Adaptive Sliding Mode Observer-Based Robust Fault Reconstruction for a Helicopter With Actuator Fault
Author:
Affiliation:
1. College of Automation Engineering; Nanjing University of Aeronautics and Astronautics; Nanjing 210016 China
2. School of Electrical and Electronic Engineering; Nanyang Technological University; Nanyang Avenue 639798 Singapore
Funder
Aeronautics Science Foundation of China
National Natural Science Foundation of China
Publisher
Wiley
Subject
Control and Systems Engineering
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1002/asjc.1243/fullpdf
Reference33 articles.
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2. Fault detection for a class of discrete time nonlinear systems subject to network induced uncertainties;Wan;Asian J. Control,2012
3. Observer-based fault diagnosis and self restore control for systems with measurement delays;Li;Asian J. Control,2012
4. Three-dimensional constrained tracking control via exact differentiation estimator of a quadrotor helicopter;Ghommam;Asian J. Control,2013
5. Actuator fault diagnosis: An adaptive observer-based technique;Wang;IEEE Trans. Autom. Control,1996
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