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Fuzzy Logic Controller Stability Analysis Using a Satisfiability Modulo Theories ApproachWhile many widely accepted methods and techniques exist for validation and verification of traditional controllers, at this time no solutions have been accepted for Fuzzy Logic Controllers (FLCs). Due to the highly nonlinear nature of such systems, and the fact that developing a valid FLC does not require a mathematical model of the system, it is quite difficult to use conventional techniques to prove controller stability. Since safety-critical systems must be tested and verified to work as expected for all possible circumstances, the fact that FLC controllers cannot be tested to achieve such requirements poses limitations on the applications for such technology. Therefore, alternative methods for verification and validation of FLCs needs to be explored. In this study, a novel approach using formal verification methods to ensure the stability of a FLC is proposed. Main research challenges include specification of requirements for a complex system, conversion of a traditional FLC to a piecewise polynomial representation, and using a formal verification tool in a nonlinear solution space. Using the proposed architecture, the Fuzzy Logic Controller was found to always generate negative feedback, but inconclusive for Lyapunov stability.
Document ID
20180008608
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Arnett, Timothy
(Cincinnati Univ. OH, United States)
Cook, Brandon
(NASA Ames Research Center Moffett Field, CA, United States)
Clark, Matthew
(Air Force Research Lab. Wright-Patterson AFB, OH, United States)
Rattan, Kuldip
(Wright State Univ. Dayton, OH, United States)
Date Acquired
December 18, 2018
Publication Date
January 9, 2017
Subject Category
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN38074
Report Number: ARC-E-DAA-TN38074
Meeting Information
Meeting: SciTech 2017
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 154692.02.10.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Fuzzy Logic Controller
Formal Verification
Stability Analysis
Satisfiability Modulo Theories (SMT) Solver
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