Modeling and Simulation of Quadrotor UAV Using PID Controller

Karahan, Mehmet; Kasnakoğlu, Coşku

doi:10.1109/ecai46879.2019.9042043

Cited by 16 publications

(2 citation statements)

References 5 publications

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“…A PID controller is designed and proposed using Newton's Euler formula to establish the nonlinear dynamics model, the simulation demonstrate that it can achieve trajectory tracking in small perturbations [5].Another similar study can be found in [6].The authors in [7] developed an implicit PID controller with time and state constrains ,the feedback gain can be obtained by using Linear Matrix Inequalities. The main defect of this controller is the effect of model uncertainty on system stability.…”

Section: Pid Controllermentioning

confidence: 92%

A review of quadrotor control methods

Wei,

Ye,

Zhang

et al. 2023

AETR

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Quadrotor play an increasingly important role in emergency rescue and other comparable missions. However, external disturbances such as wind gusts and turbulence have a great impact on the stability of quadrotor, which means the control system of the vehicle needs to have a strong capability of anti- disturbance. This paper discuss the latest research on quadrotor control methods, and analyzes their characteristics and application. Traditional methods are improved and enhanced in order to attain better control performance. Meanwhile, artificial intelligence and hybrid control methods have garnered extensive research in the realm of quadrotor.

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Section: Pid Controllermentioning

confidence: 92%

A review of quadrotor control methods

Wei,

Ye,

Zhang

et al. 2023

AETR

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“…Therefore, the controller design of the QUAV is particularly important, which is related to the safe flight and economical reliability of the UAV. For the control of QUAV, the traditional method is to use the PID control algorithm [2]. The PID algorithm is simple in design, mature in technology, and has applications in a variety of long-span fields.…”

Section: Introductionmentioning

confidence: 99%

QUAV attitude control based on linear active disturbance rejection control

Li,

Tong,

Zhu

2023

ACE

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Unmanned Aerial Vehicle (UAV) are currently gaining popularity. This paper proposes a method to apply Linear Active Disturbance Rejection Control (LADRC) to Quadrotor Unmanned Aerial Vehicle (QUAV) controller to optimize the traditional PID controller. Firstly, the application and shortcomings of traditional PID control in UAV are introduced, and the LADRC method is proposed. Then linear simplification and Parameter Setting of ADRC are carried out. In the Simulink environment, according to the mathematical model of the QUAV, a QUAV dynamics simulation platform is established. Finally, according to different control channels, different control algorithms are designed, and tracking models are introduced in various attitudes to simulate and verify the control effect of LADRC. The results show that the LADRC controller is effective, the LADRC can be effectively combined with the traditional PID control. The application in the QUAV can realize more precise QUAV speed tracking control and the stable flight of the QUAV. Compared with the traditional PID controller, under the experimental conditions of this paper, the LADRC controller has more precise control accuracy and more efficient control efficiency. Finally, this paper summarizes the design of LADRC and makes a brief outlook on the development of UAVs.

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