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afterburner aircraft and fleet altitude approximately baseline engine CIVV component deviation parameter constraints control variables CPSM cruise conditions decrease in TSFC DEEC DEHPT DELPT DINL Dryden Flight Research DWFAN DWHPC dynamics engine and linear Engine Control engine operating condition Engine parameter EPR and WCFAN F-15 aircraft fan turbine inlet Flight Research Facility function of Mach Gilyard HIDEC high-pressure compressor airflow high-pressure turbine Highly Integrated Digital Kalman filter lb/sec linear programming problem Mach number maintain FNP maximum thrust mode McDonnell Aircraft McDonnell Douglas Corporation MIL power minimum FTIT mode minimum fuel mode mode is designed NASA Dryden Flight optimization process parameter time histories percent performance seeking control PLA of 40 propulsion system model PSC algorithm PSC engaged pulse code modulation RCVV SMHC SSVM subsonic Supervisory logic Thrust increases thrust-specific fuel consumption tion TLER turbofan variables WF West Palm Beach