Research Catalog

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

Title
An optimized integrator windup protection technique applied to a turbofan engine control [microform] / Stephen R. Watts and Sanjay Garg.
Author
Watts, Stephen R.
Publication
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]

Details

Additional Authors
  • Garg, Sanjay.
  • United States. National Aeronautics and Space Administration.
Description
1 v.
Series Statement
NASA technical memorandum ; 107035
Subject
  • Circuit protection
  • Control systems design
  • Digital integrators
  • Engine control
  • Integrators
  • Multivariable control
  • Power factor controllers
  • Propulsion system configurations
  • Systems engineering
  • Turbofan engines
Note
  • Distributed to depository libraries in microfiche.
Reproduction (note)
  • Microfiche.
Call Number
READEX Microfiche NAS 1.15:107035
OCLC
marcive34804336
Author
Watts, Stephen R.
Title
An optimized integrator windup protection technique applied to a turbofan engine control [microform] / Stephen R. Watts and Sanjay Garg.
Imprint
[Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
Series
NASA technical memorandum ; 107035
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.
Added Author
Garg, Sanjay.
United States. National Aeronautics and Space Administration.
Gpo Item No.
0830-D (MF)
Sudoc No.
NAS 1.15:107035
Research Call Number
READEX Microfiche NAS 1.15:107035
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