Conventional PID, Adaptive PID, and Sliding Mode Controllers Design for Aircraft Pitch Control-Reference-Cited by-同舟云学术

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Conventional PID, Adaptive PID, and Sliding Mode Controllers Design for Aircraft Pitch Control

Published:2019-02 Issue: Volume: Page:
ISSN:
Container-title:2019 International Conference on Engineering and Emerging Technologies (ICEET)
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Author:

Khalid Adnan,Zeb Kamran,Haider Aun

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/8702267/8711817/08711871.pdf?arnumber=8711871

Cited by 13 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. Enhanced Fuzzy-Based Super-Twisting Sliding-Mode Control System for the Cessna Citation X Lateral Motion;Aerospace;2024-07-03

2. Design of an artificial neural network and proportional‐integral‐derivative controller using particle swarm optimization for Boeing 747‐400 aircraft pitch control;Advanced Control for Applications;2024-06-06

3. Control Schemes for Quadrotor UAV: Taxonomy and Survey;ACM Computing Surveys;2023-11-27

4. Comparison of Robust Stability for Pitch Attitude Boeing 747 Aircraft System Based on LQG and Observer Controller;2023 International Conference on Electrical and Information Technology (IEIT);2023-09-14

5. Implementation of Adaptive-PID Based Temperature Trajectory Tracking Control to Improve Repeatability in Coffee Roasting;2023 IEEE International Conference on Industry 4.0, Artificial Intelligence, and Communications Technology (IAICT);2023-07-13

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