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The structure of the wing of High Altitude Long Endurance (HALE) Unmanned Aerial Vehicle (UAV) is highly flexible, it's oscillation is obvious and coupled with the flight dynamic responses of the UAV, this influent the flight security seriously. In the stage of conceptual design of a solar UAV, in order to estimate the scheme rapidly and accurately, it is necessary to consider the dynamic performance...
The object of this paper is to design a robust longitudinal landing controller for a flying wing UAV, taking into account both actual ground effect and some typical atmospheric conditions. In order to track the desired trajectory even when the UAV is under influence of uncertainties and disturbances, a mixed H2/Hinfin, robust control method is adopted in this paper. The H2 part is to meet excellent...
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