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Hyperion UAV: An International Collaboration




         Jean Koster,
University of Colorado Boulder




           AIAA-ASM 2012, Nashville, TN, January 12, 2012
Collaboration

Jean Koster
   – University of Colorado Boulder, USA

Claus-Dieter Munz, Ewald Kraemer
   – University of Stuttgart, Germany

KC Wong, Dries Verstraete
   – University of Sydney Australia


                           Collaboration
                           AIAA-ASM 2012
Motivation: Green Aviation

     NASA’s ERA Goals
  Reduce:
     Aircraft fuel consumption
     Emissions
     Noise
                                                       Image credit: NASA
        …Simultaneously!



   “In 2009, … [the] United States flew 704 million passengers, a[1]
   number forecast to reach 1.21 billion by 2030.” – NASA Facts


                                 -Motivation-
                                 AIAA-ASM 2012                              3
Motivation: Reduce Noise
 Airport Noise Challenge: Aircraft noise regarded most significant hindrance to
    National Airspace System




                                                                   [1]

                                  Image credit: NASA

                                         -Motivation-
                                       AIAA-ASM 2012                              4
Motivation: Reduce Fuel Burn
 Fuel Problem:
     In 2008
            U.S. Commercial air burned 19.7 Billion Gallons
          + D.O.D. burned an additional 4.6 Billion Gallons
                                            250,000,000…
                              Tons of Carbon Dioxide (CO2)
                                                          [1]
                                      Nitrogen Oxide (NOx)

 Reduce NOx Emissions:       Goals            Reduce Fuel Burn:
     20% by 2015                               33% by 2015
     50% by 2020                               50% by 2020
                     [1]                                       [1]
    >50% beyond 2025                          >70% beyond 2025

                               -Motivation-
                              AIAA-ASM 2012                          5
Motivation: Blended Wing Body




                                    [2]

                                    Image credit: NASA

                     -Motivation-
                    AIAA-ASM 2012                        6
Purpose
WHY HYPERION?

• Society/ industry needs:
   – Aerodynamically & energy efficient aircraft
                                                                  Image credit: NASA
   – Prepare workforce in global environment

• History:
   – Colorado students developed hybrid propulsion system
   – Boeing interest in follow-the–sun design process
   – AIAA-ASM Meeting January 2010, Orlando:
      o NASA: “Environmentally Responsible Aviation (ERA) Project”
            Boeing X-48B prominently presented
      o Focus on aviation alternative fuels, fuel savings, reduced noise



                                        -Purpose-
                                      AIAA-ASM 2012
Global Project
  Why a global project?
 • Global companies operate Design Bureaus around the world.
    – Opportunities to expedite design work on new systems
    – Opportunities made available by software and internet
    – Opportunities to harvest bright minds


 • Manufacturing dispersed in many countries
    – For Boeing’s Dreamliner, 28 suppliers are located outside USA
       • Wings produced in Japan
       • Ailerons produced in Australia
       • Fairings produced in Canada
       • Doors produced in France and Sweden
       • Final assembly in USA

                                     -Purpose-
                                    AIAA-ASM 2012                     8
G.B. Shaw said:

 “If you have an apple and I have an apple
 and we exchange apples then you and I will
 still each have an apple.
 But if you have an idea and I have an idea
 and we exchange these ideas, then each of
 us will have two ideas.”
                          GBS
                      AIAA-ASM 2012
Global Team




               - Purpose -
              AIAA-ASM 2012   10
Goals




                            Boulder + Stuttgart + Sydney
   1.   Investigate new technologies for improved capabilities and efficiencies
   2.   Practice international collaboration in education

                               Undergraduate CU Team
   1.   Conceive, design, build, and test a 2nd generation hybrid propulsion
        system to be integrated into the Hyperion

                            Thank you to our sponsors!



                                      -Project Overview-
                                        AIAA-ASM 2012                             11
System Configuration




 • Aerodynamic design started by Sydney team                      See: AIAA-2012-0878

 • Raked wingtips & vertical stabilizers designed by Stuttgart team
 • Management, electronics, internal structure design & systems integration by CU

          •Hybrid-Electric Engine to explore quiet take-off and landings, quiet loitering,
          and improved efficiencies (CONOPS dependent)


                                         -Project Overview-
                                           AIAA-ASM 2012                                     12
Subsystem Design



                                               Aerodynamics


    Manufacturing

                                 Weights



                                            Materials/Structures


   Electronics


                    -Technology Overview-
                        AIAA-ASM 2012
Schedule




                                           Flight
 Start     PDR            CDR
                                          Testing




                 -Global Collaboration-
                     AIAA-ASM 2012                  14
Aerodynamics & Structures

 ½ Scale Wind Tunnel Model       Internal Structure        Center Body/Integration




  Aerodynamic Validation
                             Wing Integration/Assembly
                                                             CFD Validation




                                   -Technology Overview-
                                       AIAA-ASM 2012                                 15
Aerodynamic Analysis
   Aerodynamic Requirements:                    Aerodynamic testing was performed using
 L/D greater than 20                            multiple methods
 Statically stable                                       CFD
 Stall velocity less than 15 m/s                         1/2 scale wind tunnel testing
 Span efficiency (e) greater than 0.8
 Wing loading less than 15 kg/m²




                                        -Technology Overview-
                                            AIAA-ASM 2012                                 16
Manufacturing: Center Body
 Project Goal and Objectives
   Distributed Manufacturing




   • Negative molds milled               • Integration of internal
     from CAD-data                         structure from University
   • Fiberglass-foam-core skin             of Colorado
     laminated by hand




                           -Technology Overview-
                                 AIAA-ASM 2012                         17
Global Integration Manufacturing
              Delocalized manufacturing increases integration risk!
                                     Risk




                                   Mitigation

IDT (Interface Dimension                              Similar ideas used for
Template)                                             wing manufacturing
    • Device used to ensure
    German center body                                Winglet  Wing
    matches USA wings



                                   -Integration-
                                   AIAA-ASM 2012                               18
Global Integration

Need: Electronics integration into plane                      Problem: Plane center body in Germany!


Image
credit:
NASA



             Cubesat                        Broken Down Flat                Layout Electronics

                  Solution
 “Flat Sat” Approach (Simulation and Test-bed)
 - Used while center body is in Germany -
 • Full Scale Mockup of Center Body
 • Wire Length and placement
 • Hardware placement platform
 • Full system testing for electronics

                                              -Global Collaboration-
                                                     AIAA-ASM 2012                               19
FTS Example
 Colorado Team
 • Changes structure component
 • Does it meet Requirements?                                8 Hours
 • What does this mean for manufacturing
    and aerodynamics?

                      Sydney Team
                      • Evaluates Structural Implications on
                         Aerodynamic Design                              8 Hours
                      • Proposes design changes
                      • Provides aerodynamic feedback
      8 Hours
                                  Stuttgart Team
                                  • Evaluates Manufacturing implications on
                                     aerodynamic and structural designs
                                  • Proposes design changes
                                  • Provides manufacturing feedback



                                    -Global Collaboration-
                                        AIAA-ASM 2012
Hybrid Gas-Electric Engine
 Project Goal and Objectives
 Objective:
 Design, build and test a hybrid propulsion system to be integrated
 into the aircraft




  Offset drive                               Coaxial drive
  No control system                          Multiple flight mode control
  Focus: Efficiency, proof of                Focus: Reliability, operations
  concept                                               See: AIAA-2012-0147
                                -Technology Overview-
                                    AIAA-ASM 2012                             21
Testing
Dynamically (1/2) Scaled Prototype




 • Test aircraft capability and
   characteristics.
 • Identify unforeseen problems.
 • Pilot familiarization
 • Test: Taxi, takeoff, cruise, land
 • Test: Mass sensitivity, cg
 • Test: International analysis of data


                                  -Technology Overview-
                                          AIAA-ASM 2012   22
System Testing
  • Electric propulsion
     – Hybrid Engine fully bench tested, but not flight tested (maturity)
  • R/C Piloted
     – Successful takeoff, cruise, and landing




                                      Flight Test
                                     AIAA-ASM 2012                          23
FTS Collaboration Experiment
Pain: Efficiency in Global Industry Collaborations: needs improvement
                                   Concept
                3 Teams, distributed 8 hours apart relay work daily.
       Follow-the-Sun (FTS), produces 3 work-days in one 24 hour period


Results
• Accelerated project design progress:
   o Complete design drawn in CATIA in 5
      weeks
   o Conceived, designed, manufactured,
      and delivered aircraft to customer under
      budget and on time
   o Inception to Completion ~ 9 Months



                                  -Global Collaboration-
                                      AIAA-ASM 2012                       24
Best Practices
       IT Plan               Systems Engineering
       Concept of Operations                                                    Operation
            Develop and define
            mission phases               Verification and
                                         Validation                        Testing
             Project Requirements
                   Determine
                   verification method                               Integration
                   and develop tests

                   System Architecture
                                                                Manufacturing
                         Identify subsystem
                         interfaces and risks
                                                                                      Implement
       Project
                                         Detail IT Plan                               IT Plan
       Decomposition

                                                 Time
                                         - Integration & Testing -
                                                                                             12
        Internet Communication and Cloud File Sharing


                                         -Global Collaboration-
                                               AIAA-ASM 2012
Lessons Learned
 Language and Cultural Barriers
       Although everyone speaks Englineerish….

   Encodes/Writes                                      Decodes/Misinterprets
      Message                                                Message




  Decodes Message                                      Encodes Counter
                                                       Productive Feedback
                       Cloud Noise Filter Can Cause:   Message
                               -Loss of Tone
                              -Loss of Intent
                            -Misinterpretation

                             -Global Collaboration-
                                 AIAA-ASM 2012                           26
Lessons Learned
 Follow-the-Sun (FTS):
     • Great for CAD design work
     • Ideas across border
     • Dynamic positive synergy
     • Benefit of diversity in critical thinking
     • Helps mitigate risk through smaller team delegation
     • Difficult in academic environment due to schedules

 Follow-The-Week (FTW)
     • Suited for concept designs
     • Task assignments to small local teams
     • Finished tasks reviewed by global team
     • Weekly global team meetings.


                             -Global Collaboration-
                                 AIAA-ASM 2012               27
Lessons Learned
 • Project needs managerial infrastructure
    – Needs strong Project Manager
    – MBA candidate on team
    – Economics student on team
 • Understand international shipping requirements
    – ITAR
    – Understand international trade and regulations
 • Collaboration on “trust” and “respect”
    – Limited control over non-local teams’ efforts
    – Understand skills and capabilities of partners
    – Free sharing of information leads to IP issues
 • Planning
    – Extend the planning process significantly!
    – Better understand skills and capabilities of partners
    – Each partner should have own funding

                                  - Global Collaboration-
                                      AIAA-ASM 2012           28
Conclusion
• Successes:
   – Designed, built, and flew HYPERION in 9 months
      • Planning for 3 months
      • Design layout within 4 months
      • Aerodynamics and structures analysis using FTS
      • Controls system development
      • Delocalized manufacturing in 3 months
      • Under mass and finance budgets
      • Successful maiden flight




                                   AIAA-ASM 2012
Current Development



• Current Project Charter:
   – Design and Manufacturing shared by Stuttgart
     and Colorado
   – New wing design
       From Flying Wing to Blended Wing Body
   – Autonomous Control System
   – FAA COA
   – Integrate hybrid propulsion system and flight
     test




                                     - Current -
                                   AIAA-ASM 2012     30
Acknowledgements
A special thanks to…                              Skip Miller of Skip Miller Models
 Mike Kisska of Boeing                            James Mack of LASP (Pilot)
 Frank Doerner of Boeing
 Blaine Rawdon of Boeing
 Tom Hagen of Boeing
 Dr. Robert Liebeck of Boeing/USC
 Steven Yahata of Boeing
 Norman Princen of Boeing
 Diane Dimeff of eSpace
 Brian Taylor of NASA
 Joseph Tanner of CU
 Trent Yang of RASEI
 Dr. Donna Gerren of CU
 Prof. Eric Frew of CU
 Matt Rhode of CU
 Trudy Schwartz of CU
 Prof. Claus-Dieter Munz of Stuttgart
 Prof. Ewald Kraemer of Stuttgart
 Dr. KC Wong of Sydney
 Dr. Dries Verstraete of Sydney
                                        -Acknowledgements-
                                           AIAA-ASM 2012                              31
Student Global Team
                                             Derek Nasso                 Michael Johnson
                                               Julie Price               Eric Kenney
                                              E r i c S e r a ni         Jeremy Klammer
                                               Tom Wiley                 Lydia Mcdowell
                                            Richard Zhao                 Boris Papazov
                                           Kristen Brenner               Taylor Petersen
                                           C o r r i na G i b s o n      Robert Whitehill
                                           N a t h a n J a s t r am




 Michaela Cui                  Martin Arenz                           Kai Lehmkuehler
 Tyler Drake                   Holger Kurz                            M a t t he w A n d e r s o n
 A r t h ur K r e u t e r      David Pfeiffer                         J o s hu a B a r n e s
 Gavin Kutil                   M a t t hi a s S e i t z               Byron Wilson
 Brett Miller                  Baris Tunali                           Andrew McCloskey
 C o r e y P a c k a rd        J o n a s S c h w e ng l e r
 M a r c u s R a h i m po ur
 Gauravdev Soin


                                           -Team-
                                       AIAA-ASM 2012                                                 32
Questions?
Contact: jean.koster@colorado.edu
Budget




         Sponsors




                      - Budget-
                    AIAA-ASM 2012   34

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Hyperion Global AIAA-ASM-final

  • 1. Hyperion UAV: An International Collaboration Jean Koster, University of Colorado Boulder AIAA-ASM 2012, Nashville, TN, January 12, 2012
  • 2. Collaboration Jean Koster – University of Colorado Boulder, USA Claus-Dieter Munz, Ewald Kraemer – University of Stuttgart, Germany KC Wong, Dries Verstraete – University of Sydney Australia Collaboration AIAA-ASM 2012
  • 3. Motivation: Green Aviation NASA’s ERA Goals Reduce: Aircraft fuel consumption Emissions Noise Image credit: NASA …Simultaneously! “In 2009, … [the] United States flew 704 million passengers, a[1] number forecast to reach 1.21 billion by 2030.” – NASA Facts -Motivation- AIAA-ASM 2012 3
  • 4. Motivation: Reduce Noise Airport Noise Challenge: Aircraft noise regarded most significant hindrance to National Airspace System [1] Image credit: NASA -Motivation- AIAA-ASM 2012 4
  • 5. Motivation: Reduce Fuel Burn Fuel Problem: In 2008 U.S. Commercial air burned 19.7 Billion Gallons + D.O.D. burned an additional 4.6 Billion Gallons 250,000,000… Tons of Carbon Dioxide (CO2) [1] Nitrogen Oxide (NOx) Reduce NOx Emissions: Goals Reduce Fuel Burn: 20% by 2015 33% by 2015 50% by 2020 50% by 2020 [1] [1] >50% beyond 2025 >70% beyond 2025 -Motivation- AIAA-ASM 2012 5
  • 6. Motivation: Blended Wing Body [2] Image credit: NASA -Motivation- AIAA-ASM 2012 6
  • 7. Purpose WHY HYPERION? • Society/ industry needs: – Aerodynamically & energy efficient aircraft Image credit: NASA – Prepare workforce in global environment • History: – Colorado students developed hybrid propulsion system – Boeing interest in follow-the–sun design process – AIAA-ASM Meeting January 2010, Orlando: o NASA: “Environmentally Responsible Aviation (ERA) Project”  Boeing X-48B prominently presented o Focus on aviation alternative fuels, fuel savings, reduced noise -Purpose- AIAA-ASM 2012
  • 8. Global Project Why a global project? • Global companies operate Design Bureaus around the world. – Opportunities to expedite design work on new systems – Opportunities made available by software and internet – Opportunities to harvest bright minds • Manufacturing dispersed in many countries – For Boeing’s Dreamliner, 28 suppliers are located outside USA • Wings produced in Japan • Ailerons produced in Australia • Fairings produced in Canada • Doors produced in France and Sweden • Final assembly in USA -Purpose- AIAA-ASM 2012 8
  • 9. G.B. Shaw said: “If you have an apple and I have an apple and we exchange apples then you and I will still each have an apple. But if you have an idea and I have an idea and we exchange these ideas, then each of us will have two ideas.” GBS AIAA-ASM 2012
  • 10. Global Team - Purpose - AIAA-ASM 2012 10
  • 11. Goals Boulder + Stuttgart + Sydney 1. Investigate new technologies for improved capabilities and efficiencies 2. Practice international collaboration in education Undergraduate CU Team 1. Conceive, design, build, and test a 2nd generation hybrid propulsion system to be integrated into the Hyperion Thank you to our sponsors! -Project Overview- AIAA-ASM 2012 11
  • 12. System Configuration • Aerodynamic design started by Sydney team See: AIAA-2012-0878 • Raked wingtips & vertical stabilizers designed by Stuttgart team • Management, electronics, internal structure design & systems integration by CU •Hybrid-Electric Engine to explore quiet take-off and landings, quiet loitering, and improved efficiencies (CONOPS dependent) -Project Overview- AIAA-ASM 2012 12
  • 13. Subsystem Design Aerodynamics Manufacturing Weights Materials/Structures Electronics -Technology Overview- AIAA-ASM 2012
  • 14. Schedule Flight Start PDR CDR Testing -Global Collaboration- AIAA-ASM 2012 14
  • 15. Aerodynamics & Structures ½ Scale Wind Tunnel Model Internal Structure Center Body/Integration Aerodynamic Validation Wing Integration/Assembly CFD Validation -Technology Overview- AIAA-ASM 2012 15
  • 16. Aerodynamic Analysis Aerodynamic Requirements: Aerodynamic testing was performed using L/D greater than 20 multiple methods Statically stable CFD Stall velocity less than 15 m/s 1/2 scale wind tunnel testing Span efficiency (e) greater than 0.8 Wing loading less than 15 kg/m² -Technology Overview- AIAA-ASM 2012 16
  • 17. Manufacturing: Center Body Project Goal and Objectives Distributed Manufacturing • Negative molds milled • Integration of internal from CAD-data structure from University • Fiberglass-foam-core skin of Colorado laminated by hand -Technology Overview- AIAA-ASM 2012 17
  • 18. Global Integration Manufacturing Delocalized manufacturing increases integration risk! Risk Mitigation IDT (Interface Dimension Similar ideas used for Template) wing manufacturing • Device used to ensure German center body Winglet  Wing matches USA wings -Integration- AIAA-ASM 2012 18
  • 19. Global Integration Need: Electronics integration into plane Problem: Plane center body in Germany! Image credit: NASA Cubesat Broken Down Flat Layout Electronics Solution “Flat Sat” Approach (Simulation and Test-bed) - Used while center body is in Germany - • Full Scale Mockup of Center Body • Wire Length and placement • Hardware placement platform • Full system testing for electronics -Global Collaboration- AIAA-ASM 2012 19
  • 20. FTS Example Colorado Team • Changes structure component • Does it meet Requirements? 8 Hours • What does this mean for manufacturing and aerodynamics? Sydney Team • Evaluates Structural Implications on Aerodynamic Design 8 Hours • Proposes design changes • Provides aerodynamic feedback 8 Hours Stuttgart Team • Evaluates Manufacturing implications on aerodynamic and structural designs • Proposes design changes • Provides manufacturing feedback -Global Collaboration- AIAA-ASM 2012
  • 21. Hybrid Gas-Electric Engine Project Goal and Objectives Objective: Design, build and test a hybrid propulsion system to be integrated into the aircraft Offset drive Coaxial drive No control system Multiple flight mode control Focus: Efficiency, proof of Focus: Reliability, operations concept See: AIAA-2012-0147 -Technology Overview- AIAA-ASM 2012 21
  • 22. Testing Dynamically (1/2) Scaled Prototype • Test aircraft capability and characteristics. • Identify unforeseen problems. • Pilot familiarization • Test: Taxi, takeoff, cruise, land • Test: Mass sensitivity, cg • Test: International analysis of data -Technology Overview- AIAA-ASM 2012 22
  • 23. System Testing • Electric propulsion – Hybrid Engine fully bench tested, but not flight tested (maturity) • R/C Piloted – Successful takeoff, cruise, and landing Flight Test AIAA-ASM 2012 23
  • 24. FTS Collaboration Experiment Pain: Efficiency in Global Industry Collaborations: needs improvement Concept 3 Teams, distributed 8 hours apart relay work daily. Follow-the-Sun (FTS), produces 3 work-days in one 24 hour period Results • Accelerated project design progress: o Complete design drawn in CATIA in 5 weeks o Conceived, designed, manufactured, and delivered aircraft to customer under budget and on time o Inception to Completion ~ 9 Months -Global Collaboration- AIAA-ASM 2012 24
  • 25. Best Practices IT Plan Systems Engineering Concept of Operations Operation Develop and define mission phases Verification and Validation Testing Project Requirements Determine verification method Integration and develop tests System Architecture Manufacturing Identify subsystem interfaces and risks Implement Project Detail IT Plan IT Plan Decomposition Time - Integration & Testing - 12 Internet Communication and Cloud File Sharing -Global Collaboration- AIAA-ASM 2012
  • 26. Lessons Learned Language and Cultural Barriers Although everyone speaks Englineerish…. Encodes/Writes Decodes/Misinterprets Message Message Decodes Message Encodes Counter Productive Feedback Cloud Noise Filter Can Cause: Message -Loss of Tone -Loss of Intent -Misinterpretation -Global Collaboration- AIAA-ASM 2012 26
  • 27. Lessons Learned Follow-the-Sun (FTS): • Great for CAD design work • Ideas across border • Dynamic positive synergy • Benefit of diversity in critical thinking • Helps mitigate risk through smaller team delegation • Difficult in academic environment due to schedules Follow-The-Week (FTW) • Suited for concept designs • Task assignments to small local teams • Finished tasks reviewed by global team • Weekly global team meetings. -Global Collaboration- AIAA-ASM 2012 27
  • 28. Lessons Learned • Project needs managerial infrastructure – Needs strong Project Manager – MBA candidate on team – Economics student on team • Understand international shipping requirements – ITAR – Understand international trade and regulations • Collaboration on “trust” and “respect” – Limited control over non-local teams’ efforts – Understand skills and capabilities of partners – Free sharing of information leads to IP issues • Planning – Extend the planning process significantly! – Better understand skills and capabilities of partners – Each partner should have own funding - Global Collaboration- AIAA-ASM 2012 28
  • 29. Conclusion • Successes: – Designed, built, and flew HYPERION in 9 months • Planning for 3 months • Design layout within 4 months • Aerodynamics and structures analysis using FTS • Controls system development • Delocalized manufacturing in 3 months • Under mass and finance budgets • Successful maiden flight AIAA-ASM 2012
  • 30. Current Development • Current Project Charter: – Design and Manufacturing shared by Stuttgart and Colorado – New wing design  From Flying Wing to Blended Wing Body – Autonomous Control System – FAA COA – Integrate hybrid propulsion system and flight test - Current - AIAA-ASM 2012 30
  • 31. Acknowledgements A special thanks to… Skip Miller of Skip Miller Models Mike Kisska of Boeing James Mack of LASP (Pilot) Frank Doerner of Boeing Blaine Rawdon of Boeing Tom Hagen of Boeing Dr. Robert Liebeck of Boeing/USC Steven Yahata of Boeing Norman Princen of Boeing Diane Dimeff of eSpace Brian Taylor of NASA Joseph Tanner of CU Trent Yang of RASEI Dr. Donna Gerren of CU Prof. Eric Frew of CU Matt Rhode of CU Trudy Schwartz of CU Prof. Claus-Dieter Munz of Stuttgart Prof. Ewald Kraemer of Stuttgart Dr. KC Wong of Sydney Dr. Dries Verstraete of Sydney -Acknowledgements- AIAA-ASM 2012 31
  • 32. Student Global Team Derek Nasso Michael Johnson Julie Price Eric Kenney E r i c S e r a ni Jeremy Klammer Tom Wiley Lydia Mcdowell Richard Zhao Boris Papazov Kristen Brenner Taylor Petersen C o r r i na G i b s o n Robert Whitehill N a t h a n J a s t r am Michaela Cui Martin Arenz Kai Lehmkuehler Tyler Drake Holger Kurz M a t t he w A n d e r s o n A r t h ur K r e u t e r David Pfeiffer J o s hu a B a r n e s Gavin Kutil M a t t hi a s S e i t z Byron Wilson Brett Miller Baris Tunali Andrew McCloskey C o r e y P a c k a rd J o n a s S c h w e ng l e r M a r c u s R a h i m po ur Gauravdev Soin -Team- AIAA-ASM 2012 32
  • 34. Budget Sponsors - Budget- AIAA-ASM 2012 34