Mathematical Modelling and Identification of a Quadrotor

被引：2

作者：

Cardenas R, Cesar A. ^{[1
]}

Collazos Morales, Carlos Andres ^{[1
]}

Ospina, Juan P. ^{[1
]}

Sanchez, Joaquin F. ^{[1
]}

Caro-Ruiz, Claudia ^{[1
]}

Hugo Grisales, Victor ^{[2
]}

Ariza-Colpas, Paola ^{[3
]}

De-la-Hoz-Franco, Emiro ^{[3
]}

Gonzalez, Ramon E. R. ^{[4
]}

机构：

[1] Univ Manuela Beltran, Vicerectoria Invest, Bogota, DC, Colombia

[2] Univ Nacl Colombia, Dept Ingn Mecan & Mecatran, Bogota, DC, Colombia

[3] Univ Costa, Barranquilla, Colombia

[4] Univ Fed Pernambuco, Dept Fis, Recife, PE, Brazil

来源：

COMPUTATIONAL SCIENCE AND ITS APPLICATIONS - ICCSA 2020, PT I | 2020年 / 12249卷

关键词：

Quadrotor; VTOL; Flight dynamics; UAV;

D O I：

10.1007/978-3-030-58799-4_19

中图分类号：

TP39 [计算机的应用];

学科分类号：

081203 ; 0835 ;

摘要：

Motivated by the important growth of VTOL vehicles research such as quadrotors and to a small extent autonomous flight, a quadrotor dynamical model is presented in this work. The purpose of this study is to get a better understanding of its flight dynamics. It is an underactuated system. So, a simplified and clear model is needed to implement controllers on these kind of unmanned aerial systems. In addition, a computational tool is used for validation purposes. For future works embedded or intelligent control systems can be developed to control them. Gyroscopic and some aerodynamics effects are neglected.

引用

页码：261 / 275

页数：15

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