SpaceMaster - A Two Year Joint European Master in Space Science and Technology Shinichi Nakasuka, University of Tokyo

Transcription

1 SpaceMaster - A Two Year Joint European Master in Space Science and Technology Shinichi Nakasuka, University of Tokyo Lurea Tekniska Universitet, Kiruna

2 About Our Laboratory University of Tokyo: 29,000 students, 7300 staffs School of Engineering: 22 departments Department of Aeronautics and Astronautics: 12 labs Intelligent Space Systems Laboratory (ISSL): 20 members Major Research Themes Nano/Pico Satellite R&D and Launch/Operation Spacecraft Navigation, Guidance & Control Autonomy and Intelligence for Space Systems Novel Space Systems x gyro y gyro z gyro x wheel y wheel z wheel Fault Diagnosis Robot Solar Power Satellite

3 Erasmus Mundus Master Course SpaceMaster Joint European Master in Space Science and Technology Combine the great diversity of space expertise at six European universities to a common platform of competence Four Semester (Two Year) Program 1st Semester: Lectures and Hands-on Training at Julius-Maximilians Universität Würzburg, Germany 2nd Semester: Lectures and Hands-on Training at Luleå University of Technology, Sweden 3rd Semester: Engineering/Science Specialization at 6 different European Universities 4th Semester: Research Works at 6 European and foreign partner universities towards thesis and final defence Participating Students - about 15 European students - about 30 non-european students

4 Universities which provide educations European Core Universities Luleå University of Technology, Department of Space Science, Sweden Cranfield University, UK Czech Technical University, Prague, Czech Republic Helsinki University of Technology, Finland Julius-Maximilians Universität Würzburg, Germany Université Paul Sabatier Toulouse, France Partnership Universities Shanghai Jiao Tong University, Department of Aeronautic and Astronautic Engineering Stanford Univeristy, Department of Aeronautics and Astronautics Engineering University of Tokyo, Department of Aeronautics and Astronautics University of Toronto, Institute of Aerosppace Studies Utah State University, Mechanical and Aerospace Engineering

5 Erasmus Mundus Master Course SpaceMaster 120 ECTS Joint European Master in Space Science and Technology Compulsory courses 60 ECTS I Semester 30 ECTS - Julius-Maximilians Universität, Würzburg II Semester 30 ECTS - Department of Space Science, Kiruna Specialisation 30 ECTS + Master Thesis min 30 ECTS Cranfield University: Dynamics and Control and Systems and Structures Czech Technical University, Prague: Space Automation and Control Helsinki University of Technology: Space Robotics Julius-Maximilians Universität Würzburg: Communication of Space Robotics Université Paul Sabatier Toulouse: Space Technique and Instrumentation (engineering track), Astrophysics, Space Science,Planetology (science track) Department of Space Science, Kiruna: Space Science and Technology (engineering track), Atmospheric and Space Physics (science track) Automation, Control and

6 Joint European Master in Space Science and Technology - Erasmus Mundus, 120 ECTS Scholarships and Fees Non - EU students / 2 years from EC (20 study months x x a fixed amount of ) General category: 15 positions Specific category (for 2007): 6 students from India 1 students from China 2 students from ACP countries 1 student from Western Balkan Fee: / year EU students Erasmus Mobility 150 / month for 3-12 months ESA scholarships: 6 positions / year for the thesis work EC scholarships for studies outside EU at the partnership universities: 10 positions / year / 3 months for the thesis work 4 positions /year 800 / 1 month the for studies No fees

7 Joint European Master in Space Science and Technology - Erasmus Mundus, 120 ECTS ESA Scholarships and Stages 6 positions / stages / 3-4 months at ESTEC 20 /day incl. weekends Thesis on a topic relevant to the Human Exploration Promotion Programme within the Directorate of Human Spaceflight, Microgravity and Exploration: Space Habitation System Design (dealing with all aspects of human presence in space) Inflatable Structures for Space Applications Life Support EVA Systems for Planetary Applications Human Research for Exploration Students from ESA Member States (Austria, Belgium, Denmark, Finland, France, Germany, Greece, Ireland, Italy, Luxemburg, The Netherlands, Norway, Portugal, Spain, Sweden, Switzerland, UK)

8 Space Master Students 2005/ students from 25 countries 32 non-eu students 15 EU students 2006/ students from 32 countries: 28 non-eu students 13 EU students Mexico, China, Thailand, India, Pakistan, Greece, Italy, Austria, Spain, Germany, Poland, Finland, Sweden, Czech Rebublic, Bulgaria Mexico, Canada, Brazil, Agrentina, New Zeeland, China, Japan, Thailand, Malaysia, Vietnam, India, Pakistan, Italy, Austria, Germany, France, Spain, Finland, Sweden, Romania, Russia, Slovak Republic

9 Special Features of Education of Space Space = Integration of various fields of engineering and science Difficult to provide education covering all of these fields by one university/country Lack of expertise/experience of space education in many countries Importance of Hands-on Training Require facilities/materials to provide sufficient education Require high level of experiences and know-how Importance of International Relationships Students-level collaborations can be basis for future international collaborations in actual space projects

10 Joint European Master in Space Science and Technology - Erasmus Mundus, 120 ECTS I Semester, 30 ECTS Department of Computer Science, Julius-Maximilians Universität, Würzburg 3 September February 2008 Introduction weeks: Complementary course in German Mathematics (repetition) Cultural programme Introduction in Space Physics 8 ECTS Spacecraft System Design 8 ECTS Space Dynamics 8 ECTS The Object-Oriented Approach and Java Programming 4 ECTS Internet Technologies 4 ECTS

11 Joint European Master in Space Science and Technology - Erasmus Mundus, 120 ECTS II Semester, 30 ECTS Department of Space Science, Kiruna, Sweden February - June 2008 Spacecraft Environment Interaction 7.5 ECTS Electronics in Space 7.5 ECTS Image Processing and Remote Sensing 7.5 ECTS Optical and Radar-based Observations 7.5 ECTS Complementary course in Swedish Study visits: Swedish Institute of Space Physics Swedish Space Corporation / Esrange (European Space Launching Range) EISCAT (European Incoherent Scatter Scientific Association) LKAB (Kiruna iron ore mine) Cultural programme: lectures about Kiruna history, Sami culture, Swedish social codes, visit to the Jukkasjärvi Ice Hotel

12 Joint European Master in Space Science and Technology - Erasmus Mundus, 120 ECTS III Semester, Engineering Track Space Technology and Instrumentation, 30 ECTS Department of Space Science, Kiruna, Sweden September 2008 January 2009 Space Vehicle Systems 7.5 ECTS Principles for Space Instruments 7.5 ECTS Environmental Observations from Space 7.5 ECTS Student Project (EXUS) 15 ECTS

13 Joint European Master in Space Science and Technology - Erasmus Mundus, 120 ECTS III - IV Semesters, Engineering Track Dynamics and Control of Systems and Structures, ECTS Department of Aerospace Engineering, Cranfield University, UK September 2008 June 2009 Compulsory: Space Propulsion 5 ECTS Optional : Fiber Reinforced Plastics 5 ECTS Classical Control Methods 5 ECTS Multivariable Control for Aerospace Application 5 ECTS GPS and INS 5 ECTS Thesis 45 ECTS

14 Joint European Master in Space Science and Technology - Erasmus Mundus, 120 ECTS III - IV Semesters, Engineering Track Space Robotics, ECTS Department of Automation and Systems Technology Helsinki University of Technology, Finland September 2008 June 2009 Introduction to Robot Kinematics 4 ECTS Behaviour-based Robotics 3 ECTS Field and Service Robotics 2 ECTS SpaceMaster Project in Automation Technology 4 ECTS Seminar in Automation Technology 3 ECTS Estimation and Sensor Fusion Methods 3 ECTS Machine Perception 3 ECTS Embedded Systems in Space Technology 4 ECTS Finnish 1A 2 ECTS, Finnish 1B 2 ECTS Computer Services 2 ECTS Thesis 30 ECTS

15 Joint European Master in Space Science and Technology - Erasmus Mundus, 120 ECTS III - IV Semesters, Engineering Track Automation, Control and Communication of Space Robotics ECTS Department of Computer Science Julius-Maximilians Universität, Würzburg October 2008 October 2009 Seminar: Pico-Satellites 5 ECTS Robotics 8 ECTS Team Design Project 9 ECTS Advanced Automation and Control 8 ECTS Thesis 30 ECTS

16 Joint European Master in Space Science and Technology - Erasmus Mundus, 120 ECTS III - IV Semesters, Engineering Track Space Automation and Control, ECTS Faculty of Electrical Engineering, Technical University, Prague September 2008 June 2009 Space Systems, Modelling and Identification 7 ECTS Optimal and Robust Control Design 7 ECTS Estimation, Filtering and Fault Detection 7 ECTS Distributed Real-time Systems for Space Applications 7 ECTS Hardware Support in Space Engineering 7 ECTS Team Design Project 10 ECTS State Examination Thesis 30 ECTS

17 Joint European Master in Space Science and Technology - Erasmus Mundus, 120 ECTS III - IV Semesters Observatoire Midi-Pyrénées, Université Paul Sabatier Toulouse September 2008 June/ August 2009 Astrophysics, Space Science, Planetology, Science Track ECTS Compulsory: General Physics and Astrophysics 17 ECTS Optional: Astrophysics 13 ECTS Space Science 13 ECTS Planetology 13 ECTS Thesis 30 ECTS Space Technique and Instrumentation, Engineering Track, ECTS Technology and Systems 7 ECTS Technology for Missions 11 ECTS Practical lectures 12 ECTS Thesis 30 ECTS

18 Joint European Master in Space Science and Technology - Erasmus Mundus, 120 ECTS III - IV Semesters, Science Track Atmospheric and Space Physics, ECTS Department of Space Science, Kiruna, Sweden September 2008 June / September 2009 Atmospheric Physics 7.5 ECTS Space Plasma Physics 7.5 ECTS Solar Physics 7.5 ECTS Numerical Methods 7.5 ECTS Solar System Physics 7.5 ECTS Thesis 30 ECTS

19 Joint European Master in Space Science and Technology - Erasmus Mundus, 120 ECTS Eligibility Requirements Admission is a subject to normal admission criteria for the European students. All students must have a good quality Bachelor degree in engineering, natural science, mathematics or equivalent qualifications (like Diploma Engineering studies in the 3rd or 4th year). Students from non-english speaking countries are required to have passed English proficiency test with specified results: Cambridge CPE/CAE: Pass IELTS: min 5.0 in each test, 6.0 overall score TOEFL*: 550, TOEFL (computer based): 213 TOEIC: 750 The only exceptions from providing an English test are applicants who have taken their Bachelor degree in a country with English as the official language.

20

21 CanSat Suborbital experiment University of Tokyo s Nano-Satellite Development Activities Shinichi Nakasuka, ISSL Two CubeSats on-orbit now

22 About Our Laboratory University of Tokyo: 29,000 students, 7300 staffs School of Engineering: 22 departments Department of Aeronautics and Astronautics: 12 labs Intelligent Space Systems Laboratory (ISSL): 20 members Major Research Themes Nano/Pico Satellite R&D and Launch/Operation Spacecraft Navigation, Guidance & Control Autonomy and Intelligence for Space Systems Novel Space Systems x gyro y gyro z gyro x wheel y wheel z wheel Fault Diagnosis Robot Solar Power Satellite

23 Objectives of University of Tokyo s Nano/PicoSat Projects Target Size: Nano(<15kg), Pico(<1kg) cf. Less than MicroSat (50kg) which is too big for laboratory space and test facility Providing excellent material for space engineering education Opening new ways of space development with its low cost and short development time On-orbit research bench for space science and engineering such as microgravity experiments May lead to new space business

24 University of Tokyo s Nano-Satellite Projects CanSat Suborbital Launch Experiment 99 - now 30 m Ground Resolution Space Science CubeSat XI-IV 03/6 PRISM(Remote sensing) 08 4 km Ground Resolution CubeSat XI-V 05/10 (Sister-Sat with XI-IV launched on SSETIEXPRESS) NANO-JASMINE Multi-purpose (Astrometry Satellite PETSAT(Panel Satellite) Development Launch

25 CanSats Training Step

26 ARLISS Suborbital Launch Experiment Japan-US Joint experiment has been coordinated annually Rockets are provided by amateur rocket group CanSats are released at 4km altitude on Nevada desert ARLISS 1999 Sept. 11 Univ.of Tokyo, Titech, Arizona State, etc. ARLISS 2000: July (Japan:4, USA:3) ARLISS 2001: August (Japan:5, USA:2) 1st Come-back competition ARLISS 2002: August 2-3 (Japan:6, USA:3) ARLISS 2003: Sept (Japan:6, USA:3) ARLISS 2004: Sept (Japan:6, USA:3) ARLISS 2005: Sept (Japan:7, USA:3) ARLISS 2006: Sept (Japan:8 USA:3 Europe:1) ARLISS 2007: Sept (Japan:9 USA:2 Korea:1)

27 University of Tokyo s CubeSat Project XI XI-IV (Launched in by ROCKOT) XI-V (Launched in by COSMOS)

28 XI-IV Multiple Satellite Launch Launch (Launch Site) Launch Site: Plesetsk 800 km north of Moscow Date: June 30, 2003 Site: Plesetsk Orbit: 830km SSO Launch Vehicle Provider Eurockot other satellites Separation System Developer CalPoly CubeSat Developer Standford Univ. U of Toronto Aalborg CubeSat & Separation System Developer U of Tokyo Tokyo Inst. Tech.

29 2003/06/30 18:15:26 (Plesetsk time) CubeSat XI-IV Launched to Space!

30 More than 200 beautiful Earth Photos Taken by XI-IV ( )

31 Our 2nd Satellite: XI-V On-orbit demonstration and long-time monitoring of new type solar cells (CIGS) :52 Improved Camera Capability Launched by Consecutive capture to estimate COSMOS motion from Plesetsk, Russia

32 PRISM Project Low-cost remote sensing nano-satellite Mass : 8 kg Size : 180 x 180 x 250 mm year Satellite Resolution Weight 2002 AISat 32 m 90 kg 2005 TopSat PRISM 30 8 Pico-satellite for Remote-sensing and Innovative Space Missions

33 Anticipated Quality of Images Swath Width 5km Extensible Boom Google Earth (30m ground resolution) Under patent process

34 Nano-JASMINE Infrared astrometry satellite developed by ISSL and National Astronomical Observatory of Japan as a precursor of next JASMINE Project Size about 40[cm] cubic Mass 14[kg] Attitude Control Three axis stabilization Communication S-band/100[kbps] Mission Life Two [years] Orbit Sun-synchronous Orbit

35 PETSAT(Panel ExTension SATellite) (Under development by government fund) Mission panel 1 extension Before Separation Launch Locked Attitude Control panel 3 Communication panel 1 Attitude Control panel 2 CPU panel Battery panel Communication panel 2 Attitude Control panel 1 Mission panel 2 Plug-in of Panels having different functions deal with variety of mission requirements just like a Lego Block Mass production of panels lead to low cost/high reliability Plug-in makes system level test simple and less time consuming Open architecture to allow participation of new companies with special tech. Extending panels makes it possible to use small satellite as large sat

36 Intelligent Space Systems Laboratory (Nakasuka Laboratory) Department of Aeronautics and Astronautics University of Tokyo UNISEC (University Space Engineering Consortium)

37 UNISEC (UNIversity Space Engineering Consortium) Founded in 2002, became NPO in laboratories from 36 universities: >400 students About 100 individual and company members Mission Education and human resource training for space development/utilization Technology development for nano-satellites and hybrid rockets Outreach to general public and younger generation by students

38 Satellites development in UNISEC １ Tokyo Institute of Technology: Space Science Satellite Cute-1.7 and APD and Its Separation System Launched by M-V Cute APD (10*10*20cm3) Nano-Satellite Separation System

39 Satellites development in UNISEC 2 Kagawa Univ. STARS-1 Nihon University CubeSat SEEDS Back-up model to be launched by PSLV, UNISEC Satellites will be lanched by H-IIA in 2008 < Under Development > Tohoku Univ SPRIGHT Tokyo College CubeSat Soka Univ CubeSat Hokkaido Univ/HIT HITSAT Kyushu Univ. QSAT Launched in by M-V H.I.T. Hyper spectral 12cm-cubic, 2.7kg camera satellite

40 Development of Hybrid Rockets Tokai Univ. TSRP Hokkaido Univ CAMUI Rocket Tokyo Metropolitan Univ. Osaka Pref. Univ. Tsukuba Univ. Joint Launch experiments twice a year Currently 2000m height To be 10ｋｍ 100km

41 Come-Back Competition 2002 Participating Universities 2002 Univ. of Tokyo Tohoku Univ. Kyushu Univ. Nihon Univ. Tokyo Institute Stanford Univ. of Technology ROVER

42 XI Outlook Solar Cells Antenna Latch Antenna Camera Hole Flight-Pin Mount Interface Connector photo: XI-IV (Flight Model)

43 Inside Structure Comm. System Power System C&DH System Camera Lens Mother Board I/F Connector OBC Flight-Pin XI-III (EM model)

44

45 Structure Power-system PWR5V OBC OBC-system C-DCDC TX-system CW ROM RX TNC TX TNC TX Analog SW E-DCDC TLM TLM OBC CWRX-system TX-DCDC OBC CMD TLM Charge Circuit RX TNC RX ACK CW GEN CW PWR5V Solar Cell Digital Sensors Antenna Latch Important Analog Sensors Analog Sensors Battery

46 Launch Campaign L-26 L-25 Custom Process at Narita Airport Hand-carried to Moscow Custom process at Moscow L-19 Train Ride to Plesetsk (18 hours) L-18 Final function test of CubeSat (Clean room at Plesetsk) L-14 Integration to Rocket Adapter (No access possible hereafter) L-0 Launch (June 30, 2003)