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Accurate dynamic modeling of helicopter aeromechanics is becoming increasingly important, as progressively stringent requirements are being imposed on rotorcraft control systems. System identification plays an important role as an effective approach to the problem of deriving or fine tuning mathematical models for purposes such as handling qualities assessment and control system design. In this paper,...
In this paper, the modeling and robust control design of a vertical flight attitude control for a mini tail-sitter with variable pitch propeller is discussed. Tail-sitters vertical take-off and landing - unmanned aerial vehicles (VTOL-UAVs) have the operational flexibility of a typical helicopter while having the cruise performance of a fixed wing airplanes. The VTOL-UAVs configuration used in this...
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