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Ground and flight tests of an innovative fuel management system in a twin-engine helicopter.
Carlos C. Insaurralde
Jose M. Giron-Sierra
Santiago Cifuentes
Juan F. Jiménez
Published in:
SysCon (2013)
Keyphrases
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flight test
management system
parameter identification
flight data
fuel injection
nasa langley research center
closed loop
fuel consumption
rapid prototyping
wind tunnel
control law
digital elevation models
fuzzy model
unmanned aerial vehicles
control scheme
reinforcement learning
mathematical model
non stationary
high resolution
diesel engine
image analysis
high pressure
expert systems