Linear and Nonlinear Controllers Applied to Fixed-Wing UAV

International Journal of Advanced Robotic Systems

关键词: Airplane Dynamic Modelling;    Linear Control;    Nonlinear Control;   

DOI  :  10.5772/53616

学科分类：自动化工程

来源: InTech

【 摘 要 】

This article presents a comparison of controllers which have been applied to a fixed-wing Unmanned Aerial Vehicle (UAV). The comparison is realized between classical linear controllers and nonlinear control laws. The concerned linear controllers are: Proportional-Derivative (PD) and Proportional-Integral-Derivative (PID), while the nonlinear controllers are: backstepping, sliding modes, nested saturation and fuzzy control. These controllers are compared and analysed for altitude, yaw and roll by using simulation tests.

【 授权许可】

CC BY