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- W1888497923 abstract "It is very difficult to acquire high-fidelity flight test data for small airplanes such as typical unmanned aerial vehicles and RC airplanes because MEMS-type small sensors used in the tests do not present reliable data in general. Besides, it is not practical to conduct expensive flight tests for low-priced small airplanes in order to simulate their flight characteristics. A practical approach to obtain acceptable flight data, including stability and control derivatives and data of weights and balances, is proposed in this study. Aircraft design software such as Darcorp's AAA is used to generate aerodynamic data for small airplanes, and moments of inertia are calculated from CATIA, structural design software. These flight data from simulation software are evaluated subjectively and tailored using simulation flight by experienced pilots, based on the certified procedure in FAA AC 120-40B, which are prepared for manned airplane simulators. Use of design S/W for generation of parameter values representing flight characteristics turns out valid. In this study a practical procedural standard is established for procuring reliable data replicating flight characteristics of an airplane." @default.
- W1888497923 created "2016-06-24" @default.
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- W1888497923 date "2005-01-01" @default.
- W1888497923 modified "2023-09-23" @default.
- W1888497923 title "Derivation of Flight Characteristics Data of Small Airplanes Using Design Software and Their Validation by Subjective Tests" @default.
- W1888497923 cites W2313145432 @default.
- W1888497923 doi "https://doi.org/10.1007/978-3-540-30585-9_50" @default.
- W1888497923 hasPublicationYear "2005" @default.
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