An Electronic Workshop on the Performance Seeking Control and Propulsion Controlled Aircraft Results of the F-15 Highly Integrated Digital Electronic Control Flight Research Program
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[1] Lawrence P. Myers,et al. Performance improvements of an F-15 airplane with an integrated engine-flight control system , 1991 .
[2] R. Luppold,et al. Estimating in-flight engine performance variations using Kalman filter concepts , 1989 .
[3] James F. Stewart,et al. Flight-testing of the self-repairing flight control system using the F-15 highly integrated digital electronic control flight research facility , 1990 .
[4] J. F. Stewart,et al. Dual Engine application of the Performance Seeking Control algorithm , 1993 .
[5] B. Kock. Digital electronic engine control F-15 overview , 1984 .
[6] F. W. Burcham,et al. Effect of control logic modifications on airstart performance of F100 engine model derivative engines in an F-15 airplane , 1984 .
[7] H. H. Lambert,et al. A simulation study of turbofan engine deterioration estimation using Kalman filtering techniques , 1991 .
[8] F. W. Burcham,et al. Flight evaluation of a digital electronic engine control system in an F-15 airplane , 1982 .
[9] Lawrence P. Myers,et al. Propulsion system-flight control integration-flight evaluation and technology transition , 1990 .
[10] D. S. Mcrae,et al. A computational and experimental study of high Reynolds number viscous/inviscid interaction about a cone at high angle of attack , 1980 .
[11] K. J. Szalai. Role of research aircraft in technology development , 1984 .
[12] James Stewart,et al. Flight demonstration of a self repairing flight control system in a NASA F-15 fighter aircraft , 1990 .
[13] T. W. Putnam. Digital electronic engine control history , 1984 .
[14] James F. Stewart. Integrated flight propulsion control research results using the NASA F-15 HIDEC Flight Research Facility , 1992 .
[15] R. E. Curry,et al. Flight evaluation of a pneumatic system for unsteady pressure measurements using conventional sensors , 1989 .
[16] C. M. Carlin,et al. Propulsion/flight control integration technology (PROFIT) design analysis status , 1978 .
[17] F. W. Burcham,et al. Flight evaluation results for a digital electronic engine control in an F-15 airplane , 1983 .
[18] W. J. Barrett,et al. Digital electronic engine control system - F-15 flight test , 1983 .
[19] T. W. Putnam,et al. Summary of results of NASA F-15 flight research program , 1986 .
[20] Jennifer L. Baer-Riedhart,et al. Highly integrated digital electronic control: Digital flight control, aircraft model identification, and adaptive engine control , 1987 .
[21] W. A. Yonke,et al. Integrated flight/propulsion control - Adaptive engine control system mode , 1985 .
[22] L. D. Webb,et al. Selected results of the F-15 propulsion interactions program , 1982 .
[23] Eugene L. Duke,et al. Development and validation of a general purpose linearization program for rigid aircraft models , 1985 .
[24] Trindel A. Maine,et al. Preliminary flight test results of a fly-by-throttle emergency flight control system on an F-15 airplane , 1993 .
[25] K. G. Mackall,et al. Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane , 1984 .
[26] N. S. Dougherty,et al. Boundary-Layer Transition Correlation on a Slender Cone in Wind Tunnels and Flight for Indications of Flow Quality , 1982 .
[27] E. L. Friend,et al. WATER TUNNEL VISUALIZATION OF THE VORTEX FLOWS OF THE F-15* , 1979 .
[28] J. L. Baer-Ruedhart. Digital electronic engine control fault detection and accommodation flight evaluation , 1984 .
[29] C. R. Jarvis,et al. In-flight aerodynamic load testing of the Shuttle thermal protection system , 1981 .
[30] J. B. Johnson. Backup control airstart performance on a digital electronic engine control-equipped F100-engine , 1984 .
[31] Timothy R. Conners,et al. Supersonic Flight Test Results of a Performance Seeking Control Algorithm on a NASA F-15 Aircraft , 1997 .
[32] Odis C. Pendergraft,et al. Results of a wind tunnel/flight test program to compare afterbody/nozzle pressures on a 1/12 scale model and an F-15 aircraft , 1984 .
[33] Frank W. Burcham,et al. Controlling crippled aircraft-with throttles , 1991 .
[34] F. W. Burcham,et al. Flight evaluation of a simplified gross thrust calculation technique using an F100 turbofan engine in an F-15 airplane , 1981 .
[35] F. W. Burcham,et al. Minimum time and fuel flight profiles for an F-15 airplane with a Highly Integrated Digital Electronic Control (HIDEC) system , 1984 .
[36] J. R. Zeller,et al. Flight evaluation of modifications to a digital electronic engine control system in an F-15 airplane , 1983 .
[37] F. W. Burcham,et al. Flight evaluation of a digital electronic engine control in an F-15 airplane , 1985 .
[38] Timothy R. Conners,et al. Thrust stand evaluation of engine performance improvement algorithms in an F-15 airplane , 1992 .
[39] Frank W. Burcham,et al. Augmentor performance of an F100 engine model derivative engine in an F-15 airplane , 1986 .
[40] John S. Orme,et al. Preliminary supersonic flight test evaluation of performance seeking control , 1993 .
[41] John Chisholm,et al. In-flight optimization of the total propulsion system , 1992 .
[42] T. W. Putnam,et al. Flight testing the Digital Electronic Engine Control (DEEC) A unique management experience , 1983 .
[43] L. P. Myers. Flight testing the digital electronic engine control in the F-15 airplane , 1984 .
[44] G. W. Gallops,et al. Performance benefits of adaptive in-flight propulsion system optimization , 1992 .
[45] Lawrence P. Myers,et al. Preliminary Flight Test Results of the F100 EMD Engine in an F·15 Airplane , 1984 .
[46] P. L. Lasagna,et al. Recent propulsion system flight tests at the NASA Dryden Flight Research Center , 1981 .
[47] Frank W. Burcham,et al. A simulation evaluation of a four-engine jet transport using engine thrust modulation for flightpath control , 1991 .
[48] Donna S. Gerren. Design, analysis, and control of large transport aircraft utilizing engine thrust as a backup system for the primary flight controls , 1993 .
[49] L. P. Myers. F-15 digital electronic engine control system description , 1984 .
[50] Trindel A. Maine,et al. A preliminary evaluation of an F100 engine parameter estimation process using flight data , 1990 .
[51] Lawrence P. Myers,et al. Propulsion control experience used in the Highly Integrated Digital Electronic Control (HIDEC) program , 1984 .
[52] C. M. Carlin,et al. Propulsion/flight control integration technology (PROFIT) software system definition , 1978 .
[53] R. J. Ray,et al. Test and evaluation of the HIDEC engine uptrim algorithm , 1986 .