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DEIMOS Engenharia Technology maturation for space applications

DEIMOS Engenharia Technology maturation for space applications. Enabling space science Engineering design and development of complex systems required for science missions. science oriented tech specific. Universities & research institutes. R & D Algorithms Numerical methods.

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DEIMOS Engenharia Technology maturation for space applications

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  1. DEIMOS EngenhariaTechnology maturation for space applications

  2. Enabling space science Engineering design and development of complex systems required for science missions.

  3. science oriented tech specific Universities & research institutes R & D Algorithms Numerical methods Software design Comercial applications Software providers SW R&D software oriented Non-science

  4. All staff hold a university degree (5 year course) in aerospace, physics or software engineering About 30% of staff have a Master or PhD relevant areas of aerospace engineering Trainees from top universities: IST, FCT-UNL, UL, etc,…

  5. Science Data Processing Systems • Leading expertise in Europe • Physical description • Mathematical modeling • Operational software develop. • Example missions • SMOS (2003 - now) • Interferometer mission • Partners:INETI CRSW UPCatalunha CNRS • Sentinel 3 (2008 - ) • Optical Ground Processor Prototype • Optical System Simulator • Microwave radiometer

  6. Advanced Navigation Technologies Research & Development Galileo SoL Receiver development Advanced Hybrid Nav Systems Multi Constellation Conceptual studies Mission Critical Operational SW Galileo Orbit calibration tool Galileo Orbit & Clocks independent validation

  7. Spacecraft Simulation & Control • Guidance, Navigation and Control Algorithms & Simulation Tools • Planetary Landing • In-orbit Rendezvous • Atmospheric Entry • Satellite Formation Flying • Reference partner of ESA • Present in all European future missions • State of the art technology

  8. 40 missions to Mars last 50 years (17 successes) In orbit or local exploration, data sent to Earth Future mission = Mars... and back More complexity More authonomy Technologic challenge Automated rendezvous Low fuel orbits Hazard avoidance landing Technology for Mars Exploration

  9. Technology Maturation in RDV technology Technology readiness level TRL 9 Mission ready TRL 6 In-flight validation TRL 3 Concept validation FF GTO 2006 2003 2009 2012

  10. Formation Flying concept demo in Geo Transfer Orbit (GTO) SMART-3 baseline: 3-spacecraft interferometer in GTO Achievements Mission analysis, Scenario Modelling Guidance Algorithms for Formation Flying demonstration Development of 6DOFsimulation tool Team:IST/ISR – DEIMOS (PTF) 2003 - 2006 TRL 3

  11. Technology Maturation in RDV technology Technology readiness level TRL 9 mission ready TRL 6 In-flight validation TRL 3 Concept validation FF GTO VB-RNAV 2006 2003 2009 2012

  12. Visual-based GNC technology (TRL 3) Design automated GNC using camera sensor Mission design and analysis Design and evaluation of RVD G&C algorithms Landing & Guidance techniques for hazard avoidance during landing Guidance and Control for RVD passive target Team DEIMOS-INETI-LUSOSPACE (PTF) 2003 – 2006 TRL3 Rendezvous in Mars Orbit – credit JF&A Caloris Basin Floor (Mercury) -Source: Calvin J. Hamilton

  13. Technology Maturation in RDV technology Technology readiness level TRL 9 Mission ready TRL 6 In-flight validation GNCO-MAT TRL 3 Concept validation GNCO FF GTO VB-RNAV 2006 2003 2009 2012

  14. GNC technology for non-circular orbits (TRL 3) Fundamental for coming space exploration mission Never done at world level Achievements Full concept definition of autonomous RVD and FF in NCO Feasibility demonstration of RVD in elliptical orbits Validation complete autonomous GNC system. Team: DEIMOS, INETI, LUSOSPACE PTF 2006 -> 2008

  15. GNC technology for non-circular orbits (TRL 4) Maturation and validation Achievements Improved GNC algorithms Real-time platform On-ground experiment Team: DEIMOS INETI AURORA Program 2007 > 2010

  16. Technology Maturation in RDV technology Technology readiness level TRL 9 Mission ready PROBA 3 Exp TRL 6 In-flight validation GNCO-MAT TRL 3 Concept validation GNCO FF GTO VB-RNAV 2006 2003 2009 2012

  17. Rendezvous Experiment in elliptical orbit ( world first! ) 2008 – 2010 TRL6 • PROBA 3 Formation Flying Demo mission • All ESA FF missions • DEIMOS+INETI • National proposal GSTP4 We are part of Mission Requirements Objective: Flight Experiment

  18. Long term strategy Clear technology goals Coherence on project selection and execution Stability of partners network, specially science and users Challenges Investement in-house expertise Consolidation of technology and skills Consistent funding sources Locus of unique technologies at world level Space Flight control systems (GNC) Advanced Navigation Technologies Scientific data processing systems Wrap up Deimos vision

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