The purpose of this paper is to introduce a complex nonlinear model to a novel tandem ducted fan vehicle which adopted a structure of coaxial rotor and cyclic pitch system, considering aerodynamic coupling, disturbing between the upper and the lower rotor, and special aerodynamic characteristics of duct. On this basis, a robust hover control system has been designed to attitude control using H-infinite static output feedback theory. The results illustrate that the system has good decoupling performance and reveals great ability of attitude tracking as well as disturbance restraint.
Comprehensive nonlinear modeling and attitude control of a novel tandem ducted fan vehicle
2016-10-01
437581 byte
Conference paper
Electronic Resource
English
Modeling and Attitude Control of Tri-Tilt Ducted Fan Vehicle (AIAA 2016-0103)
British Library Conference Proceedings | 2016
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