Control System Design for a Vertical Takeoff and Landing Unmanned Aerial Vehicle Using a New Robust Optimization Method

The transitional flight control of tail-sitter aircraft is a challenging problem because the flight includes a wide operating range with nonlinearity and at low speed approaches the stall. In order to solve this problem, a robust autopilot design method using a variable environment genetic algorithm...

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Veröffentlicht in:	Theoretical and Applied Mechanics Japan 2009/02/27, Vol.57, pp.169-178
Hauptverfasser:	KUBO, Daisuke, SUZUKI, Shinji
Format:	Artikel
Sprache:	eng
Online-Zugang:	Volltext
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