Plasma Actuators for Hingeless Aerodynamic Control of an Unmanned Air Vehicle

The use of dielectric barrier discharge plasma actuators for hingeless flow control over a 47-deg 1303 unmanned combat air vehicle wing is described. Control was implemented at the wing leading edge to provide longitudinal control without the use of hinged control surfaces. Wind-tunnel tests were co...

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Veröffentlicht in:	Journal of aircraft 2007-07, Vol.44 (4), p.1264-1274
Hauptverfasser:	Patel, Mehul P, Ng, T. Terry, Vasudevan, Srikanth, Corke, Thomas C, He, Chuan
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Applied sciences Computer science control theory systems Control theory. Systems Design engineering Dielectrics Exact sciences and technology Robotics Unmanned aerial vehicles
Online-Zugang:	Volltext
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