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- W2330346380 abstract "UAV development and usage has increased dramatically in the last 15 years. In this time frame the potential has been realized for deployable UAVs to the extent that a new class of UAV was defined for these systems. Inflatable wing UAVs provide a unique solution for deployable UAVs because they are highly packable (some packing to 5-10% of their deployed volume) and have the potential for the incorporation of wing shaping. In this paper, aileron effectiveness was derived from the equations of motion of aircraft as a necessary parameter for roll control during autonomous flight. A modeling process was then developed to calculate the aileron effectiveness of a wing shaping demonstrator aircraft. Successful autonomous flight tests were performed with the demonstrator aircraft including in-flight aileron doublets to validate the predicted aileron effectiveness, which matched within 8%." @default.
- W2330346380 created "2016-06-24" @default.
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- W2330346380 date "2013-04-05" @default.
- W2330346380 modified "2023-09-25" @default.
- W2330346380 title "Modeling and Flight Testing of Wing Shaping for Autonomous Flight Control" @default.
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- W2330346380 doi "https://doi.org/10.2514/6.2013-1926" @default.
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