A Modified Feedback Linearization approach to UAV Control

The present report, consists of three major parts to approach the UAV problem which are in comparison with each other. First of all, an exact and complete dynamic model is needed for UAV problem. Followed by there exist two major viewpoints to the problem. First is the nonlinear approach without any simplification and second viewpoint is to linearized the system then applying the control theories to the simplified linear system without any loss of generality. Finally the results from each viewpoints will come in comparison with each other.

کلیدواژه ها:

Nonlinear ، linearization ، UAV