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• W2320042862 abstract "Flapping-wing ornithopters are emerging as a promising vehicle design for developing small scale unmanned air vehicles with multi-mission capabilities. One of the primary technical challenges currently impeding the maturation of apping-wing vehicle systems is the di culty in obtaining simple but accurate models of the complex aerodynamic ow elds which characterize apping ight. Typically aerodynamic models are based on rst principles, numerical models, or time-averaged wind tunnel testing. System identi cation provides an alternative that does not compromise the aerodynamic environment experienced in free ight. In this paper the authors present model structure determination results of lift and thrust forces generated by the apping wings of an ornithopter. A visual tracking system was used to obtain state measurements of the ornithopter while in trimmed straight and level mean ight. A multibody vehicle dynamics model, previous experimental results, model structure determination, and the equation-error parameter estimation routine used in both the time and frequency domains were used to determine models for the aerodynamic forces." @default.
• W2320042862 created "2016-06-24" @default.
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• W2320042862 date "2010-06-14" @default.
• W2320042862 modified "2023-09-27" @default.
• W2320042862 title "System Identification of an Ornithopter Aerodynamics Model" @default.
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• W2320042862 doi "https://doi.org/10.2514/6.2010-7632" @default.
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