Altitude and roll control of a hovering quad-rotor air vehicle using the multi-objective approximate optimization of proportional–integral–differential control-Reference-Cited by-同舟云学术

Altitude and roll control of a hovering quad-rotor air vehicle using the multi-objective approximate optimization of proportional–integral–differential control

Published:2017-02-08 Issue:10 Volume:49 Page:1704-1718
ISSN:0305-215X
Container-title:Engineering Optimization
language:en
Short-container-title:Engineering Optimization

Author:

Yoon Jaehyun¹,Lee Jongsoo¹

Affiliation:

1. School of Mechanical Engineering, Yonsei University, Seoul, Republic of Korea

Funder

This work was supported by the Korea Institute of Energy Technology Evaluation and Planning (KETEP) and the Ministry of Trade, Industry & Energy (MOTIE) of Republic of Korea.

Publisher

Informa UK Limited

Subject

Applied Mathematics,Industrial and Manufacturing Engineering,Management Science and Operations Research,Control and Optimization,Computer Science Applications

Link

https://www.tandfonline.com/doi/pdf/10.1080/0305215X.2016.1265201

Reference20 articles.

1. Optimization of Lift Force of Mini Quadrotor Helicopter by Changing of Gap Size between Rotors

2. Backstepping Control Design with Actuator Torque Bound for Spacecraft Attitude Maneuver

3. Bouabdallah, S. 2007. “Design and Control of Quadrotors with Application to Autonomous Flying.” PhD diss. École Polytechnique federale de Lausanne.

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