta, Georgia, America, April 20-22, 2010: AIAA-2010-3494.
ZHU Hong-Yu. Normal matrix design methodology of spacecraft robust attitude control, AIAA Guidance, Navigation, and Control Conference, Chicago, Illinois, America, August 10-13, 2009: AIAA-2009-6208.
CUI Ping-Yuan, ZHU Hong-Yu. Nonlinear H∞ normal matrix attitude control of spacecraft. 2009 Chinese Control and Decision Conference, Guilin, Guangxi, China, June 17-19, 2009: 1404-1409.
ZHU Hong-Yu, CUI Ping-Yuan, CUI Hu-Tao, Autonomous design of spacecraft attitude control based on normal matrix and genetic algorithm. 2008 Chinese Control and Decision Conference, Yantai, Shangdong, China, 2-4 July 2008, 3415-3420.
Research interests: Guidance and control of near space vehicle
Education
Bachelor of Engineering, School of Astronautics, Beihang University, 2005;
Master of Engineering, School of Astronautics, Beihang University, 2007;
Visiting student, Department of Aerospace engineering, Iowa State University,2008-2009;
Ph.D., School of Astronautics, Beihang University, 2010;
Experience
2011.3-present: Lecturer at Department of Guidance, Navigation, and Control for Aerospace, School of Astronautics, Beihang University, Beijing, China.
Research activities
Focus on guidance and control of near space vehicle under the sponsorship of foundations and projects. More than 10 papers were published in journals and conference proceedings.