United Nations/Austria/European Space Agency Symposium on Small Satellite Programmes for Sustainable Development Small Satellite Projects: Learning Opportunities for Satellite Systems Engineering Tools Danielle Wood PhD Candidate, Engineering Systems Division Advisor: Dr. Annalisa Weigel Assistant Professor, Aeronautics/Astronautics & Engineering Systems Center for Aerospace Systems, Policy and Architecture Research Massachusetts Institute of Technology Small satellite projects are an excellent entry point for developing countries to start building capability in satellite technology. Small satellite projects can provide both hands-on technical experience and methodological training for satellite systems engineering Background Space activities in developing countries Satellites Can Provide Valuable Services in Developing Countries Especially Through Applications in Remote Sensing, Communication and Navigation Most developing countries access satellite services via in-direct means African satellite projects reveals activity across the technology spectrum Categories of African Satellite Projects (79 Projects Total) # of Projects 25 22 Using satellite indirectly Using satellite directly 20 16 15 10 5 7 11 9 5 4 4 1 0 Key Message •Satellite services are access through a variety of technical models. • Most developing countries are consumers of data and users satellite ground segments Danielle Wood Page 6 More developing countries are getting directly involved with satellite technology Many African, Asian and Latin American countries are active in satellite technology N. Korea Algeria Iran Egypt Mexico China India UAE Japan S. Korea Malaysia Nigeria Brazil Argentina Danielle Wood Indonesia South Africa Page 8 Countries with new satellite programs face strategic decisions about how to establish local technical capability International Context National Context Space Program Capabilities: Facilities and Human Resources Relationship of Space Program to Domestic Government, Industry and Academia Relationship of Space Program to Foreign Governments or Companies Research Context Exploring process of technological capability building for countries with young satellite programs More on “Building Technological Capability” At the space program level… • Sometimes capability is increased by advancing in technological autonomy • The space program is gradually doing its activities more independently of foreign assistance • Move through procurement models… – Buying Training Licensing Building in foreign facility Building via partnership Building locally Danielle Wood Page 13 At the space program level… • Sometimes capability is increased by advancing in technological complexity • The complexity of a satellite can change based on factors such as… – Size – Number of instruments – Lifetime – Pointing accuracy – Temporal and spatial resolution of data – Orbit – Etc… Danielle Wood Page 14 Increasing technological complexity CubeSat Mass Capability Lifetime Danielle Wood < 3 pounds Technology demonstration and Education < 1 year Small EO Satellite Mass 200 to 600 pounds (100 to 400 kg) Capability Earth Imaging and Scientific Measurement Lifetime ~ 5 years Commercial EO Satellite Mass 4000 pounds (~2000 kg) Capability High resolution earth imaging Lifetime 7 to 10 years Image Sources: http://www.sstl.co.uk/Products/Platforms http://polysat.calpoly.edu/CP6.php http://launch.geoeye.com/LaunchSite/assets/download_imagery/testing1.jpg Page 15 South Korea’s Path shows advances in autonomy and complexity Increasing Technical Complexity Project Participants & Launch Date KITSAT-1 1992 KITSAT-2 1993 KITSAT-3 1999 UK + Korean Universities Korean University Korean University KOMPSAT-1 KOMPSAT-2 KOMPSAT-3 1999 2006 2010 US Firm + Korean Space Agency European Firm + Korean Space Agency European Firm + Korean Space Agency National Space Agency KOMPSAT-2 KOMPSAT-3 Technical University KITSAT-3 KITSAT-1 Danielle Wood KOMPSAT-1 KITSAT-2 SpinOff Firm RazakSat (2009) Korean Firm + Malaysian Space Agency Source: SaTReC http://satrec.kaist.ac.kr/english/SaTReC.html DubaiSat (2009) Korean Firm + UAE University Page 16 System Engineering Tools: Facilitate complex satellite and payload projects • System Modeling • Design Space Exploration and Trade Analysis • System Optimization Credit: This material is based partly on course materials from MIT’s 16.888 Multi-Disciplinary Design and Optimization Course, Prof de Weck and Prof. Wilcox: http://ocw.mit.edu/courses/aeronautics-and-astronautics/16-888multidisciplinary-system-design-optimization-spring-2004/ System Modeling Models – Mathematical descriptions of system of interest that can be manipulated to answer questions about the system design; based on requirements and confirmed with benchmarking System Models Physics Based Models Generic Software Context Empirical Models Discipline Specific Software Context (ie mechnical drafting, orbital simulation, electrical design, etc) (ie MATLAB, Excel, etc) Danielle Wood Page 18 System Modeling: Simulation models are composed of smaller modules Info fed to upstream (feedback) Info coming from upstream (feed-forward) Input Output Module i Output Input Info fed from downstream (feedback) Danielle Wood Credit: de Weck and Willcox Info fed to downstream (feed-forward) Page 19 N2 Diagram: Shows relationships between modules Danielle Wood Credit: M.S. Avnet, A.L.Weigel, An application of the Design Structure Matrix to Integrated Page 20 Concurrent Engineering, Acta Astronautica (2009), doi:10.1016/j.actaastro.2009.09.004 System Model Example with Modules Danielle Wood Page 21 Design Space Exploration and Trade Analysis System Attribute • Explore results of potential design decisions • Identify feasible design solutions Desired System Performance Danielle Wood • Establish upper and lower limits on performances Page 22 Design Space Exploration System Performance How does my system performance change when I change two parameters? Performance Parameter #2 Performance Parameter #1 Danielle Wood Page 23 System Optimization • • • • • Define Objectives J Define Design Variables x Define Constraints and Bounds g, h Determine important fixed parameters p Typical Mathematical Problem Statement: “Minimize J such that g is less than zero; h is equal to zero; and the design variables are within given bounds” For more information on optimization methods see MIT Open Course Ware website: http://ocw.mit.edu/courses/aeronautics-and-astronautics/16-888multidisciplinary-system-design-optimization-spring-2004/ Danielle Wood Page 24 Small training satellite projects focus on certain aspects of relevant learning more than others Capability building is needed in several dimensions… Extent of Codification More Explicit More Managerial Knowledge: More Theoretical Skills: More Applied Level of Application More Technical Technical Nature More Tacit Danielle Wood Page 26 Typical Satellite Architecture Payload / Instrument Spacecraft Bus: Propellant, Power, Weight Attitude Det. & Control: Range and accuracy of payload Communications: data rate and volume Command and Data Handling: telemetry req’s Power: Average/peak power requirements Thermal: Payload and battery temperature limits Structures: Launch vibration and acceleration Guidance and Navigation: Payload pointing Propulsion: Delta-V and thrust level Computer Systems: Throughput, memory Danielle Wood Satellite subsystems and major design drivers (Wertz and Larson, SMAD, 1999) Page 27 Key Differences in Design Process Small Training Satellite Missions Traditional Satellite Missions Highly constrained design architecture Less constrained design architecture Low mission complexity – easily comprehended by entire team High mission complexity – each person focuses on subsystem Engineering team focuses on manufacture, test, assembly, integration Engineering team focuses on design, analysis and system level trade-offs Small team works in close communication Large team works in disjointed fashion Danielle Wood Page 28 Conclusions • Training satellite missions can be part of a long-term process of capability building • When is it best to apply these satellite systems engineering tools for payloads and buses? • The answer depends on… – – – – – – Project objectives Long term organizational strategy Experience level of participants Strengths of training organizations Need for project documentation Etc… Danielle Wood Page 29 Future Work Satellite Project Implementation Local Space Organization Collaborative Satellite Project Foreign Partner Danielle Wood Capability Building Page 31 Future Work: Learning Stories of Collaborate Satellite Projects Turkey Algeria Egypt UAE Malaysia Nigeria Danielle Wood Photo Credits: SSTL, EADS Astrium, SaTReC-I, Yuzhnoye) Page 32 Thank you! 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