Deschide documentul
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Informaţii generale |
| Autor |
Espinoza, Tadeo; Dzul, Alejandro; Llama, Miguel |
| Publicat |
InTech Open Access Publisher, 2013
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| Ediţie |
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| Detaliază |
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| Abstract |
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. |
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International Journal of Advanced Robotic Systems
Autor: Ottaviano, Erika; Ceccarelli, Marco; Husty, Manfred; Yu, Sung-Hoon; Kim, Yong-Tae; Park, Chang-Woo; Hyun, Chang-Ho; Chen, Xiulong; Feng, Weiming; Sun, Xianyang; Gao, Qing; Grigorescu, Sorin M.; Pozna, Claudiu; Liu, Wanli; Zhankui, Wang; Guo, Meng; Fu, Guoyu; Zhang, Jin; Chen, Wenyuan; Peng, Fengchao; Yang, Pei; Chen, Chunlin; Ding, Rui; Yu, Junzhi; Yang, Qinghai; Tan, Min; Polden, Joseph; Pan, [...]
Publicat: 2004
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