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 — of-freedom module form standard 12 th  order rigid body dynamics is given.
['Jyotirmay Gadewadikar', 'Ognjen Kuljaca', 'Krunoslav Horvat']
Reduced order modeling for Unmanned Aerial Vehicle