A Study of the Interaction of Proportional-Integral- Derivative (PID) Control in a Quadcopter Unmanned Aerial Vehicle (UAV) Using Design of Experiment

Author:

Obias Karl Cedric U.,Say Marc Francis Q.,Fernandez Emil Adrian V.,Chua Alvin Y.,Sybingco Edwin

Publisher

IEEE

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Application research on improved genetic algorithm and active disturbance rejection control on quadcopters;Measurement and Control;2024-03-25

2. Design of Sliding Mode Control Law for Quadrotor With Adaptive Super Twisting Algorithm;Advances in Mechatronics and Mechanical Engineering;2024-03-15

3. Design and Simulation of a Model Predictive Control System Navigation of a Drone in Confined Spaces;2024 International Conference on Artificial Intelligence, Computer, Data Sciences and Applications (ACDSA);2024-02-01

4. Discrete Sliding Mode Control Law for Attitude & Altitude Control of Quadrotors with a Sliding Surface of PID Structure;2023 IEEE International Conference on Power Electronics, Smart Grid, and Renewable Energy (PESGRE);2023-12-17

5. Assessing optimal UAV-data pre-processing workflows for quality ortho-image generation to support coral reef mapping;Geocarto International;2022-02-09

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