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Integrated Aeropropulsion Control System Design%T Integrated Aeropropulsion Control System Design%A C-F. Lin%A Francis X. Hurley%A Jie Huang%A F. Y. Hadaegh%J International Conference on Control and Information(psi)995%C Hong Kong%D June 1995%K aeropropulsion, control, system%U http://jpltrs.jpl.nasa.gov/1995/95-0658.pdfAn integrated intelligent control approach is proposed to design a high performance control system for aeropropulsion systems based on advanced sensor processing, nonlinear control and neural fuzzy control integration. Our approach features the following innovations:??e complexity and uncertainty issues are addressed via the distributed parallel processing, learning, and online reoptimization properties of neural networks.??e nonlinear dynamics and the severe coupling can be naturally incorporated into the design framework.??e knowledge base and decision making logic furnished by fuzzy systems leads to a human intelligence enhanced control scheme.In addition, fault tolerance, health monitoring and reconfigurable control strategies will be accommodated by this approach to ensure stability, graceful degradation and reoptimization in the case of failures, malfunctions and damage.!.
Document ID
20060041871
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Lin, C. -F.
Hurley, Francis X.
Huang, Jie
Hadaegh, F. Y.
Date Acquired
August 23, 2013
Publication Date
June 1, 1996
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: International Conference on Control and Information
Location: Hong Kong
Country: China
Start Date: June 1, 1995
Distribution Limits
Public
Copyright
Other
Keywords
aeropropulsion control systems

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