A UAV flight-experiment system for the estimation of aerodynamic characteristics

Shin-Ichiro Higashino, Akira Sakurai

研究成果: Contribution to conferencePaper査読

4 被引用数 (Scopus)

抄録

A flight-experiment system including the test-bed vehicle, the ground station, and the catapult has been developed at Kyushu University, the purpose of which is to estimate aerodynamic characteristics of airplanes from flight data. Most of the sensors onboard are inexpensive and off-the-shelf ones in order to maintain the cost as low as possible, while the outputs of the sensors are carefully calibrated to assure data acquisition with high accuracy. The strong correlation among the variables which describes the change in a dependent aerodynamic variable is known as multicolinearity in regression analysis, which degrades the estimation accuracy. It is shown that this multicolinearity, which usually occurs among longitudinal variables due to elevator deflection is avoidable using an additional tail surface named a Flying Sting Balance.

本文言語英語
出版ステータス出版済み - 1 1 2003
イベント2nd AIAA "Unmanned Unlimited" Conference and Workshop and Exhibit 2003 - San Diego, CA, 米国
継続期間: 9 15 20039 18 2003

その他

その他2nd AIAA "Unmanned Unlimited" Conference and Workshop and Exhibit 2003
国/地域米国
CitySan Diego, CA
Period9/15/039/18/03

All Science Journal Classification (ASJC) codes

  • 航空宇宙工学
  • 制御およびシステム工学
  • 電子工学および電気工学
  • 機械工学

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