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Formation Flying with Flexible Structures

This project explores the control of satellites equipped with flexible appendages within a formation flying cluster. Led by Erika Ooten Biediger and Kuniyuki Omagari, the research involves institutions from the USA and Japan, including Georgia Tech and Tokyo Institute of Technology. Key objectives include developing a control architecture, input shaping, and simulations to manage the dynamics of flexible structures. The initiative fosters collaboration through shared theories and experiments, with a focus on advancing space systems and their applications in robotic arm technology and solar panels.

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Formation Flying with Flexible Structures

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  1. Formation Flyingwith Flexible Structures Erika Ooten Biediger, Masaki Nagai, Kuniyuki Omagari, Ikutaro Morita Advisors: William Singhose, Saburo Matunaga, Chang Hee-Won 2002 University Space Systems Symposium

  2. Participating Universities • Georgia Institute of Technology • Tokyo Institute of Technology • University of North Dakota • University of Tokyo Project Manager : US: Erika Biediger Japan: Kuniyuki Omagari

  3. Current State of art

  4. Final Objective • Control satellites with flexible appendages in a Formation Flying Cluster • Robotic Arm • Solar Panel • Tethered cluster

  5. Additional flexible appendage

  6. Project Tasks • Control Architecture • UT, UND, TITech • Input Shaping • Ga Tech • Simulation • NASA Goddard • Experiments • TITech, UT

  7. Scenario Collaborative projects between Japan and USA • Shared theoretical and simulation development • Comparison of Independent simulation results • Ground experiment at Ti Tech + NASDA

  8. Schedule • Control architecture for two satellites • Add a flexible mode • Add input shaping • Simulation • Experiments at TITech & NASDA • Add motto flexible modes • Revise input shaping • Experiments at TITech & NASDA

  9. Timeline

  10. Future Objective

  11. Budget • Initial money in place to begin collaboration • Expansion of project may require additional funding

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