A Design Method for Attitude Control of a Helicopter Model Using Adaptive Backstepping Method

Abstract

The backstepping method is an effective approach for non-linear models, which can be easily extended to an adaptive control. However, since it has been mainly developed from the theoretical point of view, it requires more examples of the application to real systems. This paper considers about a design method for attitude control of a helicopter model whose model is described based on non-linear models.