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H
∞
-based model following method in autolanding systems
K. Tamkaya
*
, L. Ucun,
I. Ustoglu
*
Corresponding author for this work
Department of Control and Automation Engineering
Yildiz Technical University
Research output
:
Contribution to journal
›
Article
›
peer-review
7
Citations (Scopus)
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∞
-based model following method in autolanding systems'. Together they form a unique fingerprint.
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Keyphrases
Automatic Landing System
100%
Auto-landing
100%
Model Following
100%
Following Methods
100%
Severe Weather Conditions
66%
Wind Shear
66%
Cost Function
33%
Tracking Performance
33%
Linear Matrix Inequality
33%
Dynamic Controller
33%
External Disturbances
33%
Optimal Control Problem
33%
Flight Systems
33%
Safe Landing
33%
Landing Phase
33%
Synthesis Methods
33%
Overall System
33%
K-configurations
33%
Induced Risk
33%
Engineering
Landing Aid
100%
Cost Function
33%
Design Method
33%
Synthesis Method
33%
External Disturbance
33%
Optimal Control Problem
33%