Ground and flight tests of an innovative fuel management system in a twin-engine helicopter.
Carlos C. InsaurraldeJose M. Giron-SierraSantiago CifuentesJuan F. JiménezPublished in: SysCon (2013)
Keyphrases
- 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