Optimization of Landing Attitude Stability for Quadrotor Drones

Authors

  • Yang Xiao

DOI:

https://doi.org/10.54097/ajst.v6i3.10166

Keywords:

Quadrotor drone, Attitude control, Fuzzy PID algorithm.

Abstract

During the regular landing process of drones, they are often susceptible to the impact of ground effect and wind disturbances, which results in an inability to maintain parallelism with the ground. Drones are subjected to various types of wind disturbances during landing. Therefore, this study aims to analyze and model the varying characteristics of wind speed under natural conditions and introduce it as environmental noise into the system to evaluate the performance of the control algorithm. The goal of this research is to mitigate the impact of wind disturbances, such as oscillations during the landing process. By maintaining the pitch angle within 20%, we can ensure the drone lands quickly and accurately. In terms of algorithm, this research improves upon the existing PID (Proportional-Integral-Derivative) algorithm control for landing, and adopts a modified fuzzy PID algorithm, which can effectively enhance the control performance and response time of the drone.

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References

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Published

27-07-2023

Issue

Section

Articles

How to Cite

Optimization of Landing Attitude Stability for Quadrotor Drones. (2023). Academic Journal of Science and Technology, 6(3), 26-29. https://doi.org/10.54097/ajst.v6i3.10166

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