Detection, Identification and Estimation of Surface Damage/Actuator Failure for High Performance Aircraft
Author:
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx5/4789671/4789672/04790091.pdf?arnumber=4790091
Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. A non-conservative H−/H∞ solution for early and robust fault diagnosis in aircraft control surface servo-loops;Control Engineering Practice;2014-10
2. H ∞ ∕ H − LPV solutions for fault detection of aircraft actuator faults: Bridging the gap between theory and practice;International Journal of Robust and Nonlinear Control;2014-03-16
3. Robust Detection of Abnormal Aircraft Control Surface Position for Early System Reconfiguration;Fault Diagnosis and Fault-Tolerant Control and Guidance for Aerospace Vehicles;2013-06-27
4. Design of Norm Based Fault Detection and Isolation LPV Filters;Robust Control and Linear Parameter Varying Approaches;2013
5. Fault Detection and Diagnosis in Electrical Aircraft Flight Control System;AIAA Guidance, Navigation, and Control Conference;2011-06-14
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