Propulsion system/flight control integration and optimization: flight evaluation and technology transition
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ADECS mode afterburning ailerons aircraft airdata airflow airframe-propulsion system altitude control altitude hold mode Ames Research Center angle of attack automatic inlet autopilot autothrottle compressor stall constant thrust control loop control mode cruise flight DEFCS developed digital control Digital Electronic Control digital electronic engine Dryden Flight Research dutch roll EEL mode electronic engine control engine control system engine life mode engine parameters EPR uptrim extended engine F100 engine fan and compressor fan speed Fan stall flight conditions flight control system flight demonstration flight evaluation Flight Research Facility flightpath control FTIT HIDEC and PSC HIDEC program inlet geometry intermediate power Kalman filter lateral-directional Mach hold Mach number mance maximum thrust NASA F-15 airplane nozzle optimization parameter identification percent Performance Seeking Control predicted propulsion system RCVV research program scheduled shown in Fig SR-71 fleet stability augmentation stall margin supersonic cruise temperature throttle thrust improvements Thrust increase tion turbine turbofan WFGG