Adaptive non-linear model inversion control of a twin rotor multi-input multi-output system using artificial intelligence
Author:
Affiliation:
1. School of Electrical and Electronics Engineering, Shiraz University of Technology, Shiraz, Iran
2. Department of Engineering, Queen Mary University of London, London, UK
3. King Abdulaziz University, Jeddah, Saudi Arabia
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1243/09544100JAERO155
Reference12 articles.
1. Synthesis of a helicopter nonlinear flight controller using approximate model inversion
2. Nonlinear Flight Control Using Neural Networks
3. On adaptive trajectory tracking of a robot manipulator using inversion of its neural emulator
4. Nonlinear inversion-based output tracking
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