Integral Nonlinear Dynamic Inversion based Control of Input-Derivative Affine Systems
Author:
Affiliation:
1. Institute of Space Technology,Department of Aeronautics & Astronautics,Islamabad
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/9989533/9990034/09990509.pdf?arnumber=9990509
Reference16 articles.
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3. Robust gain-scheduled linear parameter-varying control algorithm for a lab helicopter: A linear matrix inequality–based approach
4. Real time adaptive nonlinear model inversion control of a twin rotor MIMO system using neural networks
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