06.2 - Flight Dynamics and Control (UAV related)
FLIGHT MECHANICAL ANALYSIS OF A VERY FLEXIBLE HIGH-ALTITUDE PLATFORM UNDER UNCERTAINTY CONSIDERATIONS
Y.J. Hasan¹, N. Fezans¹, A. Voß, DLR Institute of Aeroelasticity, Germany; ¹DLR Institute of Flight Systems, Germany
This paper deals with a flight mechanical analysis of the high-altitude platform developed by the German Aerospace Center (DLR) respecting uncertainties. For this purpose, various weight and balance parameters of the used flexible flight dynamics model are varied and their influences on the aircraft's flight dynamics are assessed.