AERODYNAMIC IDENTIFICATION AND MODELING OF GENERIC UCAV CONFIGURATIONS WITH CONTROL SURFACE INTEGRATION
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As aircraft are increasingly specialized for low-observability and maneuverability, the aerodynamic identification process has become increasingly important. Recently, the aerodynamics of Unmanned Combat Aerial Vehicle (UCAV) configurations have been of interest. Two UCAV designs of the same planform were the subject of this research. Techniques for aerodynamic identification were explored using data generated by computational fluid dynamics (CFD). The Kestrel CFD solver was used to execute prescribed motion maneuvers, which simultaneously excite multiple flight parameters including inboard and ...