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Hybrid Decompositional Verification for Discovering Failures in Adaptive Flight Control SystemsAdaptive flight control systems hold tremendous promise for maintaining the safety of a damaged aircraft and its passengers. However, most currently proposed adaptive control methodologies rely on online learning neural networks (OLNNs), which necessarily have the property that the controller is changing during the flight. These changes tend to be highly nonlinear, and difficult or impossible to analyze using standard techniques. In this paper, we approach the problem with a variant of compositional verification. The overall system is broken into components. Undesirable behavior is fed backwards through the system. Components which can be solved using formal methods techniques explicitly for the ranges of safe and unsafe input bounds are treated as white box components. The remaining black box components are analyzed with heuristic techniques that try to predict a range of component inputs that may lead to unsafe behavior. The composition of these component inputs throughout the system leads to overall system test vectors that may elucidate the undesirable behavior
Document ID
20100036719
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Thompson, Sarah
(SGT, Inc. Moffett Field, CA, United States)
Davies, Misty D.
(NASA Ames Research Center Moffett Field, CA, United States)
Gundy-Burlet, Karen
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 25, 2013
Publication Date
April 20, 2010
Subject Category
Aircraft Stability And Control
Report/Patent Number
ARC-E-DAA-TN1542
Report Number: ARC-E-DAA-TN1542
Meeting Information
Meeting: AIAA Infotech at Aerospace 2010
Location: Atlanta, GA
Country: United States
Start Date: April 20, 2010
End Date: April 22, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA08CG83C
Distribution Limits
Public
Copyright
Public Use Permitted.
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