engleski

Reduced Order Modeling for Unmanned Aerial Vehicle

This paper presents a reduced order modeling procedure for Rotary wing Unmanned Aerial Vehicles. There is a growing interest in developing control strategies for unmanned autonomous helicopters, in particular a small scale one. The procedure for deriving a six degrees –offreedom module form standard 12th order rigid body dynamics is given.

Reduced Order Modeling; Rotary Wing Unmanned Aerial Vehicle

nije evidentirano