  This paper addresses the design and application controller for a small-size
unmanned aerial vehicle (UAV). In this work, the main objective is to study the
modeling and attitude controller design for a small size helicopter. Based on a
non-simplified helicopter model, a new robust attitude control law, which is
combined with a nonlinear control method and a model-free method, is proposed
in this paper. Both wind gust and ground effect phenomena conditions are
involved in this experiment and the result on a real helicopter platform
demonstrates the effectiveness of the proposed control algorithm and robustness
of its resultant controller.
