Quadrotor Modeling and a PID Control Approach

被引：3

作者：

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

Hugo Grisales, Victor ^{[2
]}

Collazos Morales, Carlos Andres ^{[3
]}

Ceron-Munoz, H. D. ^{[4
]}

Ariza-Colpas, Paola ^{[5
]}

Caputo-Llanos, Roger ^{[5
]}

机构：

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

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

[3] Univ Manuela Beltran, Grp Ciencias Basicas & Labs, Bogota, DC, Colombia

[4] Univ Sao Paulo, Dept Aeronaut Engn, Sao Paulo, Brazil

[5] Univ Costa, Dept Ciencias Comp & Elect, Barranquilla, Colombia

来源：

INTELLIGENT HUMAN COMPUTER INTERACTION (IHCI 2019) | 2020年 / 11886卷

关键词：

Quadrotor; PID control; VTOL; Flight dynamics;

D O I：

10.1007/978-3-030-44689-5_25

中图分类号：

TP18 [人工智能理论];

学科分类号：

081104 ; 0812 ; 0835 ; 1405 ;

摘要：

Since there has been an important increase in unmanned vehicles systems research such as quadrotors, a mathematical model and PID control laws are studied. Based on some dynamic variables, PID control is applied to compute a controller to be then use in autopilot simulations. As this kind of VTOL vehicle seems to be unstable, the aim of this work is to change even other flight mechanics parameters and control gains to study attitude and altitude variations. A well-known computational tool is used for simulation purposes, performance analysis and validation.

引用

页码：281 / 291

页数：11

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