Modeling and flight testing of the longitudinal dynamics of an inflatable wing UAV

Ainsmar X. Brown, Eric N. Johnson

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The field of man portable UAVs is currently a key area in improving the fielded warrior's capabilities. Pressurized aerostructures that can perform with results similar to solid structures could potentially change how this objective may be accomplished now and in the future. A flight dynamics simulation with reduced-order aeroelastic effects derived with Lagrangian and Eulerian dynamics approaches is developed and optimized to predict the behavior of inflatable flexible structures in small UAVs. The model also includes compensation for large buoyancy ratios and an investigation of the effects on different modes of forward flight. Existing literature documents the similarity in structural dynamics of rigid beams and inflatable beams before wrinkling. Thus, wing bending and torsional modes are approximated with the geometrically exact intrinsic beam equations using NATASHA (Nonlinear Aeroelastic Trim And Stability for HALE Aircraft) code. Some brief discussion also includes unique behaviors such as the onset of failure in the wing. An experimental glider platform is designed and flight tested. Data logged from these tests are used to support simulation model data. These results may later be used to specify recommended limits on flight maneuvers for inflatable UAVs.

Original languageEnglish (US)
Title of host publicationAIAA Atmospheric Flight Mechanics Conference 2011
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781624101533
DOIs
StatePublished - 2011
EventAIAA Atmospheric Flight Mechanics Conference 2011 - Portland, OR, United States
Duration: Aug 8 2011Aug 11 2011

Publication series

NameAIAA Atmospheric Flight Mechanics Conference 2011

Other

OtherAIAA Atmospheric Flight Mechanics Conference 2011
CountryUnited States
CityPortland, OR
Period8/8/118/11/11

All Science Journal Classification (ASJC) codes

  • Energy Engineering and Power Technology
  • Fuel Technology
  • Aerospace Engineering
  • Mechanical Engineering

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  • Cite this

    Brown, A. X., & Johnson, E. N. (2011). Modeling and flight testing of the longitudinal dynamics of an inflatable wing UAV. In AIAA Atmospheric Flight Mechanics Conference 2011 (AIAA Atmospheric Flight Mechanics Conference 2011). American Institute of Aeronautics and Astronautics Inc.. https://doi.org/10.2514/6.2011-6377