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- W2481549480 abstract "This paper discusses the development and testing of an innovative small UAS (Unmanned Aircraft System). The design of the vehicle was driven by the need to both have long endurance yet still have the convenience of V/TOL (Vertical Take-Off and Landing) operation. The paper discusses some of the design considerations and configurations evaluated in searching for a configuration that met the demanding mission requirements. The paper also discusses some aspects of the compound wing and experimental testing conducted to discern the optimum parameters for the wing's design. The paper discusses the results of the preliminary flight testing and outlines further research to be conducted." @default.
- W2481549480 created "2016-08-23" @default.
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- W2481549480 date "2015-01-05" @default.
- W2481549480 modified "2023-09-24" @default.
- W2481549480 title "Design, Development, and Testing of a Compound Wing V/TOL small UAS" @default.
- W2481549480 hasPublicationYear "2015" @default.
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