Flight mechanics analysis of a tilt-rotor UAV

Date

1999-01-01

Author

Okan, A.
Tekinalp, Ozan
Kavsaoğlut, M.Ş.
Armutcuoğlu, >Ö.
Tulunay, E.

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A new tilt-rotor UAV concept is proposed. Some results from the preliminary design study are presented. The flight mechanics equations for this tilt-rotor UAV are given. Trim flight conditions are obtained solving the optimization problems posed. For this purpose a trim program is written which uses an optimization routine. Various trim-flight conditions for hover, transition and cruise are obtained and the airplane stability at these particular flight conditions is discussed.

URI

https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=70749102415&origin=inward
https://hdl.handle.net/11511/107363

DOI

https://doi.org/10.2514/6.1999-4255

Conference Name

24th Atmospheric Flight Mechanics Conference, 1999

Collections

Department of Aerospace Engineering, Conference / Seminar

Citation Formats

A. Okan, O. Tekinalp, M. Ş. Kavsaoğlut, >. Armutcuoğlu, and E. Tulunay, “Flight mechanics analysis of a tilt-rotor UAV,” presented at the 24th Atmospheric Flight Mechanics Conference, 1999, Oregon, Amerika Birleşik Devletleri, 1999, Accessed: 00, 2023. [Online]. Available: https://www.scopus.com/inward/record.uri?partnerID=HzOxMe3b&scp=70749102415&origin=inward.