• DocumentCode
    2748887
  • Title

    Brumby Uninhabited Aerial Vehicle flight dynamics-instrumentation and flight test results

  • Author

    Campbell, Jacob L. ; Kresge, Jared T.

  • Volume
    2
  • fYear
    2003
  • fDate
    12-16 Oct. 2003
  • Abstract
    This paper provides information on the design and performance of the instrumentation on the Ohio University Avionics Engineering Center´s (AEC) Uninhabited Aerial Vehicle (UAV), the Brumby. In 1999 AEC purchased the delta wing Brumby airframe to conduct UAV related research. Recently the Brumby has been outfitted with instrumentation to collect data allowing for the system identification of the Brumby UAV. The goal was a lightweight (<10 lbs), low-power (<25 watts) data collection system designed to time-stamp and store data from the airdata probe, digital compass, Global Positioning System (GPS) receiver, low cost Inertial Measurement Unit (IMU), and control surfaces. Also presented in this paper is the design methodology used in developing the data collection system, methods of time-stamping the data with precise GPS time, lessons learned about IMU operation in a high vibration environment, as well as the future design path of the avionics.
  • Keywords
    Global Positioning System; aircraft testing; avionics; compasses; identification; radio receivers; remotely operated vehicles; Brumby uninhabited aerial vehicle; GPS receiver; Ohio university avionics engineering center; airdata probe; avionics; data collection system; delta wing Brumby airframe; digital compass; flight dynamics instrumentation; flight test; global positioning system; inertial measurement unit; system identification; time stamping methods;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 2003. DASC '03. The 22nd
  • Conference_Location
    Indianapolis, IN, USA
  • Print_ISBN
    0-7803-7844-X
  • Type

    conf

  • DOI
    10.1109/DASC.2003.1245892
  • Filename
    5731137