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Adaptive Control: Stability, Convergence and Robustness
Shankar Sastry,Marc Bodson
No preview available - 2011
accelerating flight afterburning aircraft altitude CIVV compact inlet model compact propulsion system component deviation parameter constant FNP control variables CPSM cruise flight DEEC degraded engine Dryden Flight Research DWFAN engine operating engine variables estimation process F-15 Airplane fan turbine inlet flight conditions flight data flight test evaluation flight test program flight test results FTIT reductions fuel flow mode Gilyard gine head-up display In-Flight Kalman filter lb/sec linear programming maneuver maximum thrust mode McDonnell Aircraft MIL power MIL-power setting minimum FTIT mode minimum fuel flow minimum temperature mode mode is designed NASA Dryden Flight nontest engine one-engine output variables parametric studies percent performance seeking control pilot propulsion system model PSC algorithm PSC modes PSC sys PSC system engaged RCVV refurbished engine seeking control algorithm seeking control technology single-engine SSVM stall margin subsonic flight test test engine TSFC turbine inlet temperature turbofan two-engine WACC WCFAN