Propulsion System/flight Control Integration and Optimization: Flight Evaluation and Technology TransitionNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990 - Airplanes - 22 pages |
Common terms and phrases
afterburning aircraft airdata airflow airframe-propulsion system altitude control altitude hold mode Ames Research Center angle of attack augmentation system Augmentor fuel autopilot autothrottle compressor stall constant thrust control mode cruise flight DEEC DEFCS developed digital control digital electronic engine Dryden Flight Research dutch roll EEL mode electronic engine control engine control system engine life mode EPR uptrim extended engine F100 engine flight conditions flight control integration flight control system flight demonstration flight evaluation Flight Research Facility flightpath control FTIT HIDEC and PSC HIDEC program Highly Integrated Digital inlet geometry intermediate power Kalman filter lateral-directional lb/in² Mach hold Mach number maximum thrust NASA Ames Research NASA F-15 airplane nozzle optimization percent Performance Seeking Control predicted propulsion and flight propulsion system RCVV request EPR research program scheduled shown in Fig SR-71 fleet stall margin supersonic cruise temperature throttle thrust improvements Thrust increase tion turbine turbofan WFGG