An optimized integrator windup protection technique applied to a turbofan engine control

An optimized integrator windup protection technique applied to a turbofan engine control

Bibliographic Details
Main Author: Watts, Stephen R
Corporate Author: United States National Aeronautics and Space Administration
Other Authors: Garg, Sanjay
Format: Government Document Book
Language:English
Published: [Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration ; National Technical Information Service, distributor, 1995]
Series:NASA technical memorandum 107035
Subjects:
Circuit protection
Control systems design
Digital integrators
Engine control
Integrators
Multivariable control
Power factor controllers
Propulsion system configurations
Systems engineering
Turbofan engines

Internet

Stanford University

Holdings details from Stanford University
Call Number: NAS 1.15:107035

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