The Caltech Ducted Fan is a flight control experiment whose dynamics are representatvie
of the longitudinal dynamics of an aircraft. The experiment has been designed
to study rapid transition between hover, forward flight and reverse flight, as
well as other agressive flight manuevers. It serves as a test stand for laboratory
validation of a variety of theory and software being developed at Caltech, including
LPV,MPC and nonlinear control,robust nonlinear anaysis, model validation and real-time
control algorithm.