A Robust Control Technique for Pitch Control of an Aeropendulum-Reference-Cited by-同舟云学术

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A Robust Control Technique for Pitch Control of an Aeropendulum

Published:2023-11-03 Issue: Volume:17 Page:257-261
ISSN:
Container-title:2023 6th International Conference on Robotics, Control and Automation Engineering (RCAE)
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Author:

Tanveer M. Hassan¹,Koduru Charles¹,Roy Rupam Gupta²,Lakhekar Girish V.³,Chun Cary¹

Affiliation:

1. Kennesaw State University,Department of Robotics and Mechatronics Engineering,Marietta,GA,United States,30067

2. National Institute of Technology,Department of Electronics and Instrumentation Engineering,Agartala, Barjala, Jirania, Agartala,Tripura,India

3. College of Engineering,Department of Instrumentation Engineering,Pune,Maharashtra,India

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/10398736/10398580/10398789.pdf?arnumber=10398789

Reference16 articles.

1. Nonaxisymmetric Stator Design for Boundary Layer Ingesting Fans

2. Robust pitch attitude hold with MRAC for a nonlinear light combat aircraft model

3. Optimization of PID Controller Gains of an Aircraft Pitch Control System Using Particle Swarm Optimization Algorithm

4. Optimal Real-Time Trajectory Control of a Pitch-Hover UAV with a Two Link Manipulator

5. Aircraft pitch control tracking with sliding mode control

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