Parameter‐dependent Riccati equation–based output feedback adaptive control
Author:
Affiliation:
1. School of Aerospace Engineering Georgia Institute of Technology Atlanta GA 30332 USA
2. Department of Mechanical Engineering University of South Florida Tampa FL 33620 USA
Funder
Air Force Office of Scientific Research
Publisher
Wiley
Subject
Electrical and Electronic Engineering,Signal Processing,Control and Systems Engineering
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/acs.2788
Reference41 articles.
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2. KimK YucelenT CaliseA NguyenN.Adaptive output feedback control for an aeroelastic generic transport model: A parameter dependent Riccati equation approach. Paper presented at: AIAA Guidance Navigation and Control Conference;2011;Portland Oregon USA.
3. Robustness of a Derivative-Free Adaptive Control Law
4. MuseJA TchieuAA KutayAT ChandramohanR CaliseAJ.Vortex model based adaptive flight control using synthetic jets. Paper presented at: AIAA Guidance Navigation and Control Conference;2009;Chicago IL USA.
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