Performance benefits of adaptive in-flight propulsion system optimization
Author:
Affiliation:
1. Pratt & Whitney Group, West Palm Beach, FL
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-3749
Reference6 articles.
1. Chisholm, J.D. 1992 "In-Flight Optimization of the Total Propulsion System", AIAA Paper AIAA-92-3744.
2. Ken, L.J., Nemec, T.S.Gallops, G.W., 1991 "Real-TimeEstimationofGasTurbineEngineDamageUsing a Control Based Kalman Filter Algorithm", ASME Paper 91-GT-216.
3. Luppold,R.H., Roman,J.R., Gallops,G.W., Kerr,L.J., 1989"Estimating In-Flight EnginePerformanceVariations Using Kalman Filter Concepts", AIAA Paper AIAA-89-2584.
4. Smith,R.H., Chisholm,J.D., Stewart,J.F., 1990"OptimizingAircraft Performancewith Adaptive Integrated Flighflropulsion Control", ASME Paper 9oGT-252.
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