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Dep. of Aerospace Information and Control

Wu Shufan

 

Professional experience

Time

Institution

Position

05/2018 – Present

School of Aeronautics and Astronautics, Shanghai Jiao Tong University (SJTU), China

Executive Vice Dean, Chair Professor, Doctoral Advisor

07/2017 – 04/2018

School of Aeronautics and Astronautics, Shanghai Jiao Tong University (SJTU), China

Chair Professor, Doctoral Advisor

10/2015 – 06/2017

ShanghaiTech University, China

Distinguish Professor (adjunt)

06/2013 – 06/2017

Shanghai Engineering Centre for Microsatellites (SECM), Chinese Academy of Science (CAS), China

Chief Technology Officer

10/2005 – 05/2013

 European Space Research and Technology Center (ESTEC), European Space Agency (ESA), The Netherlands

Fellow Engineer

04/2002 – 09/2005

 European Space Research and Technology Center (ESTEC), European Space Agency (ESA), the Netherlands

Senior Engineer

01/2000 – 04/2002

 Surrey Space Center, Surrey University, UK

Research Fellow

12/1998 – 12/1999

 Faculty of Aerospace Engineering, Delft Univeristy of Technology, The Netherlands

Research Fellow

04/1998 – 03/2003

 School of Automation, Nanjing University of Aeronautics and Astronautics, China

Full Professor

01/1997 – 03/1998

 School of Automation, Nanjing University of Aeronautics and Astronautics, China

Associate Professor

09/1996 – 11/1996

 Strathclyde University, UK

Academic Researcher

02/1995 – 12/1996

 Technical University of Braunschweig, Germany

Humboldt Research Fellow

12/1990 – 01/1995

 School of Automation, Nanjing University of Aeronautics and Astronautics, China

Assistant/Associate Professor

 

Educational background

Time

University

Degree

04/1987–12/1990

School of Automation, Nanjing University of Aeronautics and Astronautics, China

Ph.D.

07/1984–03/1987

School of Automation, Nanjing University of Aeronautics and Astronautics, China

MSc

09/1980–07/1984

School of Automation, Nanjing University of Aeronautics and Astronautics, China

BSc

 

Research Interests

  1. Guidance, Navigation, and Control (GNC) of Flying Vehicle
  2. Space Science and Deep Space Application
  3. Atmospheric Re-entry Dynamics and Control
  4. Spacecraft Rendezvous and Docking, Formation Flying
  5. Intelligent Spacecraft Control and Management Technologies
  6. Space System Engineering and Optimization

 

Research projects

  1. Spacecraft unltra-Accurate Measurement and Control Technologies, 03/2020–03/2022
  2. Nano-Satellite systems for multi-source short data acquisition system,06/2019–06/2021
  3. Autonomous mission planning and spacecraft intelligent control for LEO Satellite Constellation, 2020-2022
  4. APSCO Small Student Satellite, SSS-2A, 05/2017–05/2020
  5. STU-2 CubeSatellite Mission,  10/2013–03/2016

 

Selected publications

Books

  1. Automated Rendezvous and Docking of Spacecraft, Chinese Version, as a Translator and Reviewer

Papers Published in Journals and Periodicals

  1. A Multiple CubeSat Constellation for Integrated Earth Observation and Marine/Air Traffic Monitoring, Wu S. Chen W. Cao C., Zhang C. & Mu Z. https://doi.org/10.1016/j.asr.2020.04.025
  2. Finite-Time Attitude Stabilization Adaptive Control for Spacecraft with Actuator Dynamics Wang C-B, Ye D, Mu Z-C, Sun Z-W and Wu S-F, Sensors 2019, 19(24), 5568, Dec 2019
  3. A GA-SA Hybrid Planning Algorithm Combined with Improved Clustering for LEO Observation Satellite Missions,Long X-Y, Wu S-F, Wu X-F, Huang Y-X, & Mu Z-C. Algorithms 2019, 12, 231; doi:10.3390/a12110231, Nov 2019
  4. Topological Analysis of Space Network Using Burnside Theory, Wang X‑L, Wu S‑F, Gong D‑R, Wu Y‑D, Advances in Astronautics Science and Technology, https://doi.org/ 10.1007/s42423-019-00038-w, Aug 2019
  5. Discrete Legendre Polynomials-based Inequality for Stability of Time-Varying Delayed Systems,Gong D-R, Wang X-L, Wu S-F, Zhu X-D, J of Franklin Institute 356(2019) 9907-9927, Sept 2019
  6. 纳卫星电磁对接控制机构技术研究,慕忠成,叶东,吴树范,《北京航空航天学报》,Vol.44, No. 12, 2018年12月,pp2644-2650
  7. Aircraft Monitoring by the Fusion of Satellite and Ground ADS-B Data, Zhang X, Zhang J-J, Wu S-F, Cheng Q, Zhu R., ACTA ASTRONAUTICA, Vol 143, pp398-425, Jan. 2018
  8. Design and implementation of a Cube satellite mission for Antarctic Glacier and Sea Ice Observation, Wu S-F., Zhao T-C., Gao Y., & Cheng X. , ACTA ASTRONAUTICA, Vol 139, pp313-320, July 20, July 2017 (SCI收录)
  9. 基于开放式SDR架构的立方星通信系统研究及其在突发事件的应用分析,慕忠诚,吴树范,张翔,廖文和,《空间对地观测工程与技术-小卫星专刊》, 总第02期, 2014年12月, pp50-54
  10. Attitude and Orbit Control Systems for Lisa Pathfinder Spacecraft, Giulicchi L., Wu S-F., & Fenal, T. Aerospace Science and Technology, Vol.24, No.24, pp283-294 2013
  11. Spacecraft Drag-Free Attitude Control System Design with Quantitative Feedback Theory,  Wu S.-F. and Fertin D.  ACTA ASTRONAUTICA, Vol 62, pp668-682, May 2008
  12. A Comprehensive Fuzzy-Rule-Based Self-Adaptive Genetic Algorithm, Hu X.-B., Paolo E.Z. & Wu S.-F.  International Journal of Intelligent Computing and Cybernetics, Vol. 1 No. 1, pp94-109, March 2008
  13. Optimization of Spacecraft Thruster Management Function, Ankersen F., Wu S.-F.,  Aleshin A., Vankov A., & Volochinov V., AIAA Journal of Guidance, Control and Dynamics, Vol.28, No. 6, pp1283-1290, Nov-Dec. 2005
  14. On-Line Free-Flight Path Optimization Based on Improved Genetic Algorithms , Hu X., Wu S.-F. & Jiang J.,  Engineering Application of Artificial Intelligence,  Vol.17, Issue 8, pp897-907, Dec. 2004
  15. Robust MIMO Control Systems Design with Eigenstructure Assignment and QFT, Wu S.-F., Wei W.,  & Grimble M.J. IEE Proceedings on Control Theory and Applications,  Vol. 151, No. 2,  March 2004, pp198-208
  16. In-Orbit Thruster Calibration Techniques and Experiment Results with UoSAT-12, Wu, S.-F., Styen, W.H., & Bordany, R.E., IFAC Journal of Control Engineering Practice,  Vol.12, No.1, pp87-98, Jan. 2004
  17. Fuzzy Logic Based Full-Envelope Autonomous Flight Control for an Atmospheric Re-Entry Spacecraft, Wu S.-F., Engelen, C. J. H., Babuska, R., Chu, Q. P., & Mulder J. A., IFAC Journal of Control Engineering Practice, Vol.11, No.1, pp11-25, Jan. 2003.
  18. Modeling and In-Orbit Calibration Practice of a Miniature 2-Axis Analogue Sun Sensor, Wu, S.-F., & Styen, W.H.,  Aerospace Science and Technology,  Vol.6, No.6, pp.423-433, Oct. 2002
  19. Fast Prediction Algorithms of Satellite Imaging Opportunities with Attitude Controls, Wu S.-F. & Palmer P.L.,  AIAA Journal of Guidance, Control and Dynamics, Vol.25, No.4, pp.796-803, July-August 2002
  20. Atmospheric Reentry Modeling and Simulation, Costa, R. R.; Silva, J.A.; Wu, S. F.; Chu, Q. P.; Mulder, J. A., AIAA Journal of Spacecraft and Rockets, Vol .39, No.4, pp636-639, July-August 2002
  21. 一种基于遗传算法的求代数方程组数值解的新方法 ,胡小兵,吴树范,江驹,《控制理论与应用》, Vol.19, No.4, 2002年8月, pp567-570
  22. Nonlinear Dynamic Modeling and Simulation of an Atmospheric Re-Entry Spacecraft, Wu S.-F., Costa, R.R., Chu Q.-P., and Mulder J. A., Aerospace Science and Technology, Vol.5, Issue 5, pp365-381, July 2001
  23. Fuzzy Logic Based Attitude Control of the Spacecraft X-38 Along a Nominal Re-entry Trajectory, Wu S.-F., Engelen, C.J.H., Chu Q.-P., Babuska, R., Mulder J. A. and Ortega G.,   IFAC Journal of Control Engineering Practice, Vol.9, No.7, pp699-707, July 2001
  24. 民航飞机飞行航线动态实时优化仿真研究,胡小兵, 吴树范,江驹,《计算机仿真》, Vol.18 No.3  2001年5月
  25. 定量反馈理论在鲁棒与容错飞行控制系统设计中的应用, 韦巍, 吴树范, 沈勇璋, 《南京航空航天大学学报》, Vol.33, No.2, 2001年4月, pp130-134
  26. 基于GA的民航飞机水平航线动态寻优算法 ,胡小兵,吴树范,江驹,《航空计算技术》, Vol.31, No.2, 2001年3月
  27. 模糊理论在遗传算法中的运用, 胡小兵,吴树范,江驹,  《模式识别与人工智能》, Vol.14 No.1, 2001年3月, pp109-113
  28. 基于模糊逻辑控制的航天器返回段姿态控制,  江驹,吴树范,龚华军, 《南京理工大学学报》, Vol.25, No.1, pp.91~95,2001年2月
  29. Path Guidance and Control of a Guided Wheeled Mobile Robot, Wu S.-F., Mei J.-S. and Niu P.-Y.,  IFAC Journal of Control Engineering Practice, Vol.9, No.1,  pp97-105, Jan. 2001
  30. TSP的一种改进遗传算法,  胡小兵,吴树范,江驹, 《计算技术与自动化》, Vol.19,  No.4, pp.34~38, 2000年11月
  31. 再入大气层航天飞机的动力学建模与控制 , 江驹,吴树范,龚华军, 《南京航空航天大学学报》, Vol.32 No.4, 2000年8月
  32. QFT based Robust/Fault-Tolerant Flight Control Design For a Remote Pilotless Vehicle, Wu S.-F., Grimble M.J. and Wei W.,  IEEE Transactions on Control Systems Technology, Vol.8, No.6, Nov. 2000, pp.1010-1016
  33. Introduction to Quantitative Feedback Theory for Lateral Robust Flight Control System Design  Wu S-F, Grimble M.J. and Breslin S.G., IFAC Journal of Control Engineering Practice, Vol.6, No.7, 1998, pp.805-827
  34. Energy State Approach to The Integrated Flight Performance Management of Commercial Aircraft, Wu S.-F. and Reicher G. Transaction of Nanjing University of Aeronautics and Astronautics, Vol.14, No.2, Dec.1997, pp.101-108
  35. 定量反馈理论与鲁棒飞行控制器设计,吴树范, 《自动化理论、技术与应用》,Vol.4, 1997年7月, 浙江大学出版社, pp.86-91
  36. 飞行计划与空中交通流量管理系统,尹理丽,吴树范,《数据采集与处理》,Vol.11, No.4, 1996
  37. Optimum Flight Trajectory Guidance Based on Total Energy Control of Aircraft, Wu S.-F., Guo S-F.  AIAA Journal of Guidance, Control and Dynamics, Vol.17, No.2, March-April 1994, pp.291-296
  38.  Studies on Aircraft Total Energy Flight Control System: Nonlinear System Integration and Simulation. Wu S.-F., Shen Y.-Z., and Guo S.-F. Chinese Journal of Aeronautics, (ISSN1000-9361), Vol.8, No.1, Feb.1995, pp.36-44
  39. 飞机总能量控制系统的研究Ⅱ - 非线性控制律综合与仿真,吴树范,沈勇璋,郭锁凤,《航空学报》 Vol.15, No.9, 1994年9月, pp1043-1050
  40. The Decoupling Design of Aircraft Lateral Flight Control Systems with Eigenstructure Assignment, Wu S.F. and Guo S.F., Transaction of Nanjing University of Aeronautics & Astronautics,  (ISSN1005-1120) Vol.10, No.1, Dec. 1993, pp. 90-94
  41. 基于四维导引的飞机纵向飞行剖面的解算与综合,吴树范,郭锁凤,《航空学报》 ,Vol.14,No.5, 1993.5,pp261-268;
  42. 飞机总能量控制系统的研究Ⅰ - 原理分析与系统设计,吴树范,蔡维黎,沈勇璋,郭锁凤,《航空学报》 Vol.14, No.7, 1993年7月, pp.355-361
  43. 终端区自动化空中交通管理技术,吴树范,《国际航空》,第360期,1993.2,pp56-69;
  44. 飞机纵向飞行轨迹的优化与实现,吴树范,沈勇璋,《控制理论与应用》,Vol.9, No.4, 1992, 380-386
  45. 飞行管理系统的发展及其主要技术问题,吴树范, 《火力与指挥控制》,Vol.14, No.4, 1989.12, pp.1-7
  46. 民用飞机飞行性能优化的研究,吴树范,郭锁凤,《民用飞机设计与研究》,1990年第3期,1-7
  47. 一种非线性状态估计器的算法实现与解耦简化,吴树范,胡寿松,郭锁凤,《南京航空航天大学学报》,Vol.22, No.1, 1990.1, pp.35-42
  48. 综合火力/飞行控制系统的飞行与设计,吴树范,郭锁凤,《火力与指挥控制》,Vol.15, No.4, 1990.12, pp.7-15
  49. 综合火力/飞行控制系统中目标状态估计器的分析与设计,吴树范,郭锁凤,《火力与指挥控制》,Vol.14, No.2, 1989.6, pp.3-12

Papers presented in International Conferences and Symposium

  1. Xiaoliang Wang, Deren Gong*, Yuedong Wu and Shufan Wu, Adaptive terminal sliding mode attitude control of hypersonic vehicle during re-entry, The 8th International Conference on Space Technology Innovation, Shanghai, China, pp.25-30, 3-6 Sep, 2019
  2. 引力波探测任务轨道设计中的同伦方法,王巍,吴树范,侯黎强,第16届深空探测学会年会,青岛,2019年8月
  3. 小行星软着陆方案设计与分析 张祎,吴树范,侯黎强, 第16届深空探测学会年会,青岛,2019年8月
  4. Liqiang Hou, Shufan Wu, Zhongcheng Mu, and Xiangyu Long, Optimization of Low-Thrust Reconfiguration of Formation Flying Using Relaxed Stochastic Terminal Conditions, International Workshop on Satellite Constellations & Formation Flying, Glasgow,UK,16-19 July 2019
  5. Xiaoliang Wang, Shufan Wu*, Deren Gong, Zhe Su, On ground test of an IMU/GNSS receiver for atmospheric re-entry vehicle application, The International Conference on Aerospace System Science and Engineering (ICASSE 2019), Toronto, Ontario, Canada, July 30-August 1, 2019
  6. Xiaoliang Wang; Deren Gong*; Nan Wang; Shufan Wu Second-order Approximation Integral Inequality for Stability of Systems with Time Delays, The 3rd International Symposium on Autonomous Systems, 29-31 May 2019, Shanghai, 978-1-7281-1298-5/19 ©2019 IEEE, pp.261-265
  7. 一种基于Burnside定理的星间网络拓扑分析方法, 王晓亮,吴树范*,龚德仁,吴岳东, 第五届小卫星技术国际交流会,April 2019 长沙
  8. Shufan Wu, Micro/Nano Satellite Technologies and Commercial Space in China, 25th Asia-Pacific Regional Space Agency Forum (APRSAF), Singapore, Nov 6-9 2018
  9. 空间引力波探测科学卫星关键技术,吴树范,2018中国深空探测学术会议,大会特邀报告,珠海,2018.11
  10. 深空探测卫星的无拖曳控制技术,吴树范,龚德仁,王楠,2018中国深空探测学术会议,珠海,2018.11
  11. 一种通用型升力式再入航天器动力学与建模仿真软件,吴树范,王晓亮,第六届八院航天科技创新发展论坛,上海,2018.08
  12. 一种IMU/GNSS超紧耦合接收机在再入飞行器上的应用研究,王晓亮,龚德仁,吴树范,苏哲,第三届中国临近空间与空天飞行器控制会议(CNACC2018),会议文集pp.629-638,2018.05,大连
  13. 某升力体型再入航天器建模与控制技术研究,吴树范,王晓亮,第三届中国临近空间与空天飞行器控制会议(CNACC2018),大连,2018年05月
  14. Zhao Li, Shufan Wu, Kristoffer Palmer, Johan Sundqvist, Ana Zaldivar Salaverri, Tor-Arne Grönland , Xiwang Xia, Baopeng Kang, Yanping Bai, In-Orbit Demonstration of an MEMS-based Cold-Gas Micropropulsion Module, presented at the 3rd COSPAR Symposium (COSPAR Symposium 2017), Jeju, Jeju, Korea, September 18~22 2017.
  15. Wu S-F., CubeSats: Satellites from Student, presented at the 12th UK-China Workshop on Space Science and Technology, Edinburgh, UK, 5-8th Sept 2017
  16. Antarctic Glacier and Sea Ice Observation With a Chinese Cube Satellite, Wu S-F, Zhao T-C, Gao Y, Cheng X., IAC.16.B4.4.11, presented at the 67th International Astronautical Congress (IAC), Guadalajara, Mexico, 26-30, Sept. 2016
  17. Aircraft Monitoring by the Fusion of Satellite and Ground ADS-B Data, Zhang X, Zhang J-J, Wu S-F, Cheng Q, Zhu R., IAC.16.B5.2.9, presented at the 67th International Astronautical Congress (IAE Conference MODELLING, SIMULATION & CONTROL, AMSE MSC'92, Hefei, China, Oct.6-8, 199C), Guadalajara, Mexico, 26-30, Sept. 2016
  18. An efficient design and integration technology for CubeSat payload, Zhang X, Wu S-F, Chen W, Feng H., IAC.16.D1.7.7, presented at the 67th International Astronautical Congress (IAC), Guadalajara, Mexico, 26-30, Sept. 2016
  19. Design And Implementation of Electrical System For STU-2 Cubesats, Chen K, Wu S-F, IAC.16.C3.4.2, presented at the 67th International Astronautical Congress (IAC), Guadalajara, Mexico, 26-30, Sept. 2016
  20. LS-1: a new small launcher dedicated to Micro/Nano Satellite missions, Wu S-F, Liu X L, Zhang L, Zhang C W, IAC.16.D2.7.8, presented at the 67th International Astronautical Congress (IAC), Guadalajara, Mexico, 26-30, Sept. 2016
  21. The Space Greeting Card Mission, Chen L, Bai Y-P, Wu S-F, IAC.16.E1.7.11, presented at the 67th International Astronautical Congress (IAC), Guadalajara, Mexico, 26-30, Sept. 2016
  22. Magnetic-based Attitude Control Scheme for CubeSat, Xia X-W, Wu S-F, Sun G-W, Wang T, Wu Z-Y, Bai Y-P, Chen W, Mu Z-C, Proceedings of 2016 IEEE Chinese Guidance, Navigation and Control Conference – IEEE CGNCC 2016, 12-14 Aug 2016, Nanjing, China
  23. The STU-2 CubeSat Mission and In-Orbit Test Results, Wu S-F, Chen W., Cao C-X, SSC16-III-09, presented at the 30th AIAA/USU Conference on Small Satellite, Utah, USA, 8-11, Aug. 2016
  24. Attitude Determination and Control System Design for STU-2A CubeSat and In-Orbit Results, Liu G-W, Xia X-W, Wu Z-Y, Wu S-F, et al, presented at the 13th Annual CubeSat Developers’ Pre-Conference Workshop of the 30th AIAA/USU Conference on Small Satellite. Aug 6-7, 2016, Utah, USA
  25. In-Orbit Demonstration of an MEMS-based Micropropulsion system for CubeSats, Palmer K, Groenland T-A, Li, Z, Wu S-F, presented at the 13th Annual CubeSat Developers’ Pre-Conference Workshop of the 30th AIAA/USU Conference on Small Satellite. Aug 6-7, 2016, Utah, USA
  26. Nano Propulsion-based Orbit Maneuver Scheme for CubeSat, Xia X, Li Z, Wang T, Bai Y, Wu S-F., presented at  35th Chinese Control Conference (CCC2016), July 27-29 2016, Chengdu, China
  27. Discovering the sky at the Longest Wavelengths (DSL), Boonstra AJ, Garrett M, …, Wu S-F, …, et al, presented at the 2016 IEEE Aerospace Conference, Mar 6-11, 2016, Big Sky, Montana, USA
  28. STU-2: A CubeSat Mission for Earth Observation and Marine/Air Traffic Monitoring, Wu S-F. Chen W. Cao C., et al, presented at  6th CSA-IAA 6th International Conference on Space Technology Innovation, Nov. 2015, Shanghai, China
  29. CubeSats: Tiny Satellite – A Big World, Wu S-F., presented at China Satellite Conference 2015, Oct. 2015, Beijing, China
  30. Earth Observation and Marine/Air Traffic Monitoring with a Multiple CubeSat Constellation, Wu S-F. Chen W. Cao C., et al, IAC.15.B4.4.3, presented at  66th International Astronautical Congress, Oct. 2015, Jerusalem, Israel
  31. TW-1: a CubeSat constellation for space networking experiments, Wu S-F, Mu Z-C., Chen W., Rodrigues P., Mendez R., Alminde L., 6th European CubeSat Symposium, Oct 14-16th 2014, Estavayer-le-Lac, Switzerland
  32. SULFRO: a Swarm of Nano-Satellite at SE L2 for Space Ultra-Low Frequency Radio Observatory, Wu S-F, Chen W., Zhang Y-H, Baan W.A., An T., SSC14-III-9, 28th Annual AIAA/USU Conference on Small Satellites, August 4-7th 2014, Utah, USA
  33. Micro/Nano Satellite Technologies and Applications in China, Wu S-F. and Chen H., IAC.13.B4.1.5, presented at  64th International Astronautical Congress, Sept. 2013, Beijing, China
  34. Lisa Pathfinder Science Module De-spin and Sun Acquisition using micro-Newton thrusters with multiple unknown failures, Watt M., Thomas F., Wu S.-F., Strandmoe S.,  the 8th International ESA Conference on Guidance Navigation and Control Systems, Carlsbad, Czech Republic, 5-10 June 2011
  35. Attitude Control of Lisa Pathfinder Spacecraft with Micro-Newton FEEP Thrusters under Multiple Failures, Wu, S-F., Giulicchi, L. Fenal T., & Watt, M.  AIAA-2010-8199, presented at  AIAA Guidance, Navigation, and Control Conference,  Aug. 2010, Toronto, Ontario, Canada
  36. Attitude Stabilization of Lisa Pathfinder Spacecraft Using Colloidal Micro-Newton Thrusters, Wu, S-F., Giulicchi, L. Fenal T., & Watt, M. AIAA-2010-8198, presented at  AIAA Guidance, Navigation, and Control Conference,  Aug. 2010, Toronto, Ontario, Canada
  37. Lisa Pathfinder Attitude and Orbit Control Systems, Giulicchi L., and Wu S-F., IAC.09.C1.11.10, presented at  60th International Astronautical Congress, Oct. 2009, Daejeon, Republic of Korea
  38. Lisa Pathfinder Mission: Attitude and Orbit Control Based on Micropropulsion Systems,  Giulicchi L., Fenal T., and Wu S-F., AIAA-2009-5997, presented at  AIAA Guidance, Navigation, and Control Conference,  Aug. 2009, Chicago, Illinois, USA
  39.  A Self-Adaptive Generic Algorithm Based on Fuzzy Mechanism, Hu  X-B and Wu S-F., presented at IEEE Congress on Evolutionary Computation, Singapore, 25 - 28 Sept 2007
  40.  Closed Loop Performance and Limitations of the LISA Pathfinder Drag-Free Control System, Fichter W., Schleicher A., Bennani S. and Wu S., AIAA-2007-6732, presented on AIAA Guidance, Navigation, and Control Conference,  Aug. 2007, Hilton Head, South Carolina, USA
  41.  SpaceLab - A Spacecraft Simulation Library with Special Features for Parameter Initialization, Wu S-F. and Ankersen F., presented at 9th International Workshop on Simulation for European Space Programmes, Noordwijk, The Netherlands, 6 - 8 Nov 2006
  42.  Wide Field Imager Technology Reference Study, Lyngvi A., Gondoin P., Kirschner V., Wu S-F., et al, IAC-06-A3.1.05, presented at 57th International Astronautical Congress, Valencia, Spain, 2 - 6 Oct. 2006
  43. QFT Based Drag-Free and Attitude Controller Design and Tuning, Wu S-F. and Fertin D. , presented at 6th International ESA Conference on Guidance Navigation and Control Systems, Loutraki, Greece, 17 - 20 Oct 2005,
  44. On Optimization of Spacecraft Thruster Management Function , Ankersen F., Wu S.-F.,  Aleshin A., Vankov A., & Volochinov V., AIAA2004-5133, presented at AIAA Guidance, Navigation, and Control Conference,  Aug. 2004, Rhode Island, USA
  45. In-Orbit Calibration of the Cold-Gas Thrusters Onboard UoSAT-12 , Wu S.-F., Steyn, W.H., Palmer, P.L., & L. Giulicchi,  Proceedings of the 5th International ESA Conference on Guidance Navigation and Control Systems, Frascati (Rome), Italy, 22-25 October 2002, pp.473-480
  46. Robust Flight Control Design with combined QFT and Eigenstructure Assignment Methods, Wu S.-F., Wei, W. & Grimble, M.J.,  presented at 15th IFAC World Congress on Automatic Control,  Barcelona, Spain, July 21-26, 2002
  47. Fast Prediction Algorithms of Satellite Imaging Opportunities with Canted Camera and Attitude Control, Wu S.-F. & Palmer P.L., AIAA2001-4270, presented at the AIAA Guidance, Navigation, and Control Conference, 6-9, Aug. 2001, Quebec, Canada
  48. GA Based On-Line Real-Time Optimization of Commercial Aircraft’s Flight Path for a Free Flight Strategy , Hu, X.-B., Wu S.-F. & Jiang, J., AIAA2001-4234, presented at AIAA Guidance, Navigation, and Control Conference, 6-9, Aug. 2001, Montreal, Quebec, Canada
  49. In-Orbit Modeling and Calibration of the Sun Sensors on UoSAT-12 and Tsinghua-1 Satellites, Wu S.-F. & Steyn W.H., presented at the 15th AIAA/USU Conference on Small Satellite, (SSC01-V-3), Utah, USA, 13-16, Aug., 2001
  50. ImPredict: a Fast Image Prediction Software and Its Application in the SSTL off-axis Image Scheduling System, Wu S.-F., Brewer, A., & Palmer P.L., presented at the 15th AIAA/USU Conference on Small Satellite, (SSC01-VIIIa-1), Utah, USA, 13-16, Aug., 2001
  51. In-Orbit Estimation of the Inertia Matrix and Thruster Parameters of the UoSAT-12 Minisatellite , Bordany, R.E., Steyn, W.H., & Wu, S.-F., presented at the 14th Annual AIAA/USU Conference on Small Satellite, (SSC00-I-4), Utah, USA, 21-24, Aug., 2000
  52. Atmospheric Re-Entry Modeling and Simulation: Application to a Lifting Body Re-Entry Vehicle, Costa R.R., Silva J.A., Wu S.-F., Chu Q.-P., & Mulder J.A., AIAA2000-4086, presented at the AIAA Modeling and Simulation Technologies Conference and Exhibit, Denver, CO, USA, 14-17 Aug. 2000
  53. Intelligent Flight Controller Design with Fuzzy Logic for an Atmospheric Re-entry Vehicle, Wu S.-F., Engelen C.J.H., Babuska R., Chu Q.-P., & Mulder J.A., AIAA2000-0174, presented at the 38th AIAA Aerospace Sciences, Reno, Nevada, USA, 10-13 Jan. 2000
  54. Nonlinear Dynamic Modeling and Simulation of the Re-Entry Crew Return Vehicle, Wu S.-F., Costa R.R., Chu Q.-P. , Mulder J. A. and Ortega G.,  presented in the 4th ESA International Conference on Spacecraft Guidance, Navigation and Control Systems, ESTEC, Noordwijk, The Netherlands,18-21 Oct., 1999, pp.289-300
  55. Fuzzy Logic Based Flight Control of the Atmospheric Re-entry Crew Return Vehicle, Wu S.-F., Engelen, C.J.H., Babuska, R., Chu Q.-P., Mulder J. A. and Ortega G., proceedings of the 4th ESA International Conference on Spacecraft Guidance, Navigation and Control Systems, ESTEC, Noordwijk, The Netherlands,18-21 Oct., 1999, pp.309-318
  56. QFT based Robust/Fault Tolerant Flight Control Design For a Remote Pilotless Vehicle, Wu S.-F., Grimble M.J. and Wei W., Proceedings of the IEEE International Conference on Control Applications , Hawaii, 22-26 August, 1999, pp57-62
  57. Robust/Fault Tolerant Flight Control System Design with Quantitative Feedback Theory, Wu S., Wan S., and Wei W., Proceedings of the Third Asia-Pacific Conference on Control & Measurement, Dunhuang, China, Aug.31-Sept.4, 1998, pp82-86
  58. Quantitative Feedback Theory for Lateral Robust Flight Control Systems Design, Wu S-F., Grimble M.J. and Breslin S.G., Symposium on Quantitative Feedback Theory and Other Frequency Domain Methods and Applications, Glasgow, UK, Aug. 21-22, 1997, pp.235-246
  59. Design and Analysis of a Lateral Flight Control and Path Guidance System for Commercial Aircraft,  Wu S.-F. and Reichert G. DGLR-JT96-094, JAHRBUCH 1996, Vol. 1, Dresden, Germany,  Sept. 1996, pp493-502
  60. Optimized Sequencing and Scheduling Algorithms for Arrival Air Traffic Based on FCFS Principle,  Wu, S.-F., et al. Proceedings of the IFAC 7th Symposium on Transportation Systems: Theory and Application of Advanced Technology, Tianjin, PRC, Aug.24-26, 1994, Vol.2, pp.234-237;
  61. Development of a Computer Assisting System for Flight Planning and Air Traffic Flow Management. Wu, S.-F., et al. Proc. of the IFAC 7th Symposium on Transportation Systems: Theory and Application of Advanced Technology, Tianjin, PRC, Aug.24-26, 1994, Vol.2, pp.261-264;
  62. Integrated Flight Control and Management Techniques Based on Total Energy Principles.  Wu S. and Guo S., Proceedings of the First Asian Control Conference, July 27-30, 1994, Tokyo, Japan, Vol.1 of 3, pp.319-322
  63. Studies on the Flight Performance Optimization of Commercial Aircraft, Wu S. and Shen Y., Proceedings of 8th IEEE TENCON on Computer, Communication, Control and Power Engineering,  Beijing, PRC, Oct.19-21, 1993, Vol.4 of 5, pp139-145.
  64. The Decoupling Design of Aircraft Lateral Flight Control Systems with Eigenstructure Assignment, Wu S.F. and Guo S.F., Proceedings of the First Asia-Pacific Conference on Control & Measurement, Kunming, China, Aug. 1993, pp. 90-94
  65. Analysis and Development of a Total Energy Control System for a Large Transport Aircraft.  Guo S., Wu S., and Shen Y., Proceedings of the 18th ICAS (International Council of the Aeronautical Sciences) Congress, Sept.20-25, 1992, Beijing, China. Vol.2, pp. 1787-1796
  66. Synthesis and Guidance of a 4D Cruise and Descent Profile for Commercial Aircraft. Wu S. and Guo S., Proceedings of Intern. AMSE Conference on MODELLING, SIMULATION & CONTROL, AMSE MSC'92, Hefei, China, Oct.6-8, 1992, USTC Press, Vol.5, pp.3290-3303
  67. Integration of Flight Management Systems Based on Total Energy Principles.  Wu S. and Guo S., Proceedings of Intern. AMSE Conference MODELLING, SIMULATION & CONTROL, AMSE MSC'92, Hefei, China, Oct.6-8, 1992, USTC Press, Vol.5, pp.3325-3334

 

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